AeroElectric-Archive.digest.vol-pt
September 26, 2020 - October 12, 2020
>>
>> https://www.ebay.ca/itm/192243452240
>>
>> DC-DC Converter
>> 5 Amps
>> Input 3-35 V
>> Output 5-40 V
>>
>> I'm trying to support ~1 A EFIS during start so I thought 5 A would be
>> plenty but a closer look at the description says it's good for 3 A with a
>> maximum of 5 A. Turns out the 3 A is on the input side, not the output
>> side. With a voltage output set point of 10V and a ~1 A lamp connected, the
>> lamp browns out (literally) as soon as the input voltage sags below 9V. A
>> long way from the 7V minimum I was hoping for. I plugged it into a Battery
>> Analyzer at 1.0 and 0.5 A and momentarily dropped the input voltage to 8V.
>> Even when voltage is restored it takes several seconds to recover back to
>> the set voltage with a 1 A load. A 0.5 A load is fine.
>>
>>
>> Good investigative work sir! You're
>> on the right track. The up-converter
>> you have is a bit on the light side.
>>
>> I'd go for beefy . . . and the up-converter
>> needs to be characterized in Watts. A converter
>> that would support a 5A load at 14V would be
>> rated at 70 W or more.
>>
>> The test articles I have on hand are, as I recall,
>> 150 W devices. I'm hoping to put power to them
>> to see if I can characterize their dynamic qualities
>> before I send you one.
>>
>> I'm a bit out of pocket right now. Getting ready for
>> some roto-rooter work on my back . . . got a leg
>> that occasionally says, "I quit". It would not be
>> a good thing to be loading a patient and suddenly
>> find yourself on the ground asking the patient
>> to help you up!
>>
>> Doc says it's a quick fix with excellent
>> prospects for success but in the interim,
>> my forays about the shop are limited. The
>> up converters I have are, I believe, this
>> one:
>>
>> https://tinyurl.com/yxndk24a
>>
>> Price is right, size is convenient . . .
>> and there is little risk for having
>> one that is too big. Thanks for sharing
>> your observations.
>>
>>
>> Bob . . .
>>
>> These:
>>
>> https://www.ebay.com/itm/DC-DC-Converter-10-12-15-20A-150-250-300-400-1200W-Step-up-Step-down-Buck-Boost/382219150784?hash=item58fe0965c0:g:6OwAAOSwisVZrgue
>> Claim to be good down to 8.5V input. Various wattage versions available.
>>
>> Charlie
>>
>>
>> Virus-free.
>> www.avast.com
>>
>> <#m_4222304353412265700_m_4819214867954981025_DAB4FAD8-2DD7-40BB-A1B8-4E2AA1F9FDF2>
>>
>
________________________________________________________________________________
| From: | Sebastien <cluros(at)gmail.com> |
| Subject: | Re: Brownout Step Up Converter |
Very interesting Charlie. I was only using a 1A automotive bulb for load
and as you say my converter looks like it's using the same hardware as
yours so maybe the addition of the second power path makes enough of a
difference? I would not have thought so but it's worth a try, I'll wire it
up again and see.
Also when dropping the voltage down to 8V I'm doing it as quickly as
possible with the power supply fine adjustment. Were you slowly decreasing
the input voltage or doing so suddenly?
Mine was $10 CAD for one and those ones are $30 for 5 so the price is ok.
On Sat, Sep 26, 2020 at 9:55 AM Charlie England
wrote:
> Hi Sebastian,
>
> Thought I'd share some rough testing on a 4A rated booster, that seems to
> use the same inverter IC as the one you're using. I bought these:
>
> https://smile.amazon.com/gp/product/B07XG323G8/ref=ppx_yo_dt_b_asin_title_o00_s00?ie=UTF8&psc=1
> I used an automotive brake light bulb that measures 2A draw at 14V and
> ~1.8A at 12.5V (about what a tired battery might be).
>
> My results with the booster in the circuit, set for 11V output, which
> should be adequate to keep an EFIS alive.
> (list is: supply V/A booster V):
>
> 14/2.1 12.6
> 12/2.0 11.1
> 10/2.7 11.1
> 9/3.1 11.1
> 8.5/3.6 11.0
> 8.0/3.4 10.5
> Supply V/A are read off my cheap Asian variable supply display, and
> rounded to nearest tenth. Booster output V measured with Fluke meter,
> rounded to nearest tenth.
> After several minutes with the supply at 8V, the booster output starts
> dropping a bit. I *suspect* that is because the inverter IC has no heat
> sink and is beginning to thermal-limit to protect itself. In any case, the
> booster should be loaded for only a few seconds during the start event.
>
> Note: One thing I did was to insert a 'fat' diode in series with the
> supply that goes directly to the lamp (also shown in the Z figure). The
> diode output and the booster output both feed the lamp. When supply voltage
> drops below booster output, the diode prevents the booster trying to feed
> back into the supply at the booster's set voltage (obviously impossible).
>
> Did you check your battery voltage at the battery terminals, or were you
> using the EFIS to monitor battery voltage? My experience is that depending
> on how the a/c is wired, the EFIS may see a lower than actual voltage, due
> to diodes (or resistances) in the path to the EFIS input. Battery voltage
> dropping to the 6V area when starting sounds like either high resistance in
> the battery circuit, or a tired battery.
>
> My GRT EFIS has multiple diode-isolated inputs, so the next step is to
> wire the booster from my E-bus to a spare power input on the EFIS & try it
> out.
>
> Charlie
>
> On Sat, Sep 19, 2020 at 11:36 AM Sebastien wrote:
>
>> Now I'm getting confused. The converter Bob linked to has a minimum of 10
>> volts input. Charlie's is 8.5 volts. The only time we want these units
>> working is below 10 volts, and they need to work much lower than that. The
>> last start on my aircraft recorded a 7.6 from a fully charged battery and
>> that's just what the EFIS managed to capture at 1 sample per second.
>>
>> Looking again I have found a couple units that claim to work at very low
>> voltages:
>>
>>
>> https://www.ebay.ca/itm/DC-DC-10A-Buck-Boost-Converter-Step-Up-Down-regulator-Module-for-LED-Driver-US/254169431168
>>
>> https://www.ebay.ca/itm/DC-DC-Buck-Boost-Converter-Adjustable-CC-CV-Step-Up-Down-Power-Supply-Module/124260980594
>>
>> I'm considering ordering one for further testing.
>>
>> Bob best wishes for a quick recovery but take your time. Get yourself
>> fully in fettle before worrying about anyone else!
>>
>> On Sat, Sep 19, 2020 at 8:17 AM Charlie England
>> wrote:
>>
>>> On 9/19/2020 9:26 AM, Robert L. Nuckolls, III wrote:
>>>
>>> At 11:02 PM 9/17/2020, you wrote:
>>>
>>> A couple weeks ago I ordered one of these off eBay:
>>>
>>> https://www.ebay.ca/itm/192243452240
>>>
>>> DC-DC Converter
>>> 5 Amps
>>> Input 3-35 V
>>> Output 5-40 V
>>>
>>> I'm trying to support ~1 A EFIS during start so I thought 5 A would be
>>> plenty but a closer look at the description says it's good for 3 A with a
>>> maximum of 5 A. Turns out the 3 A is on the input side, not the output
>>> side. With a voltage output set point of 10V and a ~1 A lamp connected, the
>>> lamp browns out (literally) as soon as the input voltage sags below 9V. A
>>> long way from the 7V minimum I was hoping for. I plugged it into a Battery
>>> Analyzer at 1.0 and 0.5 A and momentarily dropped the input voltage to 8V.
>>> Even when voltage is restored it takes several seconds to recover back to
>>> the set voltage with a 1 A load. A 0.5 A load is fine.
>>>
>>>
>>> Good investigative work sir! You're
>>> on the right track. The up-converter
>>> you have is a bit on the light side.
>>>
>>> I'd go for beefy . . . and the up-converter
>>> needs to be characterized in Watts. A converter
>>> that would support a 5A load at 14V would be
>>> rated at 70 W or more.
>>>
>>> The test articles I have on hand are, as I recall,
>>> 150 W devices. I'm hoping to put power to them
>>> to see if I can characterize their dynamic qualities
>>> before I send you one.
>>>
>>> I'm a bit out of pocket right now. Getting ready for
>>> some roto-rooter work on my back . . . got a leg
>>> that occasionally says, "I quit". It would not be
>>> a good thing to be loading a patient and suddenly
>>> find yourself on the ground asking the patient
>>> to help you up!
>>>
>>> Doc says it's a quick fix with excellent
>>> prospects for success but in the interim,
>>> my forays about the shop are limited. The
>>> up converters I have are, I believe, this
>>> one:
>>>
>>> https://tinyurl.com/yxndk24a
>>>
>>> Price is right, size is convenient . . .
>>> and there is little risk for having
>>> one that is too big. Thanks for sharing
>>> your observations.
>>>
>>>
>>> Bob . . .
>>>
>>> These:
>>>
>>> https://www.ebay.com/itm/DC-DC-Converter-10-12-15-20A-150-250-300-400-1200W-Step-up-Step-down-Buck-Boost/382219150784?hash=item58fe0965c0:g:6OwAAOSwisVZrgue
>>> Claim to be good down to 8.5V input. Various wattage versions available.
>>>
>>> Charlie
>>>
>>>
>>> Virus-free.
>>> www.avast.com
>>>
>>> <#m_-413585332925668195_m_4222304353412265700_m_4819214867954981025_DAB4FAD8-2DD7-40BB-A1B8-4E2AA1F9FDF2>
>>>
>>
________________________________________________________________________________
| From: | Charlie England <ceengland7(at)gmail.com> |
| Subject: | Re: Brownout Step Up Converter |
I re-ran the test, dialing back to as low as 7V as quickly as possible
while using the pot on the power supply. No difference in characteristics.
I then tried it with the lamp fed only by the booster; same result. At 7V
supply, current demand is a few tenths over the 4A rating of the booster,
and output voltage dropped to right at 10V. Below 7V the booster seems to
shut down (light slowly goes out) and if V is brought back up to ~12V, it
recovers within a second or two. Remember, I'm recording data with Mk1
eyeball & pencil. I'll report again when I get it 'breadboarded' in the
plane.
What's the exchange rate & border penalty in Canada these days? I paid less
than US$8 for the pack of 5, shipped. (Sincere apologies if you're getting
Trumped.)
Charlie
On Sat, Sep 26, 2020 at 12:44 PM Sebastien wrote:
> Very interesting Charlie. I was only using a 1A automotive bulb for load
> and as you say my converter looks like it's using the same hardware as
> yours so maybe the addition of the second power path makes enough of a
> difference? I would not have thought so but it's worth a try, I'll wire it
> up again and see.
>
> Also when dropping the voltage down to 8V I'm doing it as quickly as
> possible with the power supply fine adjustment. Were you slowly decreasing
> the input voltage or doing so suddenly?
>
> Mine was $10 CAD for one and those ones are $30 for 5 so the price is ok.
>
> On Sat, Sep 26, 2020 at 9:55 AM Charlie England
> wrote:
>
>> Hi Sebastian,
>>
>> Thought I'd share some rough testing on a 4A rated booster, that seems to
>> use the same inverter IC as the one you're using. I bought these:
>>
>> https://smile.amazon.com/gp/product/B07XG323G8/ref=ppx_yo_dt_b_asin_title_o00_s00?ie=UTF8&psc=1
>> I used an automotive brake light bulb that measures 2A draw at 14V and
>> ~1.8A at 12.5V (about what a tired battery might be).
>>
>> My results with the booster in the circuit, set for 11V output, which
>> should be adequate to keep an EFIS alive.
>> (list is: supply V/A booster V):
>>
>> 14/2.1 12.6
>> 12/2.0 11.1
>> 10/2.7 11.1
>> 9/3.1 11.1
>> 8.5/3.6 11.0
>> 8.0/3.4 10.5
>> Supply V/A are read off my cheap Asian variable supply display, and
>> rounded to nearest tenth. Booster output V measured with Fluke meter,
>> rounded to nearest tenth.
>> After several minutes with the supply at 8V, the booster output starts
>> dropping a bit. I *suspect* that is because the inverter IC has no heat
>> sink and is beginning to thermal-limit to protect itself. In any case, the
>> booster should be loaded for only a few seconds during the start event.
>>
>> Note: One thing I did was to insert a 'fat' diode in series with the
>> supply that goes directly to the lamp (also shown in the Z figure). The
>> diode output and the booster output both feed the lamp. When supply voltage
>> drops below booster output, the diode prevents the booster trying to feed
>> back into the supply at the booster's set voltage (obviously impossible).
>>
>> Did you check your battery voltage at the battery terminals, or were you
>> using the EFIS to monitor battery voltage? My experience is that depending
>> on how the a/c is wired, the EFIS may see a lower than actual voltage, due
>> to diodes (or resistances) in the path to the EFIS input. Battery voltage
>> dropping to the 6V area when starting sounds like either high resistance in
>> the battery circuit, or a tired battery.
>>
>> My GRT EFIS has multiple diode-isolated inputs, so the next step is to
>> wire the booster from my E-bus to a spare power input on the EFIS & try it
>> out.
>>
>> Charlie
>>
>> On Sat, Sep 19, 2020 at 11:36 AM Sebastien wrote:
>>
>>> Now I'm getting confused. The converter Bob linked to has a minimum of
>>> 10 volts input. Charlie's is 8.5 volts. The only time we want these units
>>> working is below 10 volts, and they need to work much lower than that. The
>>> last start on my aircraft recorded a 7.6 from a fully charged battery and
>>> that's just what the EFIS managed to capture at 1 sample per second.
>>>
>>> Looking again I have found a couple units that claim to work at very low
>>> voltages:
>>>
>>>
>>> https://www.ebay.ca/itm/DC-DC-10A-Buck-Boost-Converter-Step-Up-Down-regulator-Module-for-LED-Driver-US/254169431168
>>>
>>> https://www.ebay.ca/itm/DC-DC-Buck-Boost-Converter-Adjustable-CC-CV-Step-Up-Down-Power-Supply-Module/124260980594
>>>
>>> I'm considering ordering one for further testing.
>>>
>>> Bob best wishes for a quick recovery but take your time. Get yourself
>>> fully in fettle before worrying about anyone else!
>>>
>>> On Sat, Sep 19, 2020 at 8:17 AM Charlie England
>>> wrote:
>>>
>>>> On 9/19/2020 9:26 AM, Robert L. Nuckolls, III wrote:
>>>>
>>>> At 11:02 PM 9/17/2020, you wrote:
>>>>
>>>> A couple weeks ago I ordered one of these off eBay:
>>>>
>>>> https://www.ebay.ca/itm/192243452240
>>>>
>>>> DC-DC Converter
>>>> 5 Amps
>>>> Input 3-35 V
>>>> Output 5-40 V
>>>>
>>>> I'm trying to support ~1 A EFIS during start so I thought 5 A would be
>>>> plenty but a closer look at the description says it's good for 3 A with a
>>>> maximum of 5 A. Turns out the 3 A is on the input side, not the output
>>>> side. With a voltage output set point of 10V and a ~1 A lamp connected, the
>>>> lamp browns out (literally) as soon as the input voltage sags below 9V. A
>>>> long way from the 7V minimum I was hoping for. I plugged it into a Battery
>>>> Analyzer at 1.0 and 0.5 A and momentarily dropped the input voltage to 8V.
>>>> Even when voltage is restored it takes several seconds to recover back to
>>>> the set voltage with a 1 A load. A 0.5 A load is fine.
>>>>
>>>>
>>>> Good investigative work sir! You're
>>>> on the right track. The up-converter
>>>> you have is a bit on the light side.
>>>>
>>>> I'd go for beefy . . . and the up-converter
>>>> needs to be characterized in Watts. A converter
>>>> that would support a 5A load at 14V would be
>>>> rated at 70 W or more.
>>>>
>>>> The test articles I have on hand are, as I recall,
>>>> 150 W devices. I'm hoping to put power to them
>>>> to see if I can characterize their dynamic qualities
>>>> before I send you one.
>>>>
>>>> I'm a bit out of pocket right now. Getting ready for
>>>> some roto-rooter work on my back . . . got a leg
>>>> that occasionally says, "I quit". It would not be
>>>> a good thing to be loading a patient and suddenly
>>>> find yourself on the ground asking the patient
>>>> to help you up!
>>>>
>>>> Doc says it's a quick fix with excellent
>>>> prospects for success but in the interim,
>>>> my forays about the shop are limited. The
>>>> up converters I have are, I believe, this
>>>> one:
>>>>
>>>> https://tinyurl.com/yxndk24a
>>>>
>>>> Price is right, size is convenient . . .
>>>> and there is little risk for having
>>>> one that is too big. Thanks for sharing
>>>> your observations.
>>>>
>>>>
>>>> Bob . . .
>>>>
>>>> These:
>>>>
>>>> https://www.ebay.com/itm/DC-DC-Converter-10-12-15-20A-150-250-300-400-1200W-Step-up-Step-down-Buck-Boost/382219150784?hash=item58fe0965c0:g:6OwAAOSwisVZrgue
>>>> Claim to be good down to 8.5V input. Various wattage versions available.
>>>>
>>>> Charlie
>>>>
>>>>
>>>> Virus-free.
>>>> www.avast.com
>>>>
>>>> <#m_-2951286493721026940_m_-413585332925668195_m_4222304353412265700_m_4819214867954981025_DAB4FAD8-2DD7-40BB-A1B8-4E2AA1F9FDF2>
>>>>
>>>
________________________________________________________________________________
| Subject: | Re: Brownout Step Up Converter |
| From: | Charlie England <ceengland7(at)gmail.com> |
Additional thought. Did you ensure that your bench power supply was
supplying the additional current needed when the voltage drops? Mine has
a current limit knob in addition to the voltage control; I have to be
sure I've dialed in enough current that the supply doesn't hit the limit.
Charlie
On 9/26/2020 2:29 PM, Charlie England wrote:
> I re-ran the test, dialing back to as low as 7V as quicklyas possible
> while using the pot on the powersupply. No difference in
> characteristics.
>
> I then tried it with the lamp fed only by the booster; same result. At
> 7V supply, current demand is a few tenths over the 4A rating of the
> booster, and output voltage dropped to right at 10V. Below 7V the
> booster seems to shut down (light slowly goes out) and if V is brought
> back up to ~12V, it recovers within a second or two. Remember, I'm
> recording data with Mk1 eyeball & pencil. I'll report again when I get
> it 'breadboarded' in the plane.
>
> What's the exchange rate & border penalty in Canada these days? I paid
> less than US$8 for the pack of 5, shipped. (Sincere apologies if
> you're getting Trumped.)
>
> Charlie
>
> On Sat, Sep 26, 2020 at 12:44 PM Sebastien > wrote:
>
> Very interesting Charlie. I was only using a 1A automotive bulb
> for load and as you say my converter looks like it's using the
> same hardware as yours so maybe the addition of the second power
> path makes enough of a difference? I would not have thought so but
> it's worth a try, I'll wire it up again and see.
>
> Also when dropping the voltage down to 8V I'm doing it as quickly
> as possible with the power supply fine adjustment. Were you slowly
> decreasing the input voltage or doing so suddenly?
>
> Mine was $10 CAD for one and those ones are $30 for 5 so the price
> is ok.
>
> On Sat, Sep 26, 2020 at 9:55 AM Charlie England
> > wrote:
>
> Hi Sebastian,
>
> Thought I'd share some rough testing on a 4A rated booster,
> that seems to use the same inverter IC as the one you're
> using. I bought these:
> https://smile.amazon.com/gp/product/B07XG323G8/ref=ppx_yo_dt_b_asin_title_o00_s00?ie=UTF8&psc=1
> I used an automotive brake light bulb that measures 2A draw at
> 14V and ~1.8A at 12.5V (about what a tired battery might be).
>
> My results with the booster in the circuit, set for 11V
> output, which should be adequate to keep an EFIS alive.
> (list is: supply V/A booster V):
>
> 14/2.1 12.6
> 12/2.0 11.1
> 10/2.7 11.1
> 9/3.1 11.1
> 8.5/3.6 11.0
> 8.0/3.4 10.5
> Supply V/A are read off my cheap Asian variable supply
> display, and rounded to nearest tenth. Booster output V
> measured with Fluke meter, rounded to nearest tenth.
> After several minutes with the supply at 8V, the booster
> output starts dropping a bit. I /suspect/ that is because the
> inverter IC has no heat sink and is beginning tothermal-limit
> to protect itself. In any case, the booster should be loaded
> for only a few seconds during the start event.
>
> Note: One thing I did was to insert a 'fat' diode in series
> with the supply that goes directly to the lamp (also shown in
> the Z figure). The diode output and the booster output both
> feed the lamp. When supply voltage drops below booster output,
> the diode prevents the booster trying to feed back into the
> supply at the booster's set voltage (obviously impossible).
>
> Did you check your battery voltage at the battery terminals,
> or were you using the EFIS to monitor battery voltage? My
> experience is that depending on how the a/c is wired, the EFIS
> may see a lower than actual voltage, due to diodes (or
> resistances) in the path to the EFIS input. Battery voltage
> dropping to the 6V area when starting sounds like either high
> resistance in the battery circuit, or a tired battery.
>
> My GRT EFIS has multiple diode-isolated inputs, so the next
> step is to wire the booster from my E-bus to a spare power
> input on the EFIS & try it out.
>
> Charlie
>
> On Sat, Sep 19, 2020 at 11:36 AM Sebastien > wrote:
>
> Now I'm getting confused. The converter Bob linked to has
> a minimum of 10 volts input. Charlie's is 8.5 volts. The
> only time we want these units working is below 10 volts,
> and they need to work much lower than that. The last start
> on my aircraft recorded a 7.6 from a fully charged battery
> and that's just what the EFIS managed to capture at 1
> sample per second.
>
> Looking again I have found a couple units that claim to
> work at very low voltages:
>
> https://www.ebay.ca/itm/DC-DC-10A-Buck-Boost-Converter-Step-Up-Down-regulator-Module-for-LED-Driver-US/254169431168
> https://www.ebay.ca/itm/DC-DC-Buck-Boost-Converter-Adjustable-CC-CV-Step-Up-Down-Power-Supply-Module/124260980594
>
> I'm considering ordering one for further testing.
>
> Bob best wishes for a quick recovery but take your time.
> Get yourself fully in fettle before worrying about anyone
> else!
>
> On Sat, Sep 19, 2020 at 8:17 AM Charlie England
> > wrote:
>
> On 9/19/2020 9:26 AM, Robert L. Nuckolls, III wrote:
>> At 11:02 PM 9/17/2020, you wrote:
>>> A couple weeks ago I ordered one of these off eBay:
>>>
>>> https://www.ebay.ca/itm/192243452240
>>>
>>>
>>> DC-DC Converter
>>> 5 Amps
>>> Input 3-35 V
>>> Output 5-40 V
>>>
>>> I'm trying to support ~1 A EFIS during start so I
>>> thought 5 A would be plenty but a closer look at the
>>> description says it's good for 3 A with a maximum of
>>> 5 A. Turns out the 3 A is on the input side, not the
>>> output side. With a voltage output set point of 10V
>>> and a ~1 A lamp connected, the lamp browns out
>>> (literally) as soon as the input voltage sags below
>>> 9V. A long way from the 7V minimum I was hoping for.
>>> I plugged it into a Battery Analyzer at 1.0 and 0.5
>>> A and momentarily dropped the input voltage to 8V.
>>> Even when voltage is restored it takes several
>>> seconds to recover back to the set voltage with a 1
>>> A load. A 0.5 A load is fine.
>>
>> Good investigative work sir! You're
>> on the right track. The up-converter
>> you have is a bit on the light side.
>>
>> I'd go for beefy . . . and the up-converter
>> needs to be characterized in Watts. A converter
>> that would support a 5A load at 14V would be
>> rated at 70 W or more.
>>
>> The test articles I have on hand are, as I recall,
>> 150 W devices. I'm hoping to put power to them
>> to see if I can characterize their dynamic qualities
>> before I send you one.
>>
>> I'm a bit out of pocket right now. Getting ready for
>> some roto-rooter work on my back . . . got a leg
>> that occasionally says, "I quit". It would not be
>> a good thing to be loading a patient and suddenly
>> find yourself on the ground asking the patient
>> to help you up!
>>
>> Doc says it's a quick fix with excellent
>> prospects for success but in the interim,
>> my forays about the shop are limited. The
>> up converters I have are, I believe, this
>> one:
>>
>> https://tinyurl.com/yxndk24a
>>
>>
>> Price is right, size is convenient . . .
>> and there is little risk for having
>> one that is too big. Thanks for sharing
>> your observations.
>>
>>
>> Bob . . .
>>
> These:
> https://www.ebay.com/itm/DC-DC-Converter-10-12-15-20A-150-250-300-400-1200W-Step-up-Step-down-Buck-Boost/382219150784?hash=item58fe0965c0:g:6OwAAOSwisVZrgue
> Claim to be good down to 8.5V input. Various wattage
> versions available.
>
> Charlie
>
>
> Virus-free. www.avast.com
>
>
>
> <#m_-2951286493721026940_m_-413585332925668195_m_4222304353412265700_m_4819214867954981025_DAB4FAD8-2DD7-40BB-A1B8-4E2AA1F9FDF2>
>
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________________________________________________________________________________
| Subject: | Can radials of home made ground plane be tapered? |
| From: | "rparigoris" <rparigor(at)hotmail.com> |
Hi Group I have a home made ground plane made out of aluminium for a Garmin GA-35
GPS / WAAS antenna. It has 8 radials 1" wide and ~7.75" long. I'm using the
ground plane to support the antenna. It will be living under the ceiling of the
baggage bay in a Europa. After cutting out the ground plane I find that it's
plenty strong enough to support the antenna. Is it OK to taper the radials from
1" at the root to 1/2" at the tip? I could shave off some weight from the
existing 8oz. Ron P.
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498564#498564
________________________________________________________________________________
| Subject: | Re: Can radials of home made ground plane be tapered? |
| From: | "prestonkavanagh" <preston.kavanagh(at)gmail.com> |
Others will respond on the radio theory aspect. I'll say that 8 oz is a heck of
a lot of weight, and you can do better. I believe the Europa has most of the
fiberglass work done at the factory, but I'm guessing you have some supplies
around. Slice off a thin piece of foam, shape it to fit, inset a washer with
ID equal to the antenna mount OD, one layer of BID on each side and you have
something stiff, strong and light. Top it with super thin copper sheet (below
is the one I like), and get a 2 oz mount and ground plane ready to attach to
the airplane.
Or find a friend among the composite builders! Let me know if you are close to
Tampa - I can help. PK
https://www.amazon.com/Conductive-Adhesive-Shielding-Electrical-Grounding/dp/B07R8BS843/ref=sr_1_7?dchild=1&keywords=copper+sheet+foil&qid=1601221863&sr=8-7
--------
PBK3
PA-12, BD-4, RV6a, gliders
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http://forums.matronics.com/viewtopic.php?p=498565#498565
________________________________________________________________________________
| Subject: | Re: Can radials of home made ground plane be tapered? |
| From: | "rparigoris" <rparigor(at)hotmail.com> |
Hi PK I already had all of my antennas installed and the FAA now requires an ADS-B
Out which I need to accommodate. For my situation the most logical position
for my Garmin GA-35 antenna is below the ceiling above the baggage area. The
ceiling slopes and is in a constant changing 3D equation where to lay up something
or attempt to make a metal shelf would be a chore and not look very nice.
My 8 radial .063" ground plane is not just a ground plane but the support for
the antenna. It needs to support ~12 lbs. The antenna with screws is over 8oz.
My Spider / Ninja Shuriken doesn't look too bad, it's honest. I mocked up
a shelf and it looks mucked up. I was thinking about doing exactly as you suggest,
thin glass, some thin foam and some thin glass and cover with copper foil
that I have. The antenna needs to be close to level to the longitudinal axis
which will put the front radial about 2" below the ceiling. Thx. for your offer,
I'm in NY. Aeroplanes are compromises and I'm happy with Spider / Ninja Shuriken.
If I taper the radials I think I can down to 6oz. The ground plane needs
to stay below the base of the antenna which if mounting the antenna inside
out of the slip stream negates ability to put on ceiling. If I mounted it on top
in the slip stream then I could put copper foil inside but I would need to
lift the rear of the antenna and build sort of a submarine bias cut conning tower.
Ron P.
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498566#498566
________________________________________________________________________________
| From: | "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com> |
| Subject: | Re: Can radials of home made ground plane be tapered? |
At 07:34 AM 9/27/2020, you wrote:
>
>Hi Group I have a home made ground plane made out of aluminium for a
>Garmin GA-35 GPS / WAAS antenna. It has 8 radials 1" wide and ~7.75"
>long. I'm using the ground plane to support the antenna. It will be
>living under the ceiling of the baggage bay in a Europa. After
>cutting out the ground plane I find that it's plenty strong enough
>to support the antenna. Is it OK to taper the radials from 1" at the
>root to 1/2" at the tip? I could shave off some weight from the
>existing 8oz. Ron P.
Where did you find recommendations/requirements for
a 'ground plane' on this antenna. I've looked at
some garmin docs and only find references to
antenna/coax grounding to skin . . . no requirements
for any 'tuned' or 'resonant' ground plane in
a plastic airplane.
Bob . . .
________________________________________________________________________________
| Subject: | Re: Can radials of home made ground plane be tapered? |
| From: | "rparigoris" <rparigor(at)hotmail.com> |
Hi Bob
See page 2-5 of GA-35 antenna installation manual: https://static.garmin.com/pumac/190-00848-00_f.pdf
See page 6-8 of GDL-82 installation manual: https://static.garmin.com/pumac/190-01810-00_06.pdf
Ron P.
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498569#498569
________________________________________________________________________________
| From: | Charlie England <ceengland7(at)gmail.com> |
| Subject: | Re: How do you figure C-Rating of a battery? |
On Mon, Sep 14, 2020 at 1:09 PM rparigoris wrote:
> rparigor(at)hotmail.com>
>
> Hi Bob Thank you for your review. I will post schematic when it's
> completed. A few points: I'm not too worried about LiFe batteries getting
> thermal runaway, but I am about LiPo batteries getting to a thermal
> runaway. You posted a link to: https://tinyurl.com/y4oulfy9 As far as
> LiFe batteries go, I think mfg has done a reasonable amount of homework but
> fact is there is potential for problems that Lead Acid does not have and
> they can still fail opened. Good enough for me to use. I'm not worried
> about soldered and crimped connection to aluminium wires, but the terminal
> connections can get a high resistance. Keeping connections clean and tight
> mitigate majority of problems, but not all. As far as keeping NiMh pack
> charged, using one of my AstroFlight delta peak chargers (110D or 112D),
> once or twice a year will give them a C/10 for ~ 15 hours to balance, then
> delta peak charge the rest of the times. Unless battery is very flat,
> peaking at 1C takes less time than a pre-flight. 1x!
> a year will capacity test down to 1V per cell and fuel pump equivalent
> load. BTW have you ever used an AstroFlight Whatt Meter (Whatt is correctly
> spelled)? Pretty slick meter that shows volts, amps and watt hours. Pricey
> though, here's an alternative that works pretty good:
> https://hobbyking.com/en_us/turnigy-180a-watt-meter-and-power-analyzer.html?queryID=7b349d17e0c87dff11877b2ea51342de&objectID=42854&indexName=hbk_live_magento_en_us_products
> Ron P
Ron,
I may have stumbled upon your solution. I know you don't want LiPo in the
cockpit (I can understand that). But if you're comfortable with LiFe for
your main battery....
This:
https://www.harborfreight.com/lithium-ion-jump-starter-and-power-pack-62749.html?_br_psugg_q=jump+starter
At 1st glance, I was sure that it was LiPo. There's nothing in the HF ad
that tells us anything different. But I just saw a video that shows it's
actually a LiFePO4 battery.
https://www.youtube.com/watch?v=EbIQhskJho0&t=636s
The video shows both the label on the back of the case and the label on the
battery module itself, inside the case. Now, I'm not defending the
'installation technique' he used, but the video does show what you'd be
buying. You can see the case at around 3:30 in the video.
It should easily serve the dual requirements of running the fuel pump
alone, or supplying an emergency jump start if you're off-airport
somewhere. I'd find $85 hard to argue with....
Charlie
Virus-free.
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<#DAB4FAD8-2DD7-40BB-A1B8-4E2AA1F9FDF2>
________________________________________________________________________________
| Subject: | Re: Can radials of home made ground plane be tapered? |
| From: | "user9253" <fransew(at)gmail.com> |
Maybe you should call Garmin to find out if a ground plane is really necessary.
Other GPS antenna installations do not call for a ground plane.
Garmin G3X Support
g3xpert at garmin dot com
eight six six -854-8433 - 7 to 7 Central Time M to F
--------
Joe Gores
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498571#498571
________________________________________________________________________________
| From: | "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com> |
| Subject: | Re: Can radials of home made ground plane be |
tapered?
At 03:41 PM 9/27/2020, you wrote:
>
>Hi Bob
>
>See page 2-5 of GA-35 antenna installation manual:
>https://static.garmin.com/pumac/190-00848-00_f.pdf See page 6-8 of
>GDL-82 installation manual: https://static.garmin.com/pumac/190-01810-00_06.pdf
>
>Ron P.
Okay, my copy is rev B and doesn't speak to adding
a ground plane.
I'm a bit mystified by this requirement. The gps/waas
antennas are active devices meaning that the rf samples
from the 'ether' are non-resonant 'probes'
that cannot deliver useful energy into a 50-ohm coax
without electronic (active) augmentation . . .
nor do they have the same capture area of a tuned
and/or multi-element antenna. Ground planes cannot
participate in the delivery of energy to the active
antenna's feedline . . . only in shaping radiation
(reception) patterns.
We've got all manner of gps devices from wrist
watches and little drones to telephones and
cameras. All must depend on active antennas,
in horribly challenging environs . . . no
room for a really efficient antenna.
Now we have a gps system on the backbone of
an airplane, completely free of terrestrial
noise and shadowing with an uncluttered view
of the sky . . . yet the installation instructions
speak of 'optimizing' performance with the
addition of a ground plane under an active
antenna? Hmmm . . .
What's missing from these documents is any
calibration on bang-for-the-buck. I.e. just
how much do I gain with this optimization?
There's a whole bunch of hocky-puck, gps
antennas flying with no ground plane. It
would be interesting to install both
configurations on an airplane with an A-B
switch . . . to observe just how much
optimization is secured with addition
of the ground plane.
I'd be surprised if the optimization offers
more than a little wiggle in the already
more-than-adequate signal strength displays.
Thanks for the update on the manual . . .
Bob . . .
________________________________________________________________________________
| Subject: | Re: antenna analyzer? Antennas |
| From: | Finn Lassen <finn.usa(at)gmail.com> |
Finally got around to playing with nanoVNA and DDRR antenna.
I don't see that it can be used for a Comm antenna (118-136MHz). Too
narrow bandwidth. Tried different things like changing gap, tap point,
height and length. Formulas seem to be off. Found needed smaller circle
(circumference). Also tap location closer to 0.5" that the 2.5 to 2.8"
calculated points. I used a relatively thin wire as opposed to the
recommended 1/4" to 1/2" tubing, hoping it would broaden the bandwidth
(according to this remark:"The larger D is the higher efficiency is").
Bob tried to answer that for me but I'm still not sure if "efficiency"
is related to bandwidth ("Q"). Perhaps I misunderstood that and should
try 1/4" tubing?
With a whip antenna, the bigger the diameter, the broader the bandwidth.
However, for an ELT antenna it will be perfect under engine cowling or
on turtle deck. Saw SWR below 1:1.10 while fiddling with it. Some have
installed their ELT antenna in their RV-4 under the canopy between pilot
and passenger. Obviously without measuring SWR. A hand (much less a head
or the rollover structure) severely affect SWR. Of course ground plane
is very much in question in that location.
I also tried a 3/32" brass tube originating at very rear of canopy
(ground contact to turtle deck) extending forward and up along the
canopy. Very odd frequency response and very SWR sensitive to a hand
near the tip.
At this point I'm looking at designing a streamline base for my 3/32"
brass tubing in Solidworks and 3D printing it, mounting the antenna
traditionally just behind the aft canopy skirt. Perhaps squeezing the
tubing into a somewhat streamline and/or stepping down to 1/8" after the
first 12" piece.
Finn
On 7/15/2020 11:47 PM, Robert L. Nuckolls, III wrote:
> At 04:36 PM 7/15/2020, you wrote:
>
>> I ordered this https://www.ebay.com/itm/283898850600
>> ten days ago. Will probably
>> be several weeks before I get it.
>>
>> You can get them a lot cheaper, but I wanted one that'll also be
>> useful checking transponder (and ADS-B) cable and antenna. (1GHz)
>>
>> Still haven't given up on the idea of putting VHF comm antenna under
>> the RV-4 canopy. Other than vertical polarization, ground plane will
>> probably be the biggest issue (and impedance matching if I can't get
>> the ground plane right). Got three 12" 5/32"OD brass tubes from
>> Hobby Lobby. Should give a reasonably wide bandwidth.
>>
>> Finn
>
> Check out this article from a 1971 issue of QST Magazine
>
> http://www.aeroelectric.com/articles/Antennas/DDRR_Antenna.PDF
> <http://www.aeroelectric.com/articles/Antennas/DDRR_Antenna.PDF>
>
> A 2 meter (146 Mhz) version of this antenna
> is 6" in diameter and sets about 1" off the
> ground plane. An aviation version would be
> about 7" in diameter.
>
> It's bandwidth is probably pretty narrow . . .
> you'd have to build one and sweep it to
> see if it's usable. Would this fit on
> the deck just behind the rear seat?
>
> I've got one of those analyzers but haven't
> had time to make it sing, dance and do dishes.
> I've been using the VNA Tiny which is a good
> bit more expensive. It seems to work well.
> Let us know how that 'baby' VNA works for you!
>
>
> Bob . . .
>
---
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________________________________________________________________________________
| Subject: | Re: antenna analyzer? Antennas |
| From: | Charlie England <ceengland7(at)gmail.com> |
I can't imagine a smaller dia wire spreading the freq peak, but then
I've never seen that style antenna, either. :-) Maybe 'efficiency' in
this context means usability across more of the frequency spectrum
(lower Q). Certainly seems worth trying with 3/8 or 1/2 tubing, or 1/2"
copper tape wrapped around something. Don't know if you care, but most
ELTs require using their dedicated antenna to be 'legal', somewhat
analogous to the silliness in FAA rules for GPS for IFR operations. I
don't worry about the FAA that much, but if you insure the plane, it
could give the ins co an out after an accident.
I assume you're using an old style 121Mhz ELT, right? The new dual freq
models seem to require highly specialized antennas.
RE: brass for antenna. If you're talking about outside the canopy, you
might want to re-think it. My 1st RV4 had the stainless wire whip ELT
antenna mounted there, until it didn't. It broke off at the stress riser
where it entered the long composite mounting cone. Behind the canopy is
a really 'dirty', turbulent area. Maybe you could silver-solder a length
of stainless tubing? Or 1/2" copper tape wrapped on a 'glass arrow
shaft. I bet it'll still need some kind of support a few inches above
the skin.
Have fun...
Charlie
On 9/27/2020 7:17 PM, Finn Lassen wrote:
>
> Finally got around to playing with nanoVNA and DDRR antenna.
>
> I don't see that it can be used for a Comm antenna (118-136MHz). Too
> narrow bandwidth. Tried different things like changing gap, tap point,
> height and length. Formulas seem to be off. Found needed smaller
> circle (circumference). Also tap location closer to 0.5" that the 2.5
> to 2.8" calculated points. I used a relatively thin wire as opposed to
> the recommended 1/4" to 1/2" tubing, hoping it would broaden the
> bandwidth (according to this remark:"The larger D is the higher
> efficiency is"). Bob tried to answer that for me but I'm still not
> sure if "efficiency" is related to bandwidth ("Q"). Perhaps I
> misunderstood that and should try 1/4" tubing?
>
>
> With a whip antenna, the bigger the diameter, the broader the bandwidth.
>
> However, for an ELT antenna it will be perfect under engine cowling or
> on turtle deck. Saw SWR below 1:1.10 while fiddling with it. Some have
> installed their ELT antenna in their RV-4 under the canopy between
> pilot and passenger. Obviously without measuring SWR. A hand (much
> less a head or the rollover structure) severely affect SWR. Of course
> ground plane is very much in question in that location.
>
> I also tried a 3/32" brass tube originating at very rear of canopy
> (ground contact to turtle deck) extending forward and up along the
> canopy. Very odd frequency response and very SWR sensitive to a hand
> near the tip.
>
> At this point I'm looking at designing a streamline base for my 3/32"
> brass tubing in Solidworks and 3D printing it, mounting the antenna
> traditionally just behind the aft canopy skirt. Perhaps squeezing the
> tubing into a somewhat streamline and/or stepping down to 1/8" after
> the first 12" piece.
>
> Finn
>
>
> On 7/15/2020 11:47 PM, Robert L. Nuckolls, III wrote:
>> At 04:36 PM 7/15/2020, you wrote:
>>
>>> I ordered this https://www.ebay.com/itm/283898850600
>>> ten days ago. Will
>>> probably be several weeks before I get it.
>>>
>>> You can get them a lot cheaper, but I wanted one that'll also be
>>> useful checking transponder (and ADS-B) cable and antenna. (1GHz)
>>>
>>> Still haven't given up on the idea of putting VHF comm antenna under
>>> the RV-4 canopy. Other than vertical polarization, ground plane will
>>> probably be the biggest issue (and impedance matching if I can't get
>>> the ground plane right). Got three 12" 5/32"OD brass tubes from
>>> Hobby Lobby. Should give a reasonably wide bandwidth.
>>>
>>> Finn
>>
>> Check out this article from a 1971 issue of QST Magazine
>>
>> http://www.aeroelectric.com/articles/Antennas/DDRR_Antenna.PDF
>> <http://www.aeroelectric.com/articles/Antennas/DDRR_Antenna.PDF>
>>
>> A 2 meter (146 Mhz) version of this antenna
>> is 6" in diameter and sets about 1" off the
>> ground plane. An aviation version would be
>> about 7" in diameter.
>>
>> It's bandwidth is probably pretty narrow . . .
>> you'd have to build one and sweep it to
>> see if it's usable. Would this fit on
>> the deck just behind the rear seat?
>>
>> I've got one of those analyzers but haven't
>> had time to make it sing, dance and do dishes.
>> I've been using the VNA Tiny which is a good
>> bit more expensive. It seems to work well.
>> Let us know how that 'baby' VNA works for you!
>>
>>
>> Bob . . .
>>
>
>
>
> Virus-free. www.avast.com
>
>
>
> <#DAB4FAD8-2DD7-40BB-A1B8-4E2AA1F9FDF2>
--
This email has been checked for viruses by Avast antivirus software.
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________________________________________________________________________________
| From: | "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com> |
| Subject: | Re: antenna analyzer? Antennas |
>I used a relatively thin wire as opposed to the recommended 1/4"
>to 1/2" tubing, hoping it would broaden the bandwidth (according to
>this remark:"The larger D is the higher efficiency is").
>Bob tried to answer that for me but I'm still not sure if
>"efficiency" is related to bandwidth ("Q").
>Perhaps I misunderstood that and should try 1/4" tubing?
Or even a radiator fabricated from flat sheet?
The larger the diameter, the greater the bandwidth.
Efficiency has to do with ohmic losses (how much
energy goes off in heat) and again, a larger surface
area of the radiator has lower resistance. Recall that
currents at these frequencies flow on the skin
of the conductor. At DC, there is a substantial
difference between say a 1" diameter rod and a 1"
thin wall tube. At 100 MHz there is virtually
no difference 'cause all the 'happening' is at
the surface.
>With a whip antenna, the bigger the diameter, the broader the bandwidth.
Exactly . . .
>I also tried a 3/32" brass tube originating at very rear of canopy
>(ground contact to turtle deck) extending forward and up along the
>canopy. Very odd frequency response and very SWR sensitive to a hand
>near the tip.
Interesting observation . . .
>At this point I'm looking at designing a streamline base for my
>3/32" brass tubing in Solidworks and 3D printing it, mounting the
>antenna traditionally just behind the aft canopy skirt. Perhaps
>squeezing the tubing into a somewhat streamline and/or stepping down
>to 1/8" after the first 12" piece.
Also interesting . . . let us know
what you discover.
I am pleased that you've availed yourself
of this unusual piece of test equipment. You're
gaining knowledge and experience in a manner
that you will not forget . . . and will become
valuable information source for those who
follow.
Bob . . .
________________________________________________________________________________
| Subject: | Re: evolution of lithium technologies |
| From: | Charlie England <ceengland7(at)gmail.com> |
On 9/21/2020 11:03 AM, Charlie England wrote:
>
>
> On Sun, Sep 20, 2020 at 11:56 AM Robert L. Nuckolls, III
> >
> wrote:
>
>
> I've been studying current options for lithium
> cells on the market. Discovered some interesting
> things. For example . . . this excerpt from the
> engineering data sheet on an 18650 cell cited
> as suitable for battery powered tools:
>
> [snippped]
> What insults might these cells endure if
> incorporated into a flight system? Any worse
> than those cited above? Just thinking . . .
>
>
> Bob . . .
>
> That got me thinking (and searching).
> A wade into the shallow end of the data pool yields only damp feet
> when it comes to actual *power* capacity. The highest 'continuous
> current' rating I could find on 18650 cells is around 30A. That would
> imply, at 1st glance, at least 10 parallel cells per link in the
> serial chain. Many were limited to around 2A continuous. I couldn't
> find any specs on peak current, either on the bigger vendor sites, or
> on actual mfgr data sheet pdfs. Descriptions of, and differences
> among, the various chemistries and naming conventions, are all over
> the map, depending on which interweb 'authority' you choose to accept.
> Obviously more going on than I can see in the normal data sheets,
> since there are dozens of functional examples of starting batteries on
> the market.
>
> I'd certainly be game for rolling my own battery, but picking the
> right cell seems a task not suited to mere mortals.
>
> Charlie
As a followup,
Do LiFePO4 batteries used for starting have altered chemistry or cell
size, as compared to the 'deep cycle' versions? What about charging
profiles? If not,
https://www.amazon.com/LiFePO4-Battery-Miady-Rechargeable-Maintenance-Free/dp/B07X7MD2JK/ref=sr_1_3?dchild=1&keywords=12V+LiFePO4&qid=1601260110&sr=8-3
Looks interesting as the starting point for the DIY battery idea Bob
mentioned earlier. The terminals are obviously inadequate as made, but
it would be interesting to see what it looks like inside. If larger
terminals could be installed...
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________________________________________________________________________________
| From: | "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com> |
| Subject: | Re: evolution of lithium technologies |
>As a followup,
>Do LiFePO4 batteries used for starting have altered chemistry or
>cell size, as compared to the 'deep cycle' versions? What about
>charging profiles?
Probably. The no-iron lithium products
demonstrate performance all over the map.
I suspect there are similar variations on the
LiFe theme
> If not,
>https://www.amazon.com/LiFePO4-Battery-Miady-Rechargeable-Maintenance-Free/dp/B07X7MD2JK/ref=sr_1_3?dchild=1&keywords=12V+LiFePO4&qid=1601260110&sr=8-3
>Looks interesting as the starting point for the DIY battery idea Bob
>mentioned earlier. The terminals are obviously inadequate as made,
>but it would be interesting to see what it looks like inside. If
>larger terminals could be installed...
Interesting product. Q&A's seem forthright.
He says it's got a BMS that current limits
so upsizing terminals is not likely to let
it crank engines.
It sold with free returns . . . i've ordered one
to shake out.
Bob . . .
________________________________________________________________________________
| Subject: | Re: Z13-8 modification and LSE ignition wiring |
| From: | "Tailwind1" <timmikus38(at)gmail.com> |
Thank you all for your replies to the questions.
T Mikus
--------
Flying Sonerai II with A80 Continental. Wittman W10 Tailwind under construction,
O360, dual LSE electronic ignition, airframe complete and covered, engine hung,
cowl built. Working on electrical, instrumentation, and other details.
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498578#498578
________________________________________________________________________________
| Subject: | Re: Can radials of home made ground plane be tapered? |
I would have to agree. I've had the antenna for a GTN625 installed in a fiberglass
airplane with no groundplane for 5 years and never had a problem with reception.
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498580#498580
________________________________________________________________________________
| From: | Charlie England <ceengland7(at)gmail.com> |
| Subject: | Re: Can radials of home made ground plane be tapered? |
On Sun, Sep 27, 2020 at 3:53 PM rparigoris wrote:
> rparigor(at)hotmail.com>
>
> Hi Bob
>
> See page 2-5 of GA-35 antenna installation manual:
> https://static.garmin.com/pumac/190-00848-00_f.pdf See page 6-8 of GDL-82
> installation manual: https://static.garmin.com/pumac/190-01810-00_06.pdf
>
> Ron P.
>
> I'd be at least a little suspicious of some tech writer 'boilerplating'
installation text from the last install manual he was working on. :-)
Virus-free.
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________________________________________________________________________________
| Subject: | Re: antenna analyzer? Antennas |
| From: | Finn Lassen <finn.usa(at)gmail.com> |
I guess ideally a tapered carbonfiber tube (perhaps wrapped with copper
table within another tapered carbonfiber tube).
I wonder if the carbon material is conductive enough for our purposes.
Finn
On 9/27/2020 8:51 PM, Charlie England wrote:
> RE: brass for antenna. If you're talking about outside the canopy, you
> might want to re-think it. My 1st RV4 had the stainless wire whip ELT
> antenna mounted there, until it didn't. It broke off at the stress
> riser where it entered the long composite mounting cone. Behind the
> canopy is a really 'dirty', turbulent area. Maybe you could
> silver-solder a length of stainless tubing? Or 1/2" copper tape
> wrapped on a 'glass arrow shaft. I bet it'll still need some kind of
> support a few inches above the skin.
---
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________________________________________________________________________________
| From: | "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com> |
| Subject: | Re: antenna analyzer? Antennas |
At 08:43 AM 9/28/2020, you wrote:
>
>I guess ideally a tapered carbonfiber tube (perhaps wrapped with
>copper table within another tapered carbonfiber tube).
Can you easily conduct the experiment? Sounds
interesting.
>I wonder if the carbon material is conductive enough for our purposes.
No. Antennas on our carbon aircraft at Hawker-Beech
required a beefed up ground plane. We also had to add
a distributed ground system for electrics . . . super pain
in the you know what . . .
Bob . . .
________________________________________________________________________________
| From: | "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com> |
| Subject: | Re: Can radials of home made ground plane be |
tapered?
>
>I'd be at least a little suspicious of some tech
>writer 'boilerplating' installation text from
>the last install manual he was working on. :-)=C2
Yeah, AC43-13 was a prime example of 'suggestions' offered
up by folks who never touched an airplane. EAA was invited
to comment on an 'upgrade' to the document ready for imminent
release back about 1995.
I was invited to comment on the electrics. I think a dozen
or more EAA members participated in other areas. EAA sent
a rather comprehensive data package to the FAA . . . the
document release was pushed out 10 months or so . . . and
they still didn't get all the potholes patched.
I think I've got a copy of my submission around here somewhere . . .
it would be interesting to review it 25 or so years later!
That 7.5" radius figure from Garmin doesn't approach any
multiple of 1/4 wave at the frequency of interest. Unless
going for an 'infinite' g.p. then you'd think they would
call out some odd multiple of 1/4 wave at freq of interest.
Bob . . .
________________________________________________________________________________
| Subject: | Re: Can radials of home made ground plane be tapered? |
| From: | "rparigoris" <rparigor(at)hotmail.com> |
Hi Group FWIW I called Garmin and Stein Air and both said to use a ground plane.
I also called Vans. On their RV-12 they install the GA-35 on a small bracket
FWF. I called them and asked about a ground plane and they said that the lower
cowl acts as a ground plane. Here's a post from a guy in the Vans Forum: "I
can tell you this...originally I installed mine under the cowl with little to
no ground plane. It worked....
Later I installed a bigger ground plane and the signal levels definately increased."
It was posted in reply from a 12/30/2012 question in Vans Forum, he doesn't
say what model plane he had, precisely what antenna or how large of a ground
plane. I have now heard of several Europa's and a Long EZ using the GA-35 without
a ground plane with good success. Ron P.
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498586#498586
________________________________________________________________________________
| Subject: | Re: How do you figure C-Rating of a battery? |
| From: | "rparigoris" <rparigor(at)hotmail.com> |
Hi Charlie Thank you for thinking of me! For back up I need something small to
fit in headrest. The HF unit is too big and too heavy.
FWIT here's my take:
Harbor Freight in my experience has been less than truthful when it comes to specs
and quality / reliability is an issue. I was working on a project a while
back and they offered a 18aH jump start pack. It had a battery that was marked
18aH. It was a 12aH battery in a 18aH case! We took out the supplied chargers
and I had a pile of them for a while. After 25 uses failure rate was 10 or 15%.
Just awful. Since we took apart hundreds of units, workmanship was also awful.
Northern tools isn't any better.
For another project I needed 100 amps for a short time. I purchased from Northern Tools one of their 4,000 amp jump packs. At room temp it would put out 40 amps for 3 seconds. If it was cold out probably only 20 or 25 amps.:https://www.northerntool.com/shop/tools/product_200676383_200676383
Their# is 216-464-8131
Their 4,000 amp unit can put out ~ 40 amps for 3 seconds at minimum of 10.9 volts,
after 15 seconds down to ~35 amps and if it were cold probably 20 or 25 amps.
The battery is only 8aH. (I didn't test capacity but question that as well).
Ron P.
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498587#498587
________________________________________________________________________________
| Subject: | Re: How do you figure C-Rating of a battery? |
| From: | Charlie England <ceengland7(at)gmail.com> |
On 9/28/2020 12:13 PM, rparigoris wrote:
>
> Hi Charlie Thank you for thinking of me! For back up I need something small to
fit in headrest. The HF unit is too big and too heavy.
> FWIT here's my take:
> Harbor Freight in my experience has been less than truthful when it comes to
specs and quality / reliability is an issue. I was working on a project a while
back and they offered a 18aH jump start pack. It had a battery that was marked
18aH. It was a 12aH battery in a 18aH case! We took out the supplied chargers
and I had a pile of them for a while. After 25 uses failure rate was 10 or
15%. Just awful. Since we took apart hundreds of units, workmanship was also awful.
> Northern tools isn't any better.
> For another project I needed 100 amps for a short time. I purchased from Northern Tools one of their 4,000 amp jump packs. At room temp it would put out 40 amps for 3 seconds. If it was cold out probably only 20 or 25 amps.:https://www.northerntool.com/shop/tools/product_200676383_200676383
>
> Their# is 216-464-8131
>
> Their 4,000 amp unit can put out ~ 40 amps for 3 seconds at minimum of 10.9 volts,
after 15 seconds down to ~35 amps and if it were cold probably 20 or 25
amps.
>
> The battery is only 8aH. (I didn't test capacity but question that as well).
>
> Ron P.
Yeah; if you watched the entire video, he shows the 2,800mAH battery in
the 12,000mAH case. Unfortunately, finding truth in marketing,
especially while discussing starting batteries, is a fool's quest.
Having said that, can you really fit the same power *and capacity* in
the same space, with nimh batteries? The battery itself looks to be less
than a third the volume of the case.
--
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________________________________________________________________________________
| Subject: | Re: How do you figure C-Rating of a battery? |
| From: | "rparigoris" <rparigor(at)hotmail.com> |
Hi Charlie I already have my headrest fabricated and wired. If I were to do it
again I would do things differently. Energy density of LiFe batteries is better
than that of NiMh. My NiMh pack fits like a glove. You can see the cutout in
the aluminium plate:
http://www.europaowners.org/main.php?g2_itemId=27332
My requirement if I were to switch from NiMh to something else is to have ability
for battery and BMS to fit in existing space.:
http://www.europaowners.org/main.php?g2_itemId=30608
Capacity of NiMh is less than the HF jump pack (according to Mfg. specs.), but
size and weight is a lot less. NiMh pack will weigh under 2lbs. Original old cells
were rated for 2.2aH which would accomplish the task, newest cells are rated
for 5.0aH.
Ron P.
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498589#498589
________________________________________________________________________________
| From: | Charlie England <ceengland7(at)gmail.com> |
| Subject: | Re: How do you figure C-Rating of a battery? |
On Mon, Sep 28, 2020 at 1:46 PM rparigoris wrote:
> rparigor(at)hotmail.com>
>
> Hi Charlie I already have my headrest fabricated and wired. If I were to
> do it again I would do things differently. Energy density of LiFe batteries
> is better than that of NiMh. My NiMh pack fits like a glove. You can see
> the cutout in the aluminium plate:
> http://www.europaowners.org/main.php?g2_itemId=27332
> My requirement if I were to switch from NiMh to something else is to have
> ability for battery and BMS to fit in existing space.:
> http://www.europaowners.org/main.php?g2_itemId=30608
> Capacity of NiMh is less than the HF jump pack (according to Mfg. specs.),
> but size and weight is a lot less. NiMh pack will weigh under 2lbs.
> Original old cells were rated for 2.2aH which would accomplish the task,
> newest cells are rated for 5.0aH.
> Ron P.
>
> Looks nice!
Virus-free.
www.avast.com
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________________________________________________________________________________
| Subject: | Re: antenna analyzer? Antennas |
| From: | Finn Lassen <finn.usa(at)gmail.com> |
Tried with bigger "tubing" (Did not want to spend $ and time going to
local hardware store to pick up 1/2" soft copper tubing and elbow.)
Size of wire or tubing does not appear to influence bandwidth.
So, my conclusion is unchanged: good compact vertically polarized
antenna for single-frequency use, like ELT or 144-146MHz "band".
Not usable as wideband antenna. 118-136MHz certainly is wideband.
(18/127 = 14%).
Would love to have someone else experiment with it and see if they
somehow could get 1:3 SWR over 118-136MHz.
118-137MHz, 1:4 SWR at top.
100-137MHz, 1:4 SWR at top.
You can definitely tune it to much better SWR at center frequency, but
that was not the purpose here.
Finn
On 9/27/2020 9:24 PM, Robert L. Nuckolls, III wrote:
>> I used a relatively thin wire as opposed to the recommended 1/4"
>> to 1/2" tubing, hoping it would broaden the bandwidth (according to
>> this remark:"The larger D is the higher efficiency is").
>> Bob tried to answer that for me but I'm still not sure if
>> "efficiency" is related to bandwidth ("Q").
>> Perhaps I misunderstood that and should try 1/4" tubing?
>
> Or even a radiator fabricated from flat sheet?
>
> The larger the diameter, the greater the bandwidth.
> Efficiency has to do with ohmic losses (how much
> energy goes off in heat) and again, a larger surface
> area of the radiator has lower resistance. Recall that
> currents at these frequencies flow on the skin
> of the conductor. At DC, there is a substantial
> difference between say a 1" diameter rod and a 1"
> thin wall tube. At 100 MHz there is virtually
> no difference 'cause all the 'happening' is at
> the surface.
>
>> With a whip antenna, the bigger the diameter, the broader the bandwidth.
> Exactly . . .
>
>> I also tried a 3/32" brass tube originating at very rear of canopy
>> (ground contact to turtle deck) extending forward and up along the
>> canopy. Very odd frequency response and very SWR sensitive to a hand
>> near the tip.
>
> Interesting observation . . .
>
>> At this point I'm looking at designing a streamline base for my 3/32"
>> brass tubing in Solidworks and 3D printing it, mounting the antenna
>> traditionally just behind the aft canopy skirt. Perhaps squeezing the
>> tubing into a somewhat streamline and/or stepping down to 1/8" after
>> the first 12" piece.
>
> Also interesting . . . let us know
> what you discover.
>
> I am pleased that you've availed yourself
> of this unusual piece of test equipment. You're
> gaining knowledge and experience in a manner
> that you will not forget . . . and will become
> valuable information source for those who
> follow.
>
> Bob . . .
>
---
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________________________________________________________________________________
| From: | "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com> |
| Subject: | Re: antenna analyzer? Antennas |
>
>
>Would love to have someone else experiment with it and see if they
>somehow could get 1:3 SWR over 118-136MHz.
It's been some years since I built one of these
(back in the days before vna's) and a similar
interval since I reviewed the literature.
Poked around on the 'net and my archives a bit
and I think I can confidently offer an explanation
for the fruitlessness of your endeavors.
The DDRR is a vertically polarized antenna wherein
the very short vertical mast is the radiator.
All that other stuff is a loading reactance for
the antenna . . . or 'top hat' in some circles.
Given that the radiation from an antenna is
proportional to the current flowing in the radiator
then it follows that this diminutive antenna
must have some bodacious currents. Further, where
the currents are high, losses need to be low
to minimize energy lost to heating.
My assertion about larger diameters improving
bandwidth was incorrectly applied to this
discussion. L/d ratio as it goes to bandwidth
works only in the resonant radiating portions of the
antenna . . . in this case, the mast. All
that stuff setting on top has a rapidly
diminishing current flow and besides, that
part doesn't radiate.
More surface area (diameter) helps this antenna
only in the radiator . . . the mast supporting
the top hat. Increasing surface area in the loading
portion goes to increased Q which means narrower
bandwidth.
The governing triad is profoundly demonstrated
in the magnetic loop antennas used on the HF
ham bands. There are very useful loop antennas crafted
for the 80M (3.5 to 4.0 Mhz) ham band where
the radiator is built from 1-2" copper pipe with
soldered joints in 45 degree elbows employed
to make an 8-sided 'circle'. The Q of these
antennas is very high which means hi currents
at the feedpoint, high voltages at the tuning
gap. The bandwidth of these antennas is very
narrow. The operator has to tune the antenna
in lockstep with his transceiver in order to
'cruise' that band for contacts.
http://www.oh2gqc.com/wp-content/uploads/2017/09/20170911_160930.jpg
Several sages in the design and fabrication
of antennas have noted, "one can strive for
(1) efficiency, (2) size and/or (3) bandwidth
with one overpowering caveat. Optimizing any two
qualities calls for degrading the third. So pick
two goals and live with consequences for the
third."
Therefore, your experience with the DDRR was
predictable. Yeah, you can get a really useful,
small profile antenna but because SIZE was
diminished, bandwidth suffers.
I thank you for sharing the results of your
experiment.
Bob . . .
________________________________________________________________________________
| From: | David Carter <david(at)carter.net> |
| Subject: | Z101 with Garmin GAD 27 voltage stabilizer |
I have attached a power distribution block diagram (not a schematic) that I
have been working on. I'm trying to puzzle through how best to take
advantage of the voltage stabilizer built into the Garmin GAD 27.
The GAD 27 is Garmin's electrical system controller. It's a combo box that
bundles several functions, including the voltage stabilizer, trim mixer,
flap controller, wigwag control, panel light dimmer, etc.
I'm focused on how to best leverage the voltage stabilizer function to keep
things running smoothly during engine start, and how to build in additional
redundancy by using the dual diode-isolated power inputs available in many
of the Garmin boxes by powering them both from the GAD 27 on the main bus,
and from the Aux bus. I will admit that the failure modes in Z101 where
this redundancy would be used should be exceedingly rare. But the dual
power inputs are there, why not use them?
I have also highlighted 3 devices that have dual power inputs that I'm not
planning to use. One of those, the G5 SFD, has it's own attached backup
battery.
I appreciate any suggestions this group can provide.
[image: image.png]
---
David Carter
david(at)carter.net
________________________________________________________________________________
| Subject: | Re: antenna analyzer? Antennas |
| From: | Finn Lassen <finn.usa(at)gmail.com> |
"mast" Coax to ring or ring to ground plane?
So increasing ring to ground plane to a maybe 3/4" piece of tubing would
increase bandwidth?
But probably not significantly enough to say 1:3 SWR over the 188-136MHz
band?
Finn
On 9/30/2020 5:04 PM, Robert L. Nuckolls, III wrote:
>>
>>
>> Would love to have someone else experiment with it and see if they
>> somehow could get 1:3 SWR over 118-136MHz.
>
> It's been some years since I built one of these
> (back in the days before vna's) and a similar
> interval since I reviewed the literature.
>
> Poked around on the 'net and my archives a bit
> and I think I can confidently offer an explanation
> for the fruitlessness of your endeavors.
>
> The DDRR is a vertically polarized antenna wherein
> the very short vertical mast is the radiator.
> All that other stuff is a loading reactance for
> the antenna . . . or 'top hat' in some circles.
>
> Given that the radiation from an antenna is
> proportional to the current flowing in the radiator
> then it follows that this diminutive antenna
> must have some bodacious currents. Further, where
> the currents are high, losses need to be low
> to minimize energy lost to heating.
>
> My assertion about larger diameters improving
> bandwidth was incorrectly applied to this
> discussion. L/d ratio as it goes to bandwidth
> works only in the resonant radiating portions of the
> antenna . . . in this case, the mast. All
> that stuff setting on top has a rapidly
> diminishing current flow and besides, that
> part doesn't radiate.
>
> More surface area (diameter) helps this antenna
> only in the radiator . . . the mast supporting
> the top hat. Increasing surface area in the loading
> portion goes to increased Q which means narrower
> bandwidth.
>
> The governing triad is profoundly demonstrated
> in the magnetic loop antennas used on the HF
> ham bands. There are very useful loop antennas crafted
> for the 80M (3.5 to 4.0 Mhz) ham band where
> the radiator is built from 1-2" copper pipe with
> soldered joints in 45 degree elbows employed
> to make an 8-sided 'circle'. The Q of these
> antennas is very high which means hi currents
> at the feedpoint, high voltages at the tuning
> gap. The bandwidth of these antennas is very
> narrow. The operator has to tune the antenna
> in lockstep with his transceiver in order to
> 'cruise' that band for contacts.
>
> http://www.oh2gqc.com/wp-content/uploads/2017/09/20170911_160930.jpg
>
> Several sages in the design and fabrication
> of antennas have noted, "one can strive for
> (1) efficiency, (2) size and/or (3) bandwidth
> with one overpowering caveat. Optimizing any two
> qualities calls for degrading the third. So pick
> two goals and live with consequences for the
> third."
>
> Therefore, your experience with the DDRR was
> predictable. Yeah, you can get a really useful,
> small profile antenna but because SIZE was
> diminished, bandwidth suffers.
>
> I thank you for sharing the results of your
> experiment.
>
> Bob . . .
>
---
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________________________________________________________________________________
| From: | Jeff Luckey <jluckey(at)pacbell.net> |
| Subject: | Re: Z101 with Garmin GAD 27 voltage stabilizer |
David,
Wow! That's a lot of busses!=C2- I count 4?=C2- What airplane is this g
oing in?=C2- IIRC, you have an electrically-dependent engine, right?
The block diagram is not super useful for circuit analysis 'cuz it doesn't
show how it's wired.=C2- In other words, one could come up with lots of d
ifferent way to implement what's shown on this Block diagram.=C2- For mea
ningful analysis it would be easier to have a view that is "closer to the m
etal".
Do you have an actual schematic?=C2- That might be more useful to the gro
up to analyze.
-Jeff Luckey
carter.net> wrote:
I have attached a power distribution block diagram (not a schematic) that
I have been working=C2-on. I'm trying to puzzle through how best to take
advantage of the voltage=C2-stabilizer built into the Garmin GAD 27.=C2
-
The GAD 27 is Garmin's electrical system controller. It's a combo box that
bundles several functions, including the voltage stabilizer, trim mixer, fl
ap controller, wigwag control, panel light dimmer, etc.=C2-=C2-
I'm focused on how to best leverage the voltage stabilizer function to keep
things running smoothly during engine start, and how to build in additiona
l redundancy by using the dual diode-isolated power inputs available in man
y of the Garmin boxes by powering them both from the GAD 27 on the main bus
, and from the Aux bus. I will admit that the failure modes in Z101 where t
his redundancy would be used should be exceedingly rare. But the dual power
inputs are there, why not use them?
I have also highlighted 3 devices that have dual power inputs that I'm not
planning to use. One of those, the G5 SFD, has it's own attached backup bat
tery.
I appreciate any suggestions this group can provide.=C2-
---
David Carter
david(at)carter.net
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________________________________________________________________________________
| From: | David Carter <david(at)carter.net> |
| Subject: | Re: Z101 with Garmin GAD 27 voltage stabilizer |
This will be going into a retrofit of a flying RV-7A, equipped for IFR,
with an electrically-dependent engine. Dual SDS CPI-2 ignition, but
mechanical fuel injection & engine-driven fuel pump. I haven't developed
the schematic yet, but it is almost 100% Z101. The only divergence is the
GAD-27 & powering several devices off of two of the busses vs. just one.
Maybe that's overkill.
---
David Carter
david(at)carter.net
On Wed, Sep 30, 2020 at 6:52 PM Jeff Luckey wrote:
> David,
>
> Wow! That's a lot of busses! I count 4? What airplane is this going in?
> IIRC, you have an electrically-dependent engine, right?
>
> The block diagram is not super useful for circuit analysis 'cuz it doesn't
> show how it's wired. In other words, one could come up with lots of
> different way to implement what's shown on this Block diagram. For
> meaningful analysis it would be easier to have a view that is "closer to
> the metal".
>
> Do you have an actual schematic? That might be more useful to the group
> to analyze.
>
>
> -Jeff Luckey
>
> david(at)carter.net> wrote:
>
>
> I have attached a power distribution block diagram (not a schematic) that
> I have been working on. I'm trying to puzzle through how best to take
> advantage of the voltage stabilizer built into the Garmin GAD 27.
>
> The GAD 27 is Garmin's electrical system controller. It's a combo box that
> bundles several functions, including the voltage stabilizer, trim mixer,
> flap controller, wigwag control, panel light dimmer, etc.
>
> I'm focused on how to best leverage the voltage stabilizer function to
> keep things running smoothly during engine start, and how to build in
> additional redundancy by using the dual diode-isolated power inputs
> available in many of the Garmin boxes by powering them both from the GAD 27
> on the main bus, and from the Aux bus. I will admit that the failure modes
> in Z101 where this redundancy would be used should be exceedingly rare. But
> the dual power inputs are there, why not use them?
>
> I have also highlighted 3 devices that have dual power inputs that I'm not
> planning to use. One of those, the G5 SFD, has it's own attached backup
> battery.
>
> I appreciate any suggestions this group can provide.
>
> [image: image.png]
>
>
> ---
> David Carter
> david(at)carter.net
>
________________________________________________________________________________
| From: | "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com> |
| Subject: | Re: antenna analyzer? Antennas |
At 05:33 PM 9/30/2020, you wrote:
>"mast" Coax to ring or ring to ground plane?
the ring to ground plane . . .
>So increasing ring to ground plane to a maybe 3/4" piece of tubing
>would increase bandwidth?
no . . . that radiator is a fraction of a wavelength.
It resonates based on the reactive (capacitive)
effects of the ring.
>But probably not significantly enough to say 1:3 SWR over the 118-136MHz band?
Interesting experiement . . . it might get
wider but probably way short of design
goals.
>Finn
>
>On 9/30/2020 5:04 PM, Robert L. Nuckolls, III wrote:
>>>
>>>
>>>Would love to have someone else experiment with it and see if they
>>>somehow could get 1:3 SWR over 118-136MHz.
>>
>> It's been some years since I built one of these
>> (back in the days before vna's) and a similar
>> interval since I reviewed the literature.
>>
>> Poked around on the 'net and my archives a bit
>> and I think I can confidently offer an explanation
>> for the fruitlessness of your endeavors.
>>
>> The DDRR is a vertically polarized antenna wherein
>> the very short vertical mast is the radiator.
>> All that other stuff is a loading reactance for
>> the antenna . . . or 'top hat' in some circles.
>>
>> Given that the radiation from an antenna is
>> proportional to the current flowing in the radiator
>> then it follows that this diminutive antenna
>> must have some bodacious currents. Further, where
>> the currents are high, losses need to be low
>> to minimize energy lost to heating.
>>
>> My assertion about larger diameters improving
>> bandwidth was incorrectly applied to this
>> discussion. L/d ratio as it goes to bandwidth
>> works only in the resonant radiating portions of the
>> antenna . . . in this case, the mast. All
>> that stuff setting on top has a rapidly
>> diminishing current flow and besides, that
>> part doesn't radiate.
>>
>> More surface area (diameter) helps this antenna
>> only in the radiator . . . the mast supporting
>> the top hat. Increasing surface area in the loading
>> portion goes to increased Q which means narrower
>> bandwidth.
>>
>> The governing triad is profoundly demonstrated
>> in the magnetic loop antennas used on the HF
>> ham bands. There are very useful loop antennas crafted
>> for the 80M (3.5 to 4.0 Mhz) ham band where
>> the radiator is built from 1-2" copper pipe with
>> soldered joints in 45 degree elbows employed
>> to make an 8-sided 'circle'. The Q of these
>> antennas is very high which means hi currents
>> at the feedpoint, high voltages at the tuning
>> gap. The bandwidth of these antennas is very
>> narrow. The operator has to tune the antenna
>> in lockstep with his transceiver in order to
>> 'cruise' that band for contacts.
>>
>>http://www.oh2gqc.com/wp-content/uploads/2017/09/20170911_160930.jpg
>>
>> Several sages in the design and fabrication
>> of antennas have noted, "one can strive for
>> (1) efficiency, (2) size and/or (3) bandwidth
>> with one overpowering caveat. Optimizing any two
>> qualities calls for degrading the third. So pick
>> two goals and live with consequences for the
>> third."
>>
>> Therefore, your experience with the DDRR was
>> predictable. Yeah, you can get a really useful,
>> small profile antenna but because SIZE was
>> diminished, bandwidth suffers.
>>
>> I thank you for sharing the results of your
>> experiment.
>>
>> Bob . . .
>
>
>
>[]
> Virus-free.
> www.avast.com
>
Bob . . .
________________________________________________________________________________
| Subject: | Re: antenna analyzer? Antennas |
| From: | Charlie England <ceengland7(at)gmail.com> |
I did a bit of web browsing on the DDRR. This thread is about a 2 meter
version (above our comm band):
https://forums.qrz.com/index.php?threads/2m-ddrr-antenna-for-vehicle-some-questions.368057/
The thread contains this sentence:
"The DDRR is an inverted-L. A 3" tall, 146 MHz DDRR has a radiation
resistance of 3.0 ohms. The 2:1 VSWR bandwidth is 1.5 MHz."
On 9/30/2020 7:27 PM, Robert L. Nuckolls, III wrote:
> At 05:33 PM 9/30/2020, you wrote:
>
>> "mast" Coax to ring or ring to ground plane?
>
> the ring to ground plane . . .
>
>
>> So increasing ring to ground plane to a maybe 3/4" piece of tubing
>> would increase bandwidth?
>
> no . . . that radiator is a fraction of a wavelength.
> It resonates based on the reactive (capacitive)
> effects of the ring.
>
>
>> But probably not significantly enough to say 1:3 SWR over the
>> 118-136MHz band?
>
> Interesting experiement . . . it might get
> wider but probably way short of design
> goals.
>
>
>> Finn
>>
>> On 9/30/2020 5:04 PM, Robert L. Nuckolls, III wrote:
>>>>
>>>>
>>>> Would love to have someone else experiment with it and see if they
>>>> somehow could get 1:3 SWR over 118-136MHz.
>>>
>>> It's been some years since I built one of these
>>> (back in the days before vna's) and a similar
>>> interval since I reviewed the literature.
>>>
>>> Poked around on the 'net and my archives a bit
>>> and I think I can confidently offer an explanation
>>> for the fruitlessness of your endeavors.
>>>
>>> The DDRR is a vertically polarized antenna wherein
>>> the very short vertical mast is the radiator.
>>> All that other stuff is a loading reactance for
>>> the antenna . . . or 'top hat' in some circles.
>>>
>>> Given that the radiation from an antenna is
>>> proportional to the current flowing in the radiator
>>> then it follows that this diminutive antenna
>>> must have some bodacious currents. Further, where
>>> the currents are high, losses need to be low
>>> to minimize energy lost to heating.
>>>
>>> My assertion about larger diameters improving
>>> bandwidth was incorrectly applied to this
>>> discussion. L/d ratio as it goes to bandwidth
>>> works only in the resonant radiating portions of the
>>> antenna . . . in this case, the mast. All
>>> that stuff setting on top has a rapidly
>>> diminishing current flow and besides, that
>>> part doesn't radiate.
>>>
>>> More surface area (diameter) helps this antenna
>>> only in the radiator . . . the mast supporting
>>> the top hat. Increasing surface area in the loading
>>> portion goes to increased Q which means narrower
>>> bandwidth.
>>>
>>> The governing triad is profoundly demonstrated
>>> in the magnetic loop antennas used on the HF
>>> ham bands. There are very useful loop antennas crafted
>>> for the 80M (3.5 to 4.0 Mhz) ham band where
>>> the radiator is built from 1-2" copper pipe with
>>> soldered joints in 45 degree elbows employed
>>> to make an 8-sided 'circle'. The Q of these
>>> antennas is very high which means hi currents
>>> at the feedpoint, high voltages at the tuning
>>> gap. The bandwidth of these antennas is very
>>> narrow. The operator has to tune the antenna
>>> in lockstep with his transceiver in order to
>>> 'cruise' that band for contacts.
>>>
>>> http://www.oh2gqc.com/wp-content/uploads/2017/09/20170911_160930.jpg
>>>
>>> Several sages in the design and fabrication
>>> of antennas have noted, "one can strive for
>>> (1) efficiency, (2) size and/or (3) bandwidth
>>> with one overpowering caveat. Optimizing any two
>>> qualities calls for degrading the third. So pick
>>> two goals and live with consequences for the
>>> third."
>>>
>>> Therefore, your experience with the DDRR was
>>> predictable. Yeah, you can get a really useful,
>>> small profile antenna but because SIZE was
>>> diminished, bandwidth suffers.
>>>
>>> I thank you for sharing the results of your
>>> experiment.
>>>
>>> Bob . . .
>>
>>
>> []
>> Virus-free.
>> www.avast.com
>> <#DAB4FAD8-2DD7-40BB-A1B8-4E2AA1F9FDF2>
>
>
> Bob . . .
>
--
This email has been checked for viruses by Avast antivirus software.
https://www.avast.com/antivirus
________________________________________________________________________________
| From: | "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com> |
| Subject: | Re: antenna analyzer? Antennas |
At 08:32 PM 9/30/2020, you wrote:
>I did a bit of web browsing on the DDRR. This thread is about a 2
>meter version (above our comm band):
>https://forums.qrz.com/index.php?threads/2m-ddrr-antenna-for-vehicle-some-questions.368057/
> The thread contains this sentence:
>
>"The DDRR is an inverted-L. A 3" tall, 146 MHz DDRR has a radiation
>resistance of 3.0 ohms. The 2:1 VSWR bandwidth is 1.5 MHz."
Fairly typical. Radiator height is 3/21 or 15% of the
full size 1/4 wave. They cited a vswr 2:1 bandwidth
of 1.5/146 or 1% . . . 3:1 would be a bit wider
but still far short of that necessary for our
VHF comm bandwidths.
I'm still thinking I'd like to build one for our
local fire/ems services where 1% bandwidth is
plenty. The thing could reside under a plastic
radome and sit on a dedicated ground plane held
to the vehicle with magnets in each corner. Just
one of many PITS (pie-in-the-sky) projects in
someday bucket.
This still doesn't solve Finn's problem.
Remind me sir, what airplane are we talking
about?
Bob . . .
________________________________________________________________________________
| From: | "bobnoffs" <icubob(at)gmail.com> |
hi all,
i have earthx batteries and would like to install a voltage warning separate from
my eis. the device must activate below 13.5 volts . does anyone have any
recommendations? i would think something is out there but i haven't seen it.
thanks, bob noffs
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498614#498614
________________________________________________________________________________
| Subject: | ADS-B and Transponder antenna... |
| From: | "andymeyer" <meyerkc135(at)gmail.com> |
So, all this chatter about the ELT antennas got me thinking about the ADS-B antenna
I made. I dove into the math, made some estimates, and designed two on Upverter
and had parts made. I got luck in that my SlimJim ADS-B antenna has picked
up airborne traffic over 100 miles away connected to a Stratux (I have both
SDR radios tied into a single antenna - criminal - I know, but it works and
it's small and light.)
Attached are the layouts of the two antennas and links to the actual designs on
Upverter.
I had 5 of each made. Anyone interested in testing and sharing data - maybe make
this a shared design as well. Cost is just a few bucks.
Slim Jim: https://upverter.com/eda/#tool=pcb,designId=1d1c59be761e9901
DiPole: https://upverter.com/eda/#tool=pcb,designId=9eb3fbd043861e96
(Upverter is a pretty awesome cloud based schematic and layout tool that allows
collaboration on designs, etc... Think Google Docs for circuit design.)
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498615#498615
Attachments:
http://forums.matronics.com//files/20201001_093353_131.jpg
http://forums.matronics.com//files/dipole_103.png
http://forums.matronics.com//files/slimjim_164.png
________________________________________________________________________________
| From: | Charlie England <ceengland7(at)gmail.com> |
| Subject: | Re: voltage monitor |
On Thu, Oct 1, 2020 at 8:39 AM bobnoffs wrote:
>
> hi all,
> i have earthx batteries and would like to install a voltage warning
> separate from my eis. the device must activate below 13.5 volts . does
> anyone have any recommendations? i would think something is out there but i
> haven't seen it.
> thanks, bob noffs
>
Hi Bob,
A friend of mine has been using this for years, to alert him of alternator
loss since he's using electronic ignition on his Lyc:
https://www.tomtop.com/p-e1021.html
It can be programmed to alert for both over and under-voltage and output
fed to whatever you choose; light, buzzer, etc.
I bought a couple, but they're still sitting in my 'toy box'; I haven't had
an urgent need for one yet. FWIW, the guy who's using it has one of the
nicest RV8s I've ever seen, and doesn't do anything 'half-way'. If it's
good enough for him...
Charlie
________________________________________________________________________________
| From: | Charles Kuss <chaskuss(at)yahoo.com> |
| Subject: | Re: voltage monitor |
Bob,
Here are two offerings with the ability to handle Lithium batteries, which
actually run about 1 volt above AGM and standard flooded batteries. Both ar
e small, rugged and inexpensive.
https://gammatronixltd.com/epages/bae94c71-c5b6-4572-89a1-e89006e78fbe.sf/e
n_GB/?ObjectPath=/Shops/bae94c71-c5b6-4572-89a1-e89006e78fbe/Categories/C
ategory1
http://roadstercycle.com/Motorcycle%20voltage%20monitor.htm
Per Shorai's web site, their LiFe batteries are fully charged at 14.34 volt
s, as opposed to 13.2 volts for an AGM or flooded lead/acid battery. See we
b link below
https://shoraipower.com/faq
>From that page, click on the question Q. Can I use Lead-Acid battery charge
rs or charger/tenders?
You will see Shorai's charging table.
Charlie K
com> wrote:
hi all,
i have earthx batteries and would like to install a voltage warning separa
te from my eis. the device must=C2- activate below 13.5 volts . does anyo
ne have any recommendations? i would think something is out there but i hav
en't seen it.
thanks, bob noffs
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498614#498614
-
S -
WIKI -
-
=C2- =C2- =C2- =C2- =C2- -Matt Dralle, List Admin.
________________________________________________________________________________
| Subject: | Can I power ADS-B from Transponder switched output? |
| From: | "rparigoris" <rparigor(at)hotmail.com> |
Hi Group I have a Garmin GDL-82 ADS-B that draws .35A typical and .4A maximum.
I have a Becker Mode-C transponder that has a 1A switched output. Is there a good
reason why I should not use the transponder switched output to power the ADS-B?
I don't have an avionics bus. Ron P.
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498618#498618
________________________________________________________________________________
| Subject: | Re: Can I power ADS-B from Transponder switched output? |
| From: | "user9253" <fransew(at)gmail.com> |
Since the two units work together as a team, it is not an emergency if you lose
both.
On the other hand, best practice is to protect each individual load with its own
fuse.
--------
Joe Gores
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498619#498619
________________________________________________________________________________
| Subject: | Re: Can I power ADS-B from Transponder switched output? |
| From: | "rparigoris" <rparigor(at)hotmail.com> |
Hi User 9253 The switched output of the Becker transponder has a 1 amp fuse. Is
that OK? Ron P.
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498620#498620
________________________________________________________________________________
| Subject: | Re: voltage monitor |
| From: | "rparigoris" <rparigor(at)hotmail.com> |
Hi Bob I don't know what type of regulator you have, but I have a B&C LR3D that
B&C calibrated the Low Voltage Warning for LiFe and also have a B&C AVC1 for
Rotax 914 internal generator that you can select LiFe Low Voltage Warning. I'm
using a Earth 680C. Ron P.
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498621#498621
________________________________________________________________________________
| Subject: | Re: Can I power ADS-B from Transponder switched output? |
| From: | "user9253" <fransew(at)gmail.com> |
OK then, since the transponder DC output is fused and units are related, I think
it is OK to wire them as proposed.
--------
Joe Gores
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498623#498623
________________________________________________________________________________
| From: | "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com> |
| Subject: | First peek at the HeatShrink Butt Splices |
This application specific crimp too for heat-shrink
butt-splices came in today. Thought I'd give you
a heads-up on the 'first smash'.
https://tinyurl.com/yywskeds
The RED aperture for the 22-16AWG splices
is ALMOST tight enough. About 1 in 4 splices
on 22AWG wire would fail an 8# pull test.
However, if one stripped the wire 1/2" and
doubled the stranding back, all test crimps
would pass.
The downside is that the shrink will not
close on small profile insulation . . . like
22759. Fully shrunk, there is no contact
of the insulation on the wire . . . no tell-tale
oozing of sealant from the ends telling us
that environmental protection has been
achieved.
The upside is that they do seal on the
22AWG with the larger, irradiated PVC
wire.
The rectangular crimp die does produce
less trauma to the insulation hence the
finished joint looks better that those
I've made in the past with 'non specific'
tools.
Watch this space. I'll see if I can do
a Shop Notes on this tool/materials
combination.
Bob . . .
________________________________________________________________________________
| Subject: | Re: antenna analyzer? Antennas |
| From: | "Eric Page" <edpav8r(at)yahoo.com> |
Perhaps not helpful to the antenna design y'all are pursuing in this thread, but
I came across this paper today...
http://www.jpier.org/PIERM/pierm78/11.18102701.pdf
...thanks to the guys at DarkAero...
https://www.darkaero.com/
...who are experimenting with this antenna for their all-carbon fiber aircraft.
The paper describes an interesting printed circuit board antenna of meandering
design. It looks very useful for builders looking to avoid long external antennae,
and if the bandwidth shown for a ~160MHz design can be duplicated at ~120MHz,
it should work well.
Eric
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498626#498626
________________________________________________________________________________
| Subject: | Re: voltage monitor |
| From: | "bobnoffs" <icubob(at)gmail.com> |
i ordered the tom top unit. for $5 i gotta see how it works.
talked to perihelion and i believe they can build their 'idiot light' to my
specs.this is a panel light with the electronics self contained.
any more suggestions i would like to hear.
thanks, bob noffs
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498628#498628
________________________________________________________________________________
| From: | "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com> |
| Subject: | Re: ov warning light |
> . . . warning is to protect 2 earthx batteries.
Why do your EarthX batteries need protecting?
Is your alternator/regulator system fitted with
a legacy ov management feature?
If the later is true, then an ov condition can
persist for only a few tens of milliseconds and
would probably never be noticed. Even if noticed,
what relevance would it have to your next
action in the cockpit?
Bob . . .
________________________________________________________________________________
| Subject: | Re: ADS-B and Transponder antenna design... |
| From: | "andymeyer" <meyerkc135(at)gmail.com> |
And I'm willing to send a pair of antennas to someone who's willing to analyze.
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498632#498632
________________________________________________________________________________
| From: | Charlie England <ceengland7(at)gmail.com> |
| Subject: | Re: ADS-B and Transponder antenna design... |
On Fri, Oct 2, 2020 at 4:28 PM andymeyer wrote:
> >
>
> And I'm willing to send a pair of antennas to someone who's willing to
> analyze.
>
Hi Andy,
I'm creating a new SD card 'build' for a Stratux as I type this. I'm
definitely interested; and what do you use for a combiner, and what cable
and cable length will work? I need to get the Stratux off the dash, and
mounting it between the instrument panel & firewall will be the easiest
location for me.
Assuming it'll work out for me, where & how much do I need to send?
Many thanks,
Charlie
ceengland7(at)gmail.com
________________________________________________________________________________
| From: | "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com> |
| Subject: | Re: ADS-B and Transponder antenna design... |
At 04:51 PM 10/2/2020, you wrote:
>On Fri, Oct 2, 2020 at 4:28 PM andymeyer
><meyerkc135(at)gmail.com> wrote:
>"andymeyer" <meyerkc135(at)gmail.com>
>
>And I'm willing to send a pair of antennas to
>someone who's willing to analyze.
>
>=C2
>Hi Andy,
>
>I'm creating a new SD card 'build' for a Stratux
>as I type this. I'm definitely interested; and
>what do you use for a combiner, and what cable
>and cable length will work? I need to get the
>Stratux off the dash, and mounting it between
>the instrument panel & firewall will be the easiest location for me.
combiners? ADSB antennas? enlighten me please
Bob . . .
________________________________________________________________________________
| Subject: | Re: ADS-B and Transponder antenna design... |
| From: | Charlie England <ceengland7(at)gmail.com> |
=81=A3Sent from BlueMail =8B
On Oct 2, 2020, 10:28 PM, at 10:28
PM, "Robert L=2E Nuckolls, III" wrote:
>At 04:51 PM 10/2/2020, you wrote:
>
>
>>On Fri, Oct 2, 2020 at 4:28 PM an
dymeyer
>><meyerkc135@gmail=2Ecom> wrote:
>
>>"andymeyer" <meyerkc135@gmail=2Ecom>
>>
>>And I'm willing to send a pair o
f antennas to
>>someone who's willing to analyze=2E
>>
>>=C3=82
>>Hi Andy,
>>
>>I'm creating a new SD card 'build' for a Stratux
>>as I type this=2E
I'm definitely interested; and
>>what do you use for a combiner, and what
cable
>>and cable length will work? I need to get the
>>Stratux off the
dash, and mounting it between
>>the instrument panel & firewall will be th
e easiest location for me=2E
>
> combiners? ADSB antennas? enlighten me p
lease
>
>
> Bob =2E =2E =2E
________________________________________________________________________________
| From: | "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com> |
| Subject: | Re: ADS-B and Transponder antenna design... |
>
>
>he described them with pics several days ago.
Oh yeah . . . the pix didn't come thru here but okay . . .
understand now.
Bob . . .
________________________________________________________________________________
| From: | skywagon185guy <skywagon185(at)gmail.com> |
| Subject: | Re: voltage monitor |
I personally like the idea of a panel light that will make you aware of
Under and well as Over voltage conditions.
I have experienced an under voltage on start up. Caused by a defective main
circuit breaker that opened, but did not show an indication that it had
mysteriously opened. Luckily, before beginning the taxi, I noted the
amp/volt meter was amiss.
Tested the CB and could not get it to reset. Installed new CB and had no
additional problems.
On Fri, Oct 2, 2020 at 3:41 AM bobnoffs wrote:
>
> i ordered the tom top unit. for $5 i gotta see how it works.
> talked to perihelion and i believe they can build their 'idiot light'
> to my specs.this is a panel light with the electronics self contained.
> any more suggestions i would like to hear.
> thanks, bob noffs
>
>
> Read this topic online here:
>
> http://forums.matronics.com/viewtopic.php?p=498628#498628
>
>
________________________________________________________________________________
| From: | "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com> |
| Subject: | Re: voltage monitor |
At 03:35 PM 10/3/2020, you wrote:
>I personally like the idea of a panel light that
>will make you aware of Under and well as Over voltage conditions.
>I have experienced an under voltage on start up.
>Caused by a defective main circuit breaker
>that opened, but did not show an indication that it had mysteriously
opened.
Then I take it that your system was not fitted
with active notification of low voltage. This
feature is the FIRST if not the ONLY voltage
sensing/indicating device NECESSARY for flight
operations.
Preferably, this light is bright (sunlight viewable)
and located well within peripheral vision of the pilot.
Further, it should flash at 2-3 times per second
(a legacy value for optimal attention getting
arrived at by numerous human factors studies ).
This light has been a no-extra-charge built in feature
of virtually all B&C alternator controllers. From
day-one (about 35 years ago). It was B&C's mission that
no customer would be without BOTH low volts and
over volts management.
Luckily, before beginning the taxi, I noted the amp/volt meter was amiss.
>Tested the CB and could not get it to
>reset.=C2 Installed new CB and had no additional problems.
Yes, there was an element of luck associated with
that experience. I'm pleased the event resolved
without a tense-day-in-the-cockpit.
Along with active notification of low volts, you
should plan on independent management of an over
voltage condition with a system that disables
the alternator within 500 milliseconds of having
exceeded 16 volts.
Depending on design parameters of the designer,
the ov event will be over very soon thus leaving
you with a low volts condition that will be
annunciated as cited above.
Fit your airplane with those two features and
all the other voltmeters, ammeters, beeps
and squawks from the panel mounted goodies
become mere icing on the cake.
Bob . . .
________________________________________________________________________________
| Subject: | field current supplied from B lead instead of from |
main bus
| From: | "johnbright" <john_s_bright(at)yahoo.com> |
Hi Bob,
Someone in my sphere suggested getting field current from the B lead instead of
from the main bus.
This way if the B lead shorts to ground and the fuselink opens, the field will
be de-energized.
Marked up snip of Z101B attached.
Comments?
Thanks
--------
John Bright, RV-6A, at FWF, O-360
Z-101 single batt dual alt SDS EM-5-F.
john_s_bright(at)yahoo.com, Newport News, Va
https://drive.google.com/drive/folders/1u6GeZo6pmBWsKykLNVQMvu4o1VEVyP4K
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498646#498646
Attachments:
http://forums.matronics.com//files/is_connecting_field_supply_to_b_lead_a_good_idea_210.jpg
________________________________________________________________________________
| From: | bob noffs <icubob(at)gmail.com> |
| Subject: | Re: voltage monitor |
since my first post perihelion design has let me know that their idiot
light can be made to any high/low settings. pretty slick fix. 2 leads [i
assume] and it all fits in a .55'' panel hole. light can be ordered
flashing or steady.
On Sat, Oct 3, 2020 at 4:11 PM Robert L. Nuckolls, III <
nuckolls.bob(at)aeroelectric.com> wrote:
> At 03:35 PM 10/3/2020, you wrote:
>
> I personally like the idea of a panel light that will make you aware of
> Under and well as Over voltage conditions.
> I have experienced an under voltage on start up. Caused by a defective
> main circuit breaker
> that opened, but did not show an indication that it had mysteriously
> opened.
>
>
> Then I take it that your system was not fitted
> with active notification of low voltage. This
> feature is the FIRST if not the ONLY voltage
> sensing/indicating device NECESSARY for flight
> operations.
>
> Preferably, this light is bright (sunlight viewable)
> and located well within peripheral vision of the pilot.
> Further, it should flash at 2-3 times per second
> (a legacy value for optimal attention getting
> arrived at by numerous human factors studies ).
>
> This light has been a no-extra-charge built in feature
> of virtually all B&C alternator controllers. From
> day-one (about 35 years ago). It was B&C's mission that
> no customer would be without BOTH low volts and
> over volts management.
>
> Luckily, before beginning the taxi, I noted the amp/volt meter was amiss
.
>
> Tested the CB and could not get it to reset.=C3=82 Installed new CB and
had no
> additional problems.
>
>
> Yes, there was an element of luck associated with
> that experience. I'm pleased the event resolved
> without a tense-day-in-the-cockpit.
>
> Along with active notification of low volts, you
> should plan on independent management of an over
> voltage condition with a system that disables
> the alternator within 500 milliseconds of having
> exceeded 16 volts.
>
> Depending on design parameters of the designer,
> the ov event will be over very soon thus leaving
> you with a low volts condition that will be
> annunciated as cited above.
>
> Fit your airplane with those two features and
> all the other voltmeters, ammeters, beeps
> and squawks from the panel mounted goodies
> become mere icing on the cake.
>
>
> Bob . . .
>
________________________________________________________________________________
| Subject: | Re: voltage monitor |
| From: | "bobnoffs" <icubob(at)gmail.com> |
the rub with low voltage indicators is that they set their low voltage for lead
acid batteries. this is too low and useless for earthx lipo. low voltage warning
must go on below 13.5 volts. when i started this post i talked to b and c
about a warning system they had. the voltage was not adjustable and set for lead
acid......no good for lipo. b and c said that most electronics is adjustable
today and there was never a market for a higher low warning. my system is adjustable
but i do not want to probe my ecu with my computer just to make a limit
change.
earthx users....what's in your wallet? er i mean low voltage setting?
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498650#498650
________________________________________________________________________________
| From: | "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com> |
| Subject: | Re: field current supplied from B lead instead of |
from main bus
At 11:11 PM 10/3/2020, you wrote:
>
>
>Hi Bob,
>
>Someone in my sphere suggested getting field current from the B lead
>instead of from the main bus.
>
>This way if the B lead shorts to ground and the fuselink opens, the
>field will be de-energized.
>
>Marked up snip of Z101B attached.
>
>Comments?
If there is a fault that opens the fusible
link, then the alternator is isolated from
the ship's systems. While the field would
still be energized, the resulting condition
is internal to the alternator and not a
threat to the rest of the airplane.
If the regulator senses bus voltage through
the breaker, then you will depress bus voltage
by whatever drop occurs in the b-lead. Further,
the b-terminal to field breaker lead becomes and extension
of the bus and would need to get a fusible
link at the b-lead.
Presently, I see no particular advantage
for doing this.
Bob . . .
________________________________________________________________________________
| From: | "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com> |
| Subject: | Re: voltage monitor |
At 10:58 AM 10/4/2020, you wrote:
>
>the rub with low voltage indicators is that they set their low
>voltage for lead acid batteries. this is too low and useless for
>earthx lipo. low voltage warning must go on below 13.5 volts. when i
>started this post i talked to b and c about a warning system they
>had. the voltage was not adjustable and set for lead acid......no
>good for lipo. b and c said that most electronics is adjustable
>today and there was never a market for a higher low warning. my
>system is adjustable but i do not want to probe my ecu with my
>computer just to make a limit change.
> earthx users....what's in your wallet? er i mean low voltage setting?'
Not sure I understand this. Check out this family of
discharge plots on 3 brands of LiFePo4 batteries
including an EarthX.
https://tinyurl.com/y4nsp8lr
Looks to me like 13.5V is still a good number.
Bob . . .
________________________________________________________________________________
| From: | "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com> |
| Subject: | Re: Can radials of home made ground plane be |
tapered?
At 11:43 AM 9/28/2020, you wrote:
>
>Hi Group FWIW I called Garmin and Stein Air and both said to use a
>ground plane. I also called Vans. On their RV-12 they install the
>GA-35 on a small bracket FWF. I called them and asked about a ground
>plane and they said that the lower cowl acts as a ground plane.
Not one of those assertion suggest that
there is any DATA to support the recommendation.
> Here's a post from a guy in the Vans Forum: "I can tell you
> this...originally
>I installed mine under the cowl with little to no ground plane. It worked....
Not necessarily 'hard' data but certainly
compelling . . .
>Later I installed a bigger ground plane and the signal levels
>definately increased." It was posted in reply from a 12/30/2012
>question in Vans Forum, he doesn't say what model plane he had,
>precisely what antenna or how large of a ground plane. I have now
>heard of several Europa's and a Long EZ using the GA-35 without a
>ground plane with good success. Ron P.
Interesting. I'm not suggesting that a ground
plane under a gps antenna is not beneficial,
only wondering if it's observably useful.
I recall discussions on the amateur built forums
in years past about adding a ram-air induction port
to the airplane's cowl. I seems some builder made
some valid measurements of available manifold pressure
with and without such a feature. He opined there was value
in fabricating one.
I think the discussion died out when
an engine guru reminded us that airspeed
goes up the cube root of h.p. and the fractional
improvement for the addition would be difficult
to measure much less observe in actual practice.
Methinks the GPS ground plane may fall into
this category as well. There are millions
and millions of GPS based appliances that
perform as advertised with exceedingly
'deficient' antennas. It seems that somewhere
between the least and the best, there is
a demonstrable configuration that would save
OBAM aircraft builders hours of no-value-added
effort on their project.
Bob . . .
________________________________________________________________________________
| Subject: | Re: voltage monitor |
| From: | "bobnoffs" <icubob(at)gmail.com> |
without any mod the 'idiot light' comes preset to warn below 13.0 volts. in a lead
acid set up this would catch the alternator soon after it went off line and
a lead acid would have most of its charge left. when a lipo drops below 13 volts
a lot of its charge is already been used. the goal is to catch the alternator
going out, not to monitor system voltage. my engine needs a battery or a
working alternator to keep running.
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498654#498654
________________________________________________________________________________
| From: | "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com> |
| Subject: | Re: voltage monitor |
At 01:10 PM 10/4/2020, you wrote:
>
>without any mod the 'idiot light' comes preset to warn below 13.0
>volts. in a lead acid set up this would catch the alternator soon
>after it went off line and a lead acid would have most of its charge
>left. when a lipo drops below 13 volts a lot of its charge is
>already been used.
Can you confirm that assertion from the
data offered in the three plots I've
posted?
>the goal is to catch the alternator going out, not to monitor system
>voltage. my engine needs a battery or a working alternator to keep running.
The testing I've done suggests that
there MIGHT be a bit of delay in the
LV WARN response . . . but it's minimal.
An LV condition is not a high pucker-factor
event. After the alternator
quits you can finish your cup of coffee
and sandwich, fold the map (if you still use one)
and then proceed to implement plan-b.
Conducting a lightning-fast response to the
light would have no measurable effect on
the outcome of your flight.
This is true of what ever type of battery
chemistry is on board. This is why I've
advised against numerous schemes for automatic
responses to low voltage. Such features only
add complexity that demands pre-flight testing
while failing to reduce risk.
Bob . . .
________________________________________________________________________________
| Subject: | Re: field current supplied from B lead instead of from |
main bu
| From: | "johnbright" <john_s_bright(at)yahoo.com> |
nuckolls.bob(at)aeroelect wrote:
> At 11:11 PM 10/3/2020, you wrote:
>
> If there is a fault that opens the fusible
> link, then the alternator is isolated from
> the ship's systems. While the field would
> still be energized, the resulting condition
> is internal to the alternator and not a
> threat to the rest of the airplane.
>
> If the regulator senses bus voltage through
> the breaker, then you will depress bus voltage
> by whatever drop occurs in the b-lead. Further,
> the b-terminal to field breaker lead becomes and extension
> of the bus and would need to get a fusible
> link at the b-lead.
>
> Presently, I see no particular advantage
> for doing this.
>
>
> Bob . . .
Thanks Bob.
--------
John Bright, RV-6A, at FWF, O-360
Z-101 single batt dual alt SDS EM-5-F.
john_s_bright(at)yahoo.com, Newport News, Va
https://drive.google.com/drive/folders/1u6GeZo6pmBWsKykLNVQMvu4o1VEVyP4K
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498656#498656
________________________________________________________________________________
| Subject: | Re: voltage monitor |
| From: | Charlie England <ceengland7(at)gmail.com> |
On 10/4/2020 1:27 PM, Robert L. Nuckolls, III wrote:
> At 01:10 PM 10/4/2020, you wrote:
>>
>> without any mod the 'idiot light' comes preset to warn below 13.0
>> volts. in a lead acid set up this would catch the alternator soon
>> after it went off line and a lead acid would have most of its charge
>> left. when a lipo drops below 13 volts a lot of its charge is already
>> been used.
>
> Can you confirm that assertion from the
> data offered in the three plots I've
> posted?
>
>> the goal is to catch the alternator going out, not to monitor system
>> voltage. my engine needs a battery or a working alternator to keep
>> running.
>
> The testing I've done suggests that
> there MIGHT be a bit of delay in the
> LV WARN response . . . but it's minimal.
>
> An LV condition is not a high pucker-factor
> event. After the alternator
> quits you can finish your cup of coffee
> and sandwich, fold the map (if you still use one)
> and then proceed to implement plan-b.
>
> Conducting a lightning-fast response to the
> light would have no measurable effect on
> the outcome of your flight.
>
> This is true of what ever type of battery
> chemistry is on board. This is why I've
> advised against numerous schemes for automatic
> responses to low voltage. Such features only
> add complexity that demands pre-flight testing
> while failing to reduce risk.
>
> Bob . . .
>
I think I see his point. If the 'stock' alert point is 13V, the EarthX
chart shows that to be at about the 3 AH point of the curve with total
AH capacity of about 11AH when looking at the higher discharge rates
you'd expect from an electronic injection system. Not a big deal if
there's a backup alternator, but being down roughly 1/3 before
notification could be a big deal if you're depending on battery for backup.
Charlie
--
This email has been checked for viruses by Avast antivirus software.
https://www.avast.com/antivirus
________________________________________________________________________________
| Subject: | Re: field current supplied from B lead instead of from |
main bus
| From: | "user9253" <fransew(at)gmail.com> |
Bad idea. How often do "B" leads short to ground?
The "B" lead is not going to short to ground if properly installed.
Adding an extra wire from the alternator to the instrument panel increases the
chances of a failure.
Suppose the alternator stops working for some reason.
It could be a broken belt, bad brushes, broken wire, blown "B" lead fuse.
The pilot will not know the cause. What action will the pilot take?
She might cycle the alternator field switch on and off. If the alternator still
does
not work, she might leave the switch off to conserve the battery.
I see no advantage to adding an extra wire to the engine.
--------
Joe Gores
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498657#498657
________________________________________________________________________________
| From: | "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com> |
| Subject: | Li-Ion versus LiFePO4 |
At 01:10 PM 10/4/2020, you wrote:
>
>without any mod the 'idiot light' comes preset to warn below 13.0 volts.
>in a lead acid set up this would catch the alternator soon after it went
>off line and a lead acid would have most of its charge left. when a lipo
>drops below 13 volts a lot of its charge is already been used.
Are you perhaps conflating Li-Ion with LiFePo4
chemistries?
Check out this plot https://tinyurl.com/y6o5olae
These curves are examples of the discharge characteristics
of the wildly popular lithium cells offered in the vast
majority of ads on the 'net.
As you can see, the discharge characteristics are
exceedingly different than for LiFePO4.
To achieve 100% charge you must push energy into
these cells at 4.2 volts or so. 3 cells in series
would give us a 'bus voltage' of 12.6v . . . a
tad low. Their end of service voltage of 3 volts
would power our goodies at 9V . . . waaayy too
low.
Okay, 4 cells in series gives us a bus voltage
of 16.8 volts. Yeah . . . I suppose you could
configure a system that would run happily at
that level. MOST modern avionics wouldn't care.
But your battery contactors, light bulbs and
legacy 14v accessories would care. At end of
service we would see 12v . . . just fine but
yes, it would make your existing LV warning
useless.
But are you aware of any BMS supported, engine
cranking batteries offered to the automotive
or aircraft communities that are fitted with
the Li-Ion chemistry?
LiFePo4 is a marriage made in the lab.
A 4-stack array offers full charge and end
of service voltages are quite compatible
with the lead-acid world. That's why all those supplier are
able to offer plug and play lithium upgrades
to virtually everyone . . . including those
who choose to cheat death in those
funny kites with air-thrashers on the
front.
Bob . . .
________________________________________________________________________________
| From: | Charles Kuss <chaskuss(at)yahoo.com> |
| Subject: | Re: voltage monitor |
Bob,
I suggest to view Shorai's FAQ page linked below.
https://shoraipower.com/faq
Scroll down and click on the question: Q. Can I use Lead-Acid battery char
gers or charger/tenders?
View the chart on the right side of the page. Note that at 13.0 volts, thes
e LiFe batteries have less than 40% charge left.
Charlie K
nuckolls.bob(at)aeroelectric.com> wrote:
At 01:10 PM 10/4/2020, you wrote:
--> AeroElectric-List messageposted by: "bobnoffs"
without any mod the 'idiot light' comes preset to warn below 13.0 volts.in
a lead acid set up this would catch the alternator soon after it wentoff li
ne and a lead acid would have most of its charge left. when a lipodrops bel
ow 13 volts a lot of its charge is already been used.
=C2- Can you confirm that assertion from the
=C2- data offered in the three plots I've
=C2- posted?
the goal is to catch thealternator going out, not to monitor system voltage
. my engine needs abattery or a working alternator to keep running.
=C2- The testing I've done suggests that
=C2- there MIGHT be a bit of delay in the
=C2- LV WARN response . . . but it's minimal.
=C2- An LV condition is not a high pucker-factor
=C2- event. After the alternator
=C2- quits you can finish your cup of coffee
=C2- and sandwich,=C2- fold the map (if you still use one)
=C2- and then proceed to implement plan-b.
=C2- Conducting a lightning-fast response to the
=C2- light would have no measurable effect on
=C2- the outcome of your flight.
=C2- This is true of what ever type of battery
=C2- chemistry is on board. This is why I've
=C2- advised against numerous schemes for automatic
=C2- responses to low voltage. Such features only
=C2- add complexity that demands pre-flight testing
=C2- while failing to reduce risk.
=C2- Bob . . .
________________________________________________________________________________
| From: | "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com> |
| Subject: | Re: voltage monitor |
>I think I see his point. If the 'stock' alert point is 13V, the
>EarthX chart shows that to be at about the 3 AH point of the curve
>with total AH capacity of about 11AH when looking at the higher
>discharge rates you'd expect from an electronic injection system.
>Not a big deal if there's a backup alternator, but being down
>roughly 1/3 before notification could be a big deal if you're
>depending on battery for backup.
Don't know where the 13.0 point comes from. Both
AEC and B&C have used 13.5 for a couple of decades.
But okay, let's assume 13.0
See tabular data text file. The ETX36 with a 5A
load on it will fall to 13.0 in about 40 seconds.
The image file is from plotred data of the same
test:
Kinda hard to zero in on the finer details of a
couple hour run but it shows that at 67 seconds,
the battery was down to 12.99 with an expenditure
of approx 0.1 AH
Keep in mind that voltage monitoring at
the bus is always tens of millivolts HIGHER
than battery voltage . . . with a similar
departure to the LOWER side during DISCHARGE
conditions.
So assuming one had a LV reporting system that
was not adjustable but accurate to 100 millivolts
or so at 13.0, the resulting delay between
alternator failure and annunciation is still
timely and 'wasted' energy is trivial.
Bob . . .
West Mountain Radio CBA
Test Report: YEAROLDETX36_1
Description: 4 Li-ion cells, 7.5 Ah @ 5.00A
Started At: 01/16/17 16:42:53
Starting Voltage: 13.41 V
Ending Voltage: 11.19 V
Sample Rate: 1.000
Total Time (hh:mm:ss): 2:09:53
Time (hh:mm:ss) Voltage (V) Current Temp (C)
00:00:00 13.409 0.809 0.00
00:00:01 13.409 0.809 0.00
00:00:02 13.231 4.032 0.00
00:00:03 13.184 4.773 0.00
00:00:04 13.184 4.816 0.00
00:00:05 13.165 4.968 0.00
00:00:06 13.140 4.981 0.00
00:00:07 13.135 5.002 0.00
00:00:08 13.135 5.015 0.00
00:00:09 13.135 5.011 0.00
00:00:10 13.135 4.994 0.00
00:00:11 13.130 5.011 0.00
00:00:12 13.100 5.011 0.00
00:00:13 13.100 4.994 0.00
00:00:14 13.090 5.002 0.00
00:00:15 13.085 5.002 0.00
00:00:16 13.085 4.998 0.00
00:00:17 13.085 4.998 0.00
00:00:18 13.080 4.998 0.00
00:00:19 13.085 5.011 0.00
00:00:20 13.060 4.989 0.00
00:00:21 13.065 5.002 0.00
00:00:22 13.050 5.011 0.00
00:00:23 13.045 4.981 0.00
00:00:24 13.036 5.015 0.00
00:00:25 13.035 4.989 0.00
00:00:26 13.035 5.011 0.00
00:00:27 13.035 5.006 0.00
00:00:28 13.035 4.998 0.00
00:00:29 13.035 4.998 0.00
00:00:30 13.035 5.002 0.00
00:00:31 13.031 5.011 0.00
00:00:32 13.020 4.981 0.00
00:00:33 13.016 5.002 0.00
00:00:34 13.021 5.006 0.00
00:00:35 13.006 4.994 0.00
00:00:36 13.006 4.994 0.00
00:00:37 12.991 5.011 0.00
00:00:38 12.986 4.994 0.00
00:00:39 12.986 5.015 0.00
00:00:40 12.986 4.998 0.00
________________________________________________________________________________
| From: | "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com> |
| Subject: | Re: voltage monitor |
At 02:18 PM 10/4/2020, you wrote:
>Bob,
>I suggest to view Shorai's FAQ page linked below.
>
>https://shoraipower.com/faq
>
>Scroll down and click on the question: Q. Can I use Lead-Acid
>battery chargers or charger/tenders?
>
>View the chart on the right side of the page. Note that at 13.0
>volts, these LiFe batteries have less than 40% charge left.
That's an open circuit, no-load voltage that speaks
to state of charge. That's not a milestone voltage
for a fully charged battery under load.
Two completely different conditions
Bob . . .
________________________________________________________________________________
| Subject: | Re: voltage monitor |
| From: | "bobnoffs" <icubob(at)gmail.com> |
hi all,
according to the graph posted bob is right about the very small current drained.
this is not at all how earthx describes their batteries. earthx recommends that
low voltage monitors light up below 13.5 volts.
on the b and c web site they sell an over/under voltage sensor model bc207. the
low voltage light trips at 12.5 volts according to their description.
everything i have learned about the lipo batteries has said they hold their voltage
while discharging. i have always seen a much larger % drop advertised.time
for me to call earthx.
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498666#498666
________________________________________________________________________________
| Subject: | Re: ADS-B and Transponder antenna design... |
| From: | "andymeyer" <meyerkc135(at)gmail.com> |
I simply carefully spliced the Coax. I tried a 1GHz mux with and without a terminating
resistor and didn't find any better real world performance and it was
harder to package. That's one of the reasons I'd like to find out about the analyzer
performance of these antennas.
Drop me an email as to where to send them. I assume you've got an analyzer? Let
me know where to send it. I'd much rather have them dialed in at 978 as weather
reception range is most important. If I can see 1090 traffic at 5 miles, I'm
happy, but if I can only get 978 towers at 30 or 40 miles... :(
I put my stratux back out of the way as well - talks great to my IFD540 via serial.
I've only got about 3 feet of coax, but around the house, I had these hooked
up to about 10 feet for testing. I'm flying with the Slim-jim, but recently
found a better hiding place to try to di-pole if it'll fit in my spar well without
sacrificing performance. I have 3 turns of coax at the base of the antenna
for a BalUn.
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498667#498667
________________________________________________________________________________
| From: | Charlie England <ceengland7(at)gmail.com> |
| Subject: | Re: voltage monitor |
On Sun, Oct 4, 2020 at 4:28 PM Robert L. Nuckolls, III <
nuckolls.bob(at)aeroelectric.com> wrote:
> I think I see his point. If the 'stock' alert point is 13V, the EarthX
> chart shows that to be at about the 3 AH point of the curve with total AH
> capacity of about 11AH when looking at the higher discharge rates you'd
> expect from an electronic injection system. Not a big deal if there's a
> backup alternator, but being down roughly 1/3 before notification could be
> a big deal if you're depending on battery for backup.
>
>
> Don't know where the 13.0 point comes from. Both
> AEC and B&C have used 13.5 for a couple of decades.
>
> But okay, let's assume 13.0
>
> See tabular data text file. The ETX36 with a 5A
> load on it will fall to 13.0 in about 40 seconds.
> The image file is from plotred data of the same
> test:
>
> Kinda hard to zero in on the finer details of a
> couple hour run but it shows that at 67 seconds,
> the battery was down to 12.99 with an expenditure
> of approx 0.1 AH
>
> Keep in mind that voltage monitoring at
> the bus is always tens of millivolts HIGHER
> than battery voltage . . . with a similar
> departure to the LOWER side during DISCHARGE
> conditions.
>
> So assuming one had a LV reporting system that
> was not adjustable but accurate to 100 millivolts
> or so at 13.0, the resulting delay between
> alternator failure and annunciation is still
> timely and 'wasted' energy is trivial.
>
>
> Bob . . .
>
I think he's using the EarthX PC680 relacement battery. I used EarthX's
chart for their PC680 replacement, here:
https://earthxbatteries.com/earthx_manual.pdf
and assumed ~12-14 A load, which is typical for full electronic engine
control with electronic injection. According to EarthX the 680 replacement
hovers around 13 V until around 3 AH has been depleted.
You'd know a lot better than me where the LoVolts setpoint is with B&C
stuff; that's why I said 'if'. :-)
Charlie
________________________________________________________________________________
| From: | Charlie England <ceengland7(at)gmail.com> |
| Subject: | Re: ADS-B and Transponder antenna design... |
Sounds affordable to me. I don't have an analyzer now, but I've been
planning to purchase one. This will motivate me. :-)
I'll send my address direct to your email address.
Thanks!
Charlie
On Sun, Oct 4, 2020 at 5:12 PM andymeyer wrote:
> >
>
> I simply carefully spliced the Coax. I tried a 1GHz mux with and without a
> terminating resistor and didn't find any better real world performance and
> it was harder to package. That's one of the reasons I'd like to find out
> about the analyzer performance of these antennas.
>
> Drop me an email as to where to send them. I assume you've got an
> analyzer? Let me know where to send it. I'd much rather have them dialed in
> at 978 as weather reception range is most important. If I can see 1090
> traffic at 5 miles, I'm happy, but if I can only get 978 towers at 30 or 40
> miles... :(
>
> I put my stratux back out of the way as well - talks great to my IFD540
> via serial. I've only got about 3 feet of coax, but around the house, I had
> these hooked up to about 10 feet for testing. I'm flying with the Slim-jim,
> but recently found a better hiding place to try to di-pole if it'll fit in
> my spar well without sacrificing performance. I have 3 turns of coax at the
> base of the antenna for a BalUn.
>
>
> Read this topic online here:
>
> http://forums.matronics.com/viewtopic.php?p=498667#498667
>
>
________________________________________________________________________________
| From: | "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com> |
| Subject: | Re: voltage monitor |
At 04:50 PM 10/4/2020, you wrote:
>
>hi all,
> according to the graph posted bob is right about the very small
> current drained.
>this is not at all how earthx describes their batteries.
Can you point us to the download for
information that gives you concern?
>earthx recommends that low voltage monitors light up below 13.5 volts.
B&C and I both have promoted that lv setpoint
value for decades . . .
> on the b and c web site they sell an over/under voltage sensor
> model bc207. the low voltage light trips at 12.5 volts according to
> their description.
>
That device was originally crafted
for ultralights about 30 years ago.
In fact, it was the first, stand-alone
monitor device produced there.
It was never intended for installation
in 'real' airplanes. I really wish
they didn't sell that any more but
I think Aircraft Spruce shows it in
their catalog. NOT RECOMMENDED FOR
NEW DESIGN.
> everything i have learned about the lipo batteries has said they
> hold their voltage while discharging.
And in what way does the data I've posted
argue with that?
The AeroVoltz plot shows a working range
on the order of 13.2 to 12.5 volts.
Miady 13.2 to about 12.0
EarthX from 13.2 to 12.5
Where are you going to find anything
flatter for a discharge curve? All three
deliver power within a 5% or smaller
window.
I have always seen a much larger % drop advertised.time for me to call earthx.
. . . and ask what? Help me understand
your question. Before you seek verbal
guidance, let us examine data-in-print
and data-measured so that disconnects can
be clearly articulated. I'd be happy
to call them myself if there are real
points of contention.
I've talked to both EarthX and Shorai
numerous times but a considerable time
ago . . . wouldn't mind renewing some
contacts.
Bob . . .
________________________________________________________________________________
| From: | Ken Ryan <keninalaska(at)gmail.com> |
| Subject: | Re: voltage monitor |
From: Technical Manual for Model No. LR3D-14 and LR3D-28 Linear
RegulatorWith Over-Voltage Protection, Low-Voltage Sensing, And
Field-Adjustable Charging Voltage
"The LV warning light will begin to flash when the voltage sensed at
terminal 3 drops to approximately 12.7V and below"
Disregard if this is not relevant to this discussion.
On Sun, Oct 4, 2020 at 2:26 PM Charlie England wrote:
>
>
> On Sun, Oct 4, 2020 at 4:28 PM Robert L. Nuckolls, III <
> nuckolls.bob(at)aeroelectric.com> wrote:
>
>> I think I see his point. If the 'stock' alert point is 13V, the EarthX
>> chart shows that to be at about the 3 AH point of the curve with total AH
>> capacity of about 11AH when looking at the higher discharge rates you'd
>> expect from an electronic injection system. Not a big deal if there's a
>> backup alternator, but being down roughly 1/3 before notification could be
>> a big deal if you're depending on battery for backup.
>>
>>
>> Don't know where the 13.0 point comes from. Both
>> AEC and B&C have used 13.5 for a couple of decades.
>>
>> But okay, let's assume 13.0
>>
>> See tabular data text file. The ETX36 with a 5A
>> load on it will fall to 13.0 in about 40 seconds.
>> The image file is from plotred data of the same
>> test:
>>
>> Kinda hard to zero in on the finer details of a
>> couple hour run but it shows that at 67 seconds,
>> the battery was down to 12.99 with an expenditure
>> of approx 0.1 AH
>>
>> Keep in mind that voltage monitoring at
>> the bus is always tens of millivolts HIGHER
>> than battery voltage . . . with a similar
>> departure to the LOWER side during DISCHARGE
>> conditions.
>>
>> So assuming one had a LV reporting system that
>> was not adjustable but accurate to 100 millivolts
>> or so at 13.0, the resulting delay between
>> alternator failure and annunciation is still
>> timely and 'wasted' energy is trivial.
>>
>>
>>
>>
>>
>> Bob . . .
>>
> I think he's using the EarthX PC680 relacement battery. I used EarthX's
> chart for their PC680 replacement, here:
> https://earthxbatteries.com/earthx_manual.pdf
> and assumed ~12-14 A load, which is typical for full electronic engine
> control with electronic injection. According to EarthX the 680 replacement
> hovers around 13 V until around 3 AH has been depleted.
>
> You'd know a lot better than me where the LoVolts setpoint is with B&C
> stuff; that's why I said 'if'. :-)
>
> Charlie
>
>
________________________________________________________________________________
| Subject: | Re: voltage monitor |
| From: | "bobnoffs" <icubob(at)gmail.com> |
the link charlie posted shows a graph i am used to seeing with the earthx. i take
this graph to mean i will give up 3ah of battery by using 13.0 as a setpoint
vs. 13.5 volts. i have no second alternator so it is important to me to know
asap when i have only battery power to keep the engine running.
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498676#498676
________________________________________________________________________________
| From: | "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com> |
| Subject: | Re: voltage monitor |
New post
Posted: Sun Oct 04, 2020 4:51 pm Post subject: voltage monitor
<http://forums.matronics.com/posting.php?mode=quote&p=498671&sid=6781a385e9dbba117a35c9138433dbef>
Reply with quote
----------
From: Technical Manual for Model No. LR3D-14 and LR3D-28 Linear
RegulatorWith Over-Voltage Protection, Low-Voltage Sensing, And
Field-Adjustable Charging Voltage
"The LV warning light will begin to flash when the voltage sensed at
terminal 3 drops to approximately 12.7V and below"
Disregard if this is not relevant to this discussion.
It is very relevant. Thank you.
This is news to me but I've not been directly
involved or plugged in to B&C design decisions
for some years
With that in mind, and given the number and
variety of programs I've worked it seemed
prudent to verify the hip-pocket archives.
Dug out my AEC9005 drawings and the setpoint
was 13.0 volts. All the data I have on early
LR3 series regulators suggest that 12.7
has been the setpoint from day one.
Just for grins, I plotted Time-to-12.7v
for four batteries. An AeroVolts, an
exemplar EarthX, a Miady 16AH device
and just for the heck of it, a fresh
Enersy 16AH battery. Plots attached.
I've also included a test for a A123,
26650 cell where I deduce that a 4x4
array of these cells in a 14v system
battery would fall below 13.5 volts
in about 30 seconds.
I suggest these plots show that a 13.5
volt lo volts warning threshold would
be suited to all chemistries. Note that
the SVLA falls like a rock to well under
12.7 when it looses alternator support . . .
well, it IS a 12v battery while LiFePO4
devices are generally considered to be
13.2 volt batteries (although AeroVolts
labels theirs as a 12V while the plots
show that it has the highest alternator-
out voltage of the lot).
Hence, I stand better informed and
agree that the legacy LR3 configuration
is unsuitable for lithium battery management
without (easy to do) modification as
is our AEC9005 LV Warning Module.
Sorry for ignoring you the past day or
so. Been wrestling with some issues
in a car I've got sold . . . along
with a recalcitrant wifi router.
Ever see the look on the fact of a couple
teenagers when you tell them, "the
wifi is down"?
Bob . . .
________________________________________________________________________________
| From: | "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com> |
| Subject: | Re: voltage monitor |
At 05:52 AM 10/5/2020, you wrote:
>
>the link charlie posted shows a graph i am used to seeing with the
>earthx. i take this graph to mean i will give up 3ah of battery by
>using 13.0 as a setpoint vs. 13.5 volts. i have no second
>alternator so it is important to me to know asap when i have only
>battery power to keep the engine running.
13.5 is cool . . .
Bob . . .
________________________________________________________________________________
| Subject: | Peer review, Z16 Rotax engine, Ducati Regulator |
| From: | "velletazjp" <velletazjp(at)gmail.com> |
Hi everybody
Many thanks for all the help I received when I designed the electric system for
my Jodel's friend.
The plane is now airworthy and so far everything is working like a charm.
I now start helping an other fellow aviator who'w building an Aero101. He is a
professional carpenter and the airplane is a true beauty but electicity is not
he's strong skill.
I designed a very simple electric system, 90% inspired by bob's Z16.
Once again Bob [and all the other members of this forum], thanks for all the knowledge
you're spreading...
My friend had 2 requirement that forced me to differ from Bob's design :
- he doesn't want to use a battery relay (I personally don't neither the load
on the bus is less than 5Amp and a simple switch can handle that kind of current)
- he bought a rather expensive start key (see installation manual attached) that
permits to turn ON the battery, select Ignition 1 and/or 2, and activate the
stater. He don't want any other switches (unless safety mandates).
Initially, the supplier doesn't advised to install a OV disconnect relay, but I
used Bob's design to adapt one on his airplane.
Please let me know if you see any flaws or improvement possible.
Many thanks
--------
2020 contribution paid
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498689#498689
Attachments:
http://forums.matronics.com//files/loraviacom_regulateur_912_ducati_395.pdf
http://forums.matronics.com//files/schema_electrique_objet_176.pdf
http://forums.matronics.com//files/120883263_336407514294840_7206115166821084811_n_649.jpg
________________________________________________________________________________
| From: | "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com> |
| Subject: | Re: Peer review, Z16 Rotax engine, Ducati Regulator |
>
>Initially, the supplier doesn't advised to install a OV disconnect
>relay, but I used Bob's design to adapt one on his airplane.
>
>
>Please let me know if you see any flaws or improvement possible.
The crowbar ov module wires ACROSS the
alternator disconnect relay DOWNSTREAM
of the 5A breaker. See figure Z16.
Bob . . .
________________________________________________________________________________
| Subject: | Re: Peer review, Z16 Rotax engine, Ducati Regulator |
| From: | "user9253" <fransew(at)gmail.com> |
The crowbar module will short out the battery.
There is a long, always-hot wire connected between the battery and
terminal 1 of that expensive switch. In an accident, that wire could make
sparks and start a fire. A battery contactor can shut off power close to the battery.
--------
Joe Gores
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498692#498692
________________________________________________________________________________
| From: | David Saylor <saylor.dave(at)gmail.com> |
| Subject: | Breaker then pump failure |
I just had the Tyco switch/breaker for my boost pump fail. It made a bad
smell, then became intermittent, then failed completely in the span of a
few minutes. I replaced it with the same make and model.
2.5 flight hours later my boost pump failed. The new breaker never
tripped. The pump just stopped running. The pump circuit has no
resistance and I get full bus voltage at the pump, even with the pump still
connected. So it's open inside. The new switch is working fine.
The pump is from Airflow Performance. They're common in RVs. The pump and
the switch had almost 2000 airframe hours since installed. I use it for
take-off and landing, so the powered time is a fraction of the total time.
The airplane had been sitting for almost a year, then flown about 15 hours
in the last two weeks.
Does anyone have an understanding of any relationship between these two
failures? They seem too similar to be completely unrelated. My guess is
that a faulty pump somehow overloaded a faulty breaker, then failed
completely. I couldn't say that I noticed any particular fuel pressure
issues before the failure. Everything was in the green.
Thoughts?
________________________________________________________________________________
| Subject: | Engine Monitor P-lead question |
| From: | "farmrjohn" <faithvineyard(at)yahoo.com> |
I'm installing an Electronics International CGR-30P engine monitor. For the tach
function they have two leads that connect to the left and right P-lead on the
ignition switch which are not shielded. The P-leads from the mags to the switch
are shielded. Will this be an issue? Can those two leads be included in
a wire bundle or should they have their on run away from other wires? Thanks,
John
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498693#498693
________________________________________________________________________________
| Subject: | AC 43.13-1B circuit protection recommendations |
| From: | "Tailwind1" <timmikus38(at)gmail.com> |
Looking at table 11-3 in the 43.13, the table shows lower amperage recommendations
for fuses versus circuit breakers in many cases. Bob has shown us how much
quicker a fuse operates versus a CB so logic seems to suggest a higher fuse rating
versus a CB. What am I missing?
Thanks!
--------
Flying Sonerai II with A80 Continental. Wittman W10 Tailwind under construction,
O360, dual LSE electronic ignition, airframe complete and covered, engine hung,
cowl built. Working on electrical, instrumentation, and other details.
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498695#498695
________________________________________________________________________________
| Subject: | Re: antenna analyzer? Antennas |
| From: | "hairy_kiwi" <hamish.mead(at)gmail.com> |
Hi Group,
Long time lurker here. Hopefully, as the OP made the title rather broadband ;)
a general discussion on aviation / aircraft antenna design and using antenna
analyzers for verifying experiments is welcome here. Otherwise, apologies for
further dragging the discussion away from the otherwise fascinating DDRR antenna
design...
I recently bought a Rig Expert AA 230 ZOOM analyzer, primarily for helping to diagnose
faults in antenna coax while doing the odd bit of experimental aircraft
rewiring. Its been a great tool for quickly and easily finding poorly made BNC
terminations for example (wire disconnected from center pin in a poorly made,
screw-together style BNC connector) and checking SWR in a comm antenna epoxied
into a composite aircraft is still acceptable years after construction.
As for using an analyzer for antenna design, the interesting, very detailed paper
Eric posted a link to, titled 'Airborne VHF Printed Monopole Antenna for Platform
Constrained Applications' looks like it could be a fun design to experiment
with - possibly for installing inside the fin of the Kitfox I'm going to
be building - especially as the ground plane is incorporated in the same plane
as the antenna.
I have a basic understanding of antenna design, but its very basic - and with a
few antenna issues and projects on the go, I'd be very interested in furthering
my knowledge and doing some experimenting with the aid of the analyzer. What
would be useful are some links to modern literature on aviation/aircraft antenna
design - many thanks Eric for your post!
I had a browse through the ARRL Antenna Book which is a great tome of info, however
the vast majority of that material is aimed at ground station antennas. So
I'm still unclear on such things as by how much proximity to The Earth the SWR
of an aircraft (comm) antennas is affected. Maybe a flight vs ground test comparison
using an analyzer might be interesting to conduct, even if it proves
'no significant difference', particularly for 1/2 wave dipoles fitted internally
to composite aircraft.
I've found some other recently published and interesting material with test results
on (ground based) 2m 1/2 wave dipole designs that might be worth experimenting
/ adapting for aircraft use, but will save that for another post if there's
interest.
Cheers,
Jim
Hamish 'Jim' Mead
Ledbury, UK
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498696#498696
________________________________________________________________________________
| Subject: | Re: AC 43.13-1B circuit protection recommendations |
| From: | "johnbright" <john_s_bright(at)yahoo.com> |
Here's an image of Table 11-3.
--------
John Bright, RV-6A, at FWF, O-360
Z-101 single batt dual alt SDS EM-5-F.
john_s_bright(at)yahoo.com, Newport News, Va
https://drive.google.com/drive/folders/1u6GeZo6pmBWsKykLNVQMvu4o1VEVyP4K
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498698#498698
Attachments:
http://forums.matronics.com//files/ac_4313_1b_table_11_3_301.jpg
________________________________________________________________________________
| From: | "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com> |
| Subject: | Re: Breaker then pump failure |
At 10:14 PM 10/7/2020, you wrote:
I just had the Tyco switch/breaker for my boost pump fail. It made a
bad smell, then became intermittent, then failed completely in the
span of a few minutes. I replaced it with the same make and model.
Do you still have the carcass? I'd like to have
it . . .
2.5 flight hours later my boost pump failed. The new breaker never
tripped. The pump just stopped running. The pump circuit has no
resistance and I get full bus voltage at the pump, even with the pump
still connected. So it's open inside. The new switch is working fine.
Agreed
The pump is from Airflow Performance. They're common in RVs. The
pump and the switch had almost 2000 airframe hours since
installed. I use it for take-off and landing, so the powered time is
a fraction of the total time.
I think that pump has a PM motor with brushes.
It's not uncommon for such devices to suffer
as much degradation from idle time as from
service life. In any case, I'm betting that
the pathway through the armature is open for
reasons we do not yet know. Does the pump
have a 'cure' value? If not, I'd be pleased
to do a autopsy on it too.
The airplane had been sitting for almost a year, then flown about 15
hours in the last two weeks.
Does anyone have an understanding of any relationship between these
two failures? They seem too similar to be completely unrelated. My
guess is that a faulty pump somehow overloaded a faulty breaker, then
failed completely. I couldn't say that I noticed any particular fuel
pressure issues before the failure. Everything was in the green.
Thoughts?
I suspect they are not related. In theory, you
can't damage a breaker by 'overloading' it . . . after
all, its core mission in life is to protect from
the consequences of such conditions including self
destruction. Getting a look at the carcasses might
offer more clues.
Bob . . .
________________________________________________________________________________
| From: | "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com> |
| Subject: | Re: AC 43.13-1B circuit protection recommendations |
At 07:25 AM 10/8/2020, you wrote:
>
>Looking at table 11-3 in the 43.13, the table shows lower amperage
>recommendations for fuses versus circuit breakers in many cases. Bob
>has shown us how much quicker a fuse operates versus a CB so logic
>seems to suggest a higher fuse rating versus a CB. What am I missing?
I haven't a clue. I questioned this in the critical review
we submitted through EAA many moons ago but the item
was never modified or explained. If I were to WAG this
one, the writer may have been comparing performance
of fuses vs. magnetic breakers. In this case the breakers
are faster than fuses . . . but TERRIBLE choices for
general use in light aircraft power distribution.
If one simply compares the fusing dynamics of the
fuses vs. thermal breakers, the AC43-13 suggestion
doesn't make sense at all.
Actually, there's no reason to up-size the rating
of protection based on the technology. Breaker and
wire ratings are based on effects of the wire's
natural self-heating and is concerned only with
the wire's INSULATION. Long term heating effects
are a function of NORMAL current flows, voltage
drops in wire and temperature of the environment
which includes both the airframe and adjacent
wires in bundles.
That's a real snarl of snakes to unwind for
all but design goals of the most pedantic
of program managers. For our purposes, the
rule of thumb is, "if in doubt, up-size the
wire and protection to the next step."
Moving up can only reduce effects of NORMAL
heating. Consider that 99% of all
breaker/fuse events are caused by ABNORMAL
current well above the NORMAL . . . like
hard shorts or catastrophic failures in
appliances. We are virtually never victims
of a failed insulation condition . . .
The short answer is: Your common sense questioning
of the AC43-13 assertion is valid. Ignoring
it based on your own study of PROPERTIES
OF MATERIALS is not a risky thing to do.
Bob . . .
________________________________________________________________________________
| From: | Charlie England <ceengland7(at)gmail.com> |
| Subject: | Re: Breaker then pump failure |
On Thu, Oct 8, 2020 at 11:42 AM Robert L. Nuckolls, III <
nuckolls.bob(at)aeroelectric.com> wrote:
> At 10:14 PM 10/7/2020, you wrote:
> snipped .
>
> 2.5 flight hours later my boost pump failed. The new breaker never
> tripped. The pump just stopped running. The pump circuit has no
> resistance and I get full bus voltage at the pump, even with the pump still
> connected. So it's open inside. The new switch is working fine.
>
> Agreed
>
>
> The pump is from Airflow Performance. They're common in RVs. The pump
> and the switch had almost 2000 airframe hours since installed. I use it
> for take-off and landing, so the powered time is a fraction of the total
> time.
>
> I think that pump has a PM motor with brushes.
> It's not uncommon for such devices to suffer
> as much degradation from idle time as from
> service life. In any case, I'm betting that
> the pathway through the armature is open for
> reasons we do not yet know. Does the pump
> have a 'cure' value? If not, I'd be pleased
> to do a autopsy on it too.
>
> The airplane had been sitting for almost a year, then flown about 15 hours
> in the last two weeks.
>
>
> Does anyone have an understanding of any relationship between these two
> failures? They seem too similar to be completely unrelated. My guess is
> that a faulty pump somehow overloaded a faulty breaker, then failed
> completely. I couldn't say that I noticed any particular fuel pressure
> issues before the failure. Everything was in the green.
>
> Thoughts?
>
> I suspect they are not related. In theory, you
> can't damage a breaker by 'overloading' it . . . after
> all, its core mission in life is to protect from
> the consequences of such conditions including self
> destruction. Getting a look at the carcasses might
> offer more clues.
>
>
> Bob . . .
>
The core pump in the AFP pumps I'm familiar with are Airtex brand in-line
fuel injection pumps, available online for between $60 & $100. Like this?
https://www.amazon.com/Airtex-E2000-Electric-Fuel-Pump/dp/B000C1KHJG/ref=sr_1_7?dchild=1&keywords=airtex+fep2000+fuel+pump&qid=1602176199&sr=8-7
Either E2000 or FEP2000. Note that the hose barb shown on one end screws
off, allowing various other adapters.
If the OP wishes, I can measure my FEP2000 to verify dimensions.
Charlie
________________________________________________________________________________
| From: | "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com> |
| Subject: | Re: Breaker then pump failure |
>
>The core pump in the AFP pumps I'm familiar with
>are Airtex brand in-line fuel injection pumps,
>available online for between $60 & $100. Like this?
>https://www.amazon.com/Airtex-E2000-Electric-Fuel-Pump/dp/B000C1KHJG/
ref=sr_1_7?dchild=1&keywords=airtex+fep2000+fuel+pump&qid=1602176199
&sr=8-7
>Either E2000 or FEP2000. Note that the hose barb
>shown on one end screws off, allowing various other adapters.
>If the OP wishes, I can measure my FEP2000=C2 to verify dimensions.=C2
>
>Charlie
Interesting. The specs speak to commutators and
brushes. I also deduce that this style of pump
is used on a lot of medium pressure EFI systems.
It will be interesting to see if we can open
Dave's dead one for a closer looksee.
Bob . . .
________________________________________________________________________________
| From: | "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com> |
| Subject: | Re: antenna analyzer? Antennas |
At 07:53 AM 10/8/2020, you wrote:
Hi Group,
Long time lurker here. Hopefully, as the OP made the
title rather broadband ;) a general discussion on
aviation / aircraft antenna design and using antenna
analyzers for verifying experiments is welcome here.
Otherwise, apologies for further dragging the discussion
away from the otherwise fascinating DDRR antenna design...
I think we're done with the DDRR for now.
It seems unlikely that a satisfactory fabrication
technique for increasing bandwidth will be
forthcoming.
The antenna gurus all seem to agree that the
perfect triad of size, efficency and bandwidth
is like finding a way to to resolve cube roots
with a pencil/paper. Unfortunately for the DDRR, the
primary driver (size) put the kibosh on at least
one of the other two, mainly bandwidth.
I recently bought a Rig Expert AA 230 ZOOM analyzer,
I've seen those tools on the web . . . they seem
widely utilized with satisfaction.
As for using an analyzer for antenna design, the interesting, very
detailed paper Eric posted a link to, titled 'Airborne VHF Printed
Monopole Antenna for Platform Constrained Applications' looks like it
could be a fun design to experiment with - possibly for installing
inside the fin of the Kitfox I'm going to be building - especially as
the ground plane is incorporated in the same plane as the antenna.
On page 2 we find this statement, "The major constraint
in designing an airborne printed monopole antenna
in VHF/UHF band is achieving compactness and wide
bandwidth simultaneously, along with sufficient gain."
This assertion pays homage to the SEB triad with
the operative phrase being "sufficient gain".
Figure 6 shows that a very satisfactory bandwidth
was achieved while Figure 7 shows the sacrifices in
efficiency wherein the two test conditions demonstrate
losses of 6 to 15 dB over the bandwidth of interest.
That's 1/4 to 1/32 of the radiated energy offered
by the reference antenna. Sufficient? Maybe. Recall
that all VHF comm is line of sight . . . you don't
talk past the horizon and in any case, it's almost
never necessary to have conversation beyond 50
miles or so. So maybe, just maybe an antenna with
that efficiency profile would provide satisfactory
communications for some if not all builders.
The proof is in the pudding (I prefer vanilla-tapicoa
myself).
I had a browse through the ARRL Antenna Book which is a great tome of
info, however the vast majority of that material is aimed at ground
station antennas. So I'm still unclear on such things as by how much
proximity to The Earth the SWR of an aircraft (comm) antennas is affected.
It's not . . . but proximity to conducting aircraft
structure (artificial ground) is. So ground vs.
airborne testing is probably not useful.
The flight test of intense interest would be with
perhaps a software driven receiver (SDR) on board
where you would fly 360s out 40 miles or so from a handy
ground station and plot comparative azimuth measurements of your
test antenna with respect to a more conventional vhf comm
whip. We used to do a good bit of this type testing
at Hawer-Beech . . . which requires another previously
expensive but now not so much spectrum analyzer/receiver
with signal strength display.
I've found some other recently published and interesting material
with test results on (ground based) 2m 1/2 wave dipole designs that
might be worth experimenting / adapting for aircraft use, but will
save that for another post if there's interest.
Let's look at them . . .
Bob . . .
________________________________________________________________________________
| From: | "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com> |
| Subject: | Some new battery chemistries on the horizon? |
While lithium products are the fair-haired
children in the portable energy storage
sandbox, there's a couple of interesting
technologies being spun-up in the EV
world:
https://tinyurl.com/yy8cqwbe
https://tinyurl.com/y2ptgrjz
These MIGHT find application in aviation
and consumer products with some dispatch.
Contemporary EV batteries evolved up
from the smaller, less energetic
consumer products. These new kids
on the block will enjoy immediate
success and large scale production in
a particularly battery-intensive market:
EVs.
It seems likely that they could 'spill
out' into the consumer markets quickly.
It's intuitively easier to evolve-
down a product that's already enjoying
high volume successes.
We'll have to wait and see . . .
Bob . . .
________________________________________________________________________________
| Subject: | Re: Breaker then pump failure |
| From: | Kelly McMullen <kellym(at)aviating.com> |
I believe Airflow Performance with do a rebuild at reasonable price.
Might not get the diagnosis desired, but could be cheaper than alternatives.
On 10/8/2020 12:08 PM, Robert L. Nuckolls, III wrote:
>>
>> The core pump in the AFP pumps I'm familiar with are Airtex brand
>> in-line fuel injection pumps, available online for between $60 & $100.
>> Like this?
>> https://www.amazon.com/Airtex-E2000-Electric-Fuel-Pump/dp/B000C1KHJG/ref=sr_1_7?dchild=1&keywords=airtex+fep2000+fuel+pump&qid=1602176199&sr=8-7
>>
>> Either E2000 or FEP2000. Note that the hose barb shown on one end
>> screws off, allowing various other adapters.
>> If the OP wishes, I can measure my FEP2000 to verify dimensions.
>>
>> Charlie
>
> Interesting. The specs speak to commutators and
> brushes. I also deduce that this style of pump
> is used on a lot of medium pressure EFI systems.
>
> It will be interesting to see if we can open
> Dave's dead one for a closer looksee.
>
>
> Bob . . .
>
________________________________________________________________________________
| From: | David Saylor <saylor.dave(at)gmail.com> |
| Subject: | Re: Breaker then pump failure |
Charlie wrote:
> The core pump in the AFP pumps I'm familiar with are Airtex brand in-line
> fuel injection pumps, available online for between $60 & $100. Like this?
>
> https://www.amazon.com/Airtex-E2000-Electric-Fuel-Pump/dp/B000C1KHJG/ref=sr_1_7?dchild=1&keywords=airtex+fep2000+fuel+pump&qid=1602176199&sr=8-7
> Either E2000 or FEP2000. Note that the hose barb shown on one end screws
> off, allowing various other adapters.
> If the OP wishes, I can measure my FEP2000 to verify dimensions.
>
> Charlie
>
Between Amazon and the Airtex web site, my pump seems most like an E8445.
There are a lot of models and I haven't ID'd it exactly. The E2000 looks
the same but it puts out almost three times the pressure that I see.
I sent my pump assy to AFP where they replaced the pump for a little more
than the Amazon price. They did a great job, shipping back the repaired
assembly within hours of receiving it.
Bob, if I get the old pump back, I'll send it to you along with the breaker.
BTW, I just became aware of an AD from 2008 to replace this type of CB
switch in Beechcraft products.
--Dave
________________________________________________________________________________
| From: | David Saylor <saylor.dave(at)gmail.com> |
| Subject: | Re: Breaker then pump failure |
Bob wrote:
> Do you still have the carcass? I'd like to have
> it . . .
>
Here's a picture for now. I broke in before I sent my initial message.
Charred remains to follow.
I'm almost certain that the braid broke when I opened it.
The little barbequed U spring is missing most of its legs. I wonder if one
broke off and shorted something to start the failure.
The switch had lost it's "snap" after it quit.
Here's a picture from a Beech website.
These are serviceable and
very similar to what I have.
[image: image.png]
________________________________________________________________________________
| Subject: | Re: Breaker then pump failure |
| From: | Finn Lassen <finn.usa(at)gmail.com> |
NO. The braid is the weak point.
Where it's spot welded to the contact it's hardened. As the switch is
turned on/off the braid flexes. Same as what happens when you have a
soldered flexible wire that is not supported at a point where the wire
is still flexible (after the solder penetration).
It's a glaring design failure. Easily fixed by two molded pins in the
plastic housing that would provide support where braid is again
flexible. Why they haven't done that after the extensive failure history
is beyond me.
Do not use these switch/breakers for flight-critical items!
Finn
On 10/9/2020 1:50 AM, David Saylor wrote:
>
> Bob wrote:
>
> Do you still have the carcass? I'd like to have
> it . . .
>
>
> Here's a picture for now. I broke in before I sent my initial
> message. Charred remains to follow.
>
> I'm almost certain that the braid broke when I opened it.
>
> The little barbequed U spring is missing most of its legs. I wonder
> if one broke off and shorted something to start the failure.
>
> The switch had lost it's "snap" after it quit.
>
> Here's a picture from a Beech website.
> These are
> serviceable and very similar to what I have.
>
>
---
This email has been checked for viruses by Avast antivirus software.
https://www.avast.com/antivirus
________________________________________________________________________________
| From: | "Eric Page" <edpav8r(at)yahoo.com> |
Hi Bob,
I'm building a Kitfox that will probably use an auto-based engine conversion.
I like the look of your Z102 architecture for its redundancy in engine electrical
supply, as well as the auxiliary bus for pre-flight ground activities. But,
I have a couple of questions:
1. Am I correct in my understanding that:
a) the auxiliary battery is normally paralleled with the main battery during engine
start *and* during normal operation (bus voltage >13V) so that it can be
recharged by the alternator?
b) the auxiliary battery will be isolated to engine-related functions only, if
the bus falls below 13V?
2. The Z102 schematic shows a START CMD signal from the push-to-start switch to
an AEC90XX Aux Battery Management Module (ABMM). The only thing like this that
I can find is your AEC9005 series of Low Voltage Warning and ABMM devices.
However, the AEC9005 schematic in this document...
http://www.aeroelectric.com/DIY/LV_Warn_Fab_and_Install.pdf
...does not include an input for the START CMD signal. Is there another ABMM design
on the drawing board, or does Z102 contemplate an iteration of AEC9005 with
the addition of the START CMD facility? If the latter, then is it safe to
assume that START CMD is simply a gate drive signal to the FET, diode isolated
from the comparator output?
3. On the AEC9005 schematic linked above, what is the purpose of Zener diode Z118?
Is it to protect the FET against excessive V(d-s) in case the contactor's
flyback diode fails to perform, or is missing?
Many thanks!
Eric
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498724#498724
________________________________________________________________________________
| From: | "Argonaut36" <fmlibrino(at)msn.com> |
I would like to replace my wire stripper that has recently failed. I am interested
in a tool that can strip wires in the range 10-22 AWG and possibly smaller
wires as the ones sometimes used in avionics and instruments. I would buy 2
strippers, if necessary.
Could somebody make a recommendation for a good quality, reliable tool?
Thanks
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498730#498730
________________________________________________________________________________
| Subject: | Re: Wire stripper |
| From: | Robert Borger <rlborger(at)mac.com> |
Argonaut36,
The Ideal Stripmaster 45-097 from B&C (bandc.com) is an excellent wire stripper.
As received it strips wire from 16-26 AWG. The stripper blades are replaceable
and an adjustable wire stop is available for it. Im sure similar strippers
are available at other electronics site.
Blue skies & tailwinds,
Bob Borger
Europa XS Tri, Rotax 914, Airmaster C/S Prop.
Little Toot Sport Biplane, Lycoming Thunderbolt AEIO-320 EXP, Hercules Prop.
3705 Lynchburg Dr.
Corinth, TX 76208-5331
Cel: 817-992-1117
rlborger(at)mac.com
> On Oct 9, 2020, at 6:33 PM, Argonaut36 wrote:
>
>
> I would like to replace my wire stripper that has recently failed. I am interested
in a tool that can strip wires in the range 10-22 AWG and possibly smaller
wires as the ones sometimes used in avionics and instruments. I would buy
2 strippers, if necessary.
>
> Could somebody make a recommendation for a good quality, reliable tool?
>
> Thanks
>
>
>
>
> Read this topic online here:
>
> http://forums.matronics.com/viewtopic.php?p=498730#498730
>
>
>
>
>
>
>
>
>
________________________________________________________________________________
| Subject: | Re: Wire stripper |
| From: | Charlie England <ceengland7(at)gmail.com> |
On 10/9/2020 6:33 PM, Argonaut36 wrote:
>
> I would like to replace my wire stripper that has recently failed. I am interested
in a tool that can strip wires in the range 10-22 AWG and possibly smaller
wires as the ones sometimes used in avionics and instruments. I would buy
2 strippers, if necessary.
>
> Could somebody make a recommendation for a good quality, reliable tool?
>
> Thanks
>
Do you want basic strippers, or an 'automatic' version? Auto is faster
(and a lot more expensive), but I find them harder to use when I need to
strip an exact amount for things like subD terminals. Ideal makes
automatic versions, if that's what you want.
Klein can almost always be counted on to make good tools; just google
'Klein wire strippers' to see what's available.
I've got an Ideal automatic, a Klein, and several other variations,
but to be honest, my go-to stripper is one I bought from a surplus goods
mail order company over 30 years ago. It might be worthwhile to take a
few wire scraps to a local hardware store, or even a 'big box' store, &
play with their selection of strippers. Pick one you're comfortable with
& go with it.
Charlie
--
This email has been checked for viruses by Avast antivirus software.
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________________________________________________________________________________
| Subject: | Kinda slick demisting fan speed control |
| From: | "rparigoris" <rparigor(at)hotmail.com> |
Hi Group Figured would share a kinda kool speed control for demisting / cooling
fans on instrument module. Fans are 12 volts. Using a DPTT switch. Either 2P2S
or 4P:
https://1drv.ms/u/s!Ah1S270Nwg9V3SVeUvEe3G84uKjR?e=HLzX1T
Pic of fans:
http://www.europaowners.org/main.php?g2_itemId=79733
Ron P.
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498735#498735
________________________________________________________________________________
| Subject: | Re: On-the-ground power jack |
| From: | "prestonkavanagh" <preston.kavanagh(at)gmail.com> |
I'm picking up this old thread because of the excellent walk through of the "why"
of the circuit....Building a Z101 Cozy and adding a ground power function using
Piper jacks. I need to find a suitable overvoltage protector. I don't see
the OVM-14 on the B&C site, but I wonder if I can use a Lambda LMOV unit.
Or am I better off mucking around with some MOS-FET's? Here's the Lambda OV protection
I have in mind - comments?
https://www.ebay.com/itm/Lambda-LMOV-2-Overvoltage-Protector-6-20v-dc/292566713401
The rest of the circuit would not change. Thanks for the help. Preston K.
--------
PBK3
PA-12, BD-4, RV6a, gliders
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498736#498736
________________________________________________________________________________
| Subject: | Re: On-the-ground power jack |
| From: | "user9253" <fransew(at)gmail.com> |
According to this pdf: https://www.mavin.com/pdf/LMOV-9.pdf
The LMOV-2 shorts out the power supply in case of over voltage. So it should work.
Another option is Perihelion Design's over voltage protection module $88.
http://www.periheliondesign.com/lovm.htm
It works by opening a circuit instead of shorting it out.
--------
Joe Gores
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498737#498737
________________________________________________________________________________
| Subject: | Re: On-the-ground power jack |
| From: | Charlie England <ceengland7(at)gmail.com> |
On 10/9/2020 8:59 PM, user9253 wrote:
>
> According to this pdf: https://www.mavin.com/pdf/LMOV-9.pdf
> The LMOV-2 shorts out the power supply in case of over voltage. So it should
work.
> Another option is Perihelion Design's over voltage protection module $88.
> http://www.periheliondesign.com/lovm.htm
> It works by opening a circuit instead of shorting it out.
>
> --------
> Joe Gores
>
>
Or the one I linked earlier, from Tomtop.
--
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________________________________________________________________________________
| From: | "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com> |
| Subject: | Some new battery chemistries on the horizon? |
While lithium products are the fair-haired
children in the portable energy storage
sandbox, there's a couple of interesting
technologies being spun-up in the EV
world:
https://tinyurl.com/yy8cqwbe
https://tinyurl.com/y2ptgrjz
A follow up on the two articles I cited above . . .
Here's a more detailed description of the
tab-less construction of the proposed
cylindrical cell by Tesla:
https://tinyurl.com/y4vv7ozl
Some of you may recall a few years back
when a start-up in Golden Colorado called
Bolder Technologies was rolling out
an improved version of SVLA jelly-roll
cells.
https://tinyurl.com/y42v9ztj
We looked at these at B&C. Examples of
the 'Start Stick' made appearances at
OSH about that time too. Truly amazing
performance . . . when they worked.
Seems that one, and perhaps the most important
process to master was how to achieve good
electrical contact with the (-) and (+)
plates on each end of the jelly-roll. You had
to get hooked up to the entire length of the
exposed edges at each end. Failing that,
achieving a consistent. 2 milliohm cell
resistance was not possible. Degradation of
that connection resulted in rapid failure of
the cell.
The company folded in the US and I think
the idea was sold . . . perhaps a couple
of times . . . off shore. Haven't hear
anything about them lately.
Now, it seems that the smart guys at Tesla
have a different approach to getting a grip
on the edges of foils. This may signal a
quantum jump in cell performance. Cells
like that would allow folks like AeroVoltz
to achieve really BIG cranking currents from
their relatively small packages.
I recall a conversation with Skip Koss
(battery guru par excellence at Concorde)
wherein diminutive cells with good
cranking might be fabricated into a battery
module that would fit right onto the back
of a starter motor . . . zero-length
fat wires in the cranking circuit.
For our purposes, this would allow dual
alternator systems to drop distribution wire
sizes down to just system loads and take
the battery out of the operational power
loop.
Interesting stuff . . .
Bob . . .
________________________________________________________________________________
| Subject: | Re: Wire stripper |
| From: | "Argonaut36" <fmlibrino(at)msn.com> |
Thanks to All for the help.
I placed an order for the Ideal Stripmaster 45-097.
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498740#498740
________________________________________________________________________________
| Subject: | Re: Peer review, Z16 Rotax engine, Ducati Regulator |
| From: | "velletazjp" <velletazjp(at)gmail.com> |
Thanks for your and Bob's wisdom...
Guess we're always learning...
I've taken into account the suggestion of the battery relay, explained the argument
once again, leveled pros & cons but it still a no in this situation.
Moved the crow bar.
Should at least work as it's intended...
--------
2020 contribution paid
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498742#498742
Attachments:
http://forums.matronics.com//files/schema_electrique_rev_b_184.pdf
________________________________________________________________________________
| Subject: | Garmin 400 series memory battery low |
Hi all,
After 16 years of sevice, our GPS 400 memory battery just died.
All stored data are lost, so no problem preserving them.
It seems the CR 14250 SE (3V) internal battery is soldered onto the
mother board.
According to some sources, replacement is straightforward, except some
ESD precautions are mandatory
https://www.ulimike.de/umhtml/gns_430.html
Has anyone here already performed such a replacement, and could shade
some light on the actual precautions (soldering iron, work table
covering, grounding wrist band, etc.) ?
Thanks in advance for you input, take care
--
Best regards,
Gilles
http://contrails.free.fr
http://lapierre.skunkworks.free.fr
________________________________________________________________________________
| From: | David Saylor <saylor.dave(at)gmail.com> |
| Subject: | Re: Garmin 400 series memory battery low |
I=99ve done a couple of those. It=99s pretty straightforward.
I don=99t recall
taking ESD precautions but if I did it again, I would.
=94Dave
On Sun, Oct 11, 2020 at 16:44 Gilles Thesee <gilles@elixir-aircraft.com>
wrote:
> gilles@elixir-aircraft.com>
>
> Hi all,
>
> After 16 years of sevice, our GPS 400 memory battery just died.
>
> All stored data are lost, so no problem preserving them.
>
> It seems the CR 14250 SE (3V) internal battery is soldered onto the
> mother board.
>
> According to some sources, replacement is straightforward, except some
> ESD precautions are mandatory
>
> https://www.ulimike.de/umhtml/gns_430.html
>
>
> Has anyone here already performed such a replacement, and could shade
> some light on the actual precautions (soldering iron, work table
> covering, grounding wrist band, etc.) ?
>
>
> Thanks in advance for you input, take care
>
> --
> Best regards,
> Gilles
> http://contrails.free.fr
> http://lapierre.skunkworks.free.fr
===========
===========
===========
===========
===========
>
>
________________________________________________________________________________
| From: | Charles Kuss <chaskuss(at)yahoo.com> |
| Subject: | Re: Garmin 400 series memory battery low |
Gilles,
I would suggest you use Google Translate to translate the German instructi
ons into English.
https://translate.google.com/#view=home&op=translate&sl=de&tl=en
Charlie K
e(at)gmail.com> wrote:
I=99ve done a couple of those. It=99s pretty straightforward.
=C2- I don=99t recall taking ESD precautions but if I did it again,
I would.
=94Dave
On Sun, Oct 11, 2020 at 16:44 Gilles Thesee <gilles@elixir-aircraft.com> wr
ote:
aft.com>
Hi all,
After 16 years of sevice, our GPS 400 memory battery just died.
All stored data are lost, so no problem preserving them.
It seems the CR 14250 SE (3V) internal battery is soldered onto the
mother board.
According to some sources, replacement is straightforward, except some
ESD precautions are mandatory
https://www.ulimike.de/umhtml/gns_430.html
Has anyone here already performed such a replacement, and could shade
some light on the actual precautions (soldering iron, work table
covering, grounding wrist band, etc.) ?
Thanks in advance for you input, take care
--
Best regards,
Gilles
http://contrails.free.fr
http://lapierre.skunkworks.free.fr
-
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m/Navigator?AeroElectric-List
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eferrer" target="_blank">http://forums.matronics.com
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errer" target="_blank">http://wiki.matronics.com
b Site -
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rel="noreferrer" target="_blank">http://www.matronics.com/contribution
________________________________________________________________________________
| From: | Charlie England <ceengland7(at)gmail.com> |
| Subject: | Re: Breaker then pump failure |
On Fri, Oct 9, 2020 at 12:24 AM David Saylor wrote:
> Charlie wrote:
>
>
>> The core pump in the AFP pumps I'm familiar with are Airtex brand in-line
>> fuel injection pumps, available online for between $60 & $100. Like this?
>>
>> https://www.amazon.com/Airtex-E2000-Electric-Fuel-Pump/dp/B000C1KHJG/ref=sr_1_7?dchild=1&keywords=airtex+fep2000+fuel+pump&qid=1602176199&sr=8-7
>> Either E2000 or FEP2000. Note that the hose barb shown on one end screws
>> off, allowing various other adapters.
>> If the OP wishes, I can measure my FEP2000 to verify dimensions.
>>
>> Charlie
>>
>
> Between Amazon and the Airtex web site, my pump seems most like an E8445.
> There are a lot of models and I haven't ID'd it exactly. The E2000 looks
> the same but it puts out almost three times the pressure that I see.
>
> I sent my pump assy to AFP where they replaced the pump for a little more
> than the Amazon price. They did a great job, shipping back the repaired
> assembly within hours of receiving it.
>
> Bob, if I get the old pump back, I'll send it to you along with the
> breaker.
>
> BTW, I just became aware of an AD from 2008 to replace this type of CB
> switch in Beechcraft products.
>
> --Dave
>
> Congrats on the inexpensive repair! The reason I'd bet on the E2000 is
that the E8445 appears to have a fixed hose barb output, while the E2000
has a threaded fitting on the output, allowing choice of fittings. Note
that both pumps are capable of much higher pressure (and volume) than
Bendix injection (or even automotive electronic injection) uses. Both types
require a mechanical 'bypass' style pressure regulator to set pressure, and
excess fuel is vented by the regulator. In the older cars where these pumps
were used, the bypassed fuel returned to the fuel tank. With the AFP pump
assembly, that extra block of metal in the assembly is the regulator and
routes the bypassed fuel back to the pump inlet. In later models, the same
device functions as a check valve, allowing the engine's mechanical pump to
'suck' fuel around the electric pump itself. Earlier models had a separate
check valve, IIRC.
Charlie
________________________________________________________________________________
| Subject: | Re: Breaker then pump failure |
| From: | Kelly McMullen <kellym(at)aviating.com> |
That AD is rather controversial, in that the exact same breaker is used
in many other plane models and brands, but the AD was only issued
against specific Beech models.
Kelly
On 10/12/2020 6:37 AM, Charlie England wrote:
> BTW, I just became aware of an AD from2008 to replace this type of
> CB switch in Beechcraft products.
>
> --Dave
>
________________________________________________________________________________
| From: | David Saylor <saylor.dave(at)gmail.com> |
| Subject: | Re: Breaker then pump failure |
Charlie,
The one that came back looked identical. Same threaded inlet, same banjo
outlet, same terminals. It's marked "Delphi FD0011". Delphi has a store
on Amazon, and the description is for a solenoid pump.
The new one sounds much different. I suppose it's a healthier sound now
but it seems much higher pitch.
AFP didn't send the old one back.
--Dave
>
>>
>
>> Congrats on the inexpensive repair! The reason I'd bet on the E2000 is
> that the E8445 appears to have a fixed hose barb output, while the E2000
> has a threaded fitting on the output, allowing choice of fittings. Note
> that both pumps are capable of much higher pressure (and volume) than
> Bendix injection (or even automotive electronic injection) uses. Both types
> require a mechanical 'bypass' style pressure regulator to set pressure, and
> excess fuel is vented by the regulator. In the older cars where these pumps
> were used, the bypassed fuel returned to the fuel tank. With the AFP pump
> assembly, that extra block of metal in the assembly is the regulator and
> routes the bypassed fuel back to the pump inlet. In later models, the same
> device functions as a check valve, allowing the engine's mechanical pump to
> 'suck' fuel around the electric pump itself. Earlier models had a separate
> check valve, IIRC.
>
> Charlie
>
________________________________________________________________________________
| From: | David Saylor <saylor.dave(at)gmail.com> |
| Subject: | Re: Breaker then pump failure |
Very interesting Finn. That makes a lot of sense.
On Fri, Oct 9, 2020 at 7:31 AM Finn Lassen wrote:
> NO. The braid is the weak point.
>
> Where it's spot welded to the contact it's hardened. As the switch is
> turned on/off the braid flexes. Same as what happens when you have a
> soldered flexible wire that is not supported at a point where the wire is
> still flexible (after the solder penetration).
>
________________________________________________________________________________
| From: | "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com> |
| Subject: | Re: Breaker then pump failure |
At 08:58 AM 10/12/2020, you wrote:
>
>That AD is rather controversial, in that the exact same breaker is
>used in many other plane models and brands, but the AD was only
>issued against specific Beech models.
>Kelly
I was on the team that worked that issue at Beech.
The failure mode that started the investigation
involved switch-breakers subject to the highest of
ship's loads, i.e. electric prop de-ice. I know that
same s/b was used on some Cessna models . . . but
perhaps only on lightly loaded circuits.
Root cause is a mechanical issue. The fine strand
jumper wire starts to loose strands due to operational
flexing of the jumper.
In the incident switches, loss of that jumper caused
system current to flow through the spring. For the
smaller switches, 5-10A, there is no immediate
indication of failure. For the higher current
applications, the spring heats up causing
smoke from the burning of the switch's housing.
I read that the smoke rather jetted from around
the switch's actuator handle.
Here's my library of photos and illustrations
generated to support my task at Beech along
with documents speaking to field responses.
https://tinyurl.com/y48y93rk
I worked analysis of the carcasses while others
researched affected aircraft . . . which was
a whole lot! There was a potential for thousands
of aircraft and tens of thousands of switches to be
at risk.
Cessna had a similar situation as cited in documents
offered above.
This was a tough one. Existence of the insulator
did not stop mechanical failure of the braid . . .
it only prevents smoke generation by the heavily
loaded switches. With the insulator in place,
the switch simply opens up.
Replacing all the at-risk switches in all fielded
aircraft was a really BIG deal. The Bonanza Society
and AOPA did a survey of affected aircraft owners
and came to the conclusion that the failures
were rare, occurrences of spring failure and
smoke were rarer still. They opined that these
events were very low risk and that a more relaxed
approach to dealing with the condition was
warranted. The FAA agreed.
Bob . . .
________________________________________________________________________________
| From: | Charlie England <ceengland7(at)gmail.com> |
| Subject: | Re: Breaker then pump failure |
The 1st hit I got on Amazon shows what appears to be a clone of the E2000.
(Or the E2000 is a clone of the Delphi; who knows? :-) ) The Amazon ad
says 'solenoid style'. Not sure what they mean by that, other than it's a
cylindrical container like the activator solenoid on a starter motor. The
pump is an electric motor, driving either a gerotor or roller-vane pump,
all inside that housing. The sound is a whir or whine, right? Not a
clicking sound. The low pressure Facet 'cube pumps' used as carb boost
pumps make a clicking/buzzing/rattling sound; they are effectively
'solenoid' pumps.
Just to be sure you know...Try your best to be sure that the pump gets a
prime (pumps fuel) quickly when you 1st run the pump, even if you have to
open the output side so it pumps into an open container. Most pumps like
these will self prime, but they will only survive for a few minutes without
fuel flowing through them. Configured like the AFP 'system' with the
regulator bypass back to the inlet, they sometimes *won't* self-prime
because they pump air in a loop around the pump instead of sucking fuel.
That can kill the pump in a few minutes.
Charlie
On Mon, Oct 12, 2020 at 10:41 AM David Saylor wrote:
> Charlie,
>
> The one that came back looked identical. Same threaded inlet, same banjo
> outlet, same terminals. It's marked "Delphi FD0011". Delphi has a store
> on Amazon, and the description is for a solenoid pump.
>
> The new one sounds much different. I suppose it's a healthier sound now
> but it seems much higher pitch.
>
> AFP didn't send the old one back.
>
> --Dave
>
>
>>
>>>
>>
>>> Congrats on the inexpensive repair! The reason I'd bet on the E2000 is
>> that the E8445 appears to have a fixed hose barb output, while the E2000
>> has a threaded fitting on the output, allowing choice of fittings. Note
>> that both pumps are capable of much higher pressure (and volume) than
>> Bendix injection (or even automotive electronic injection) uses. Both types
>> require a mechanical 'bypass' style pressure regulator to set pressure, and
>> excess fuel is vented by the regulator. In the older cars where these pumps
>> were used, the bypassed fuel returned to the fuel tank. With the AFP pump
>> assembly, that extra block of metal in the assembly is the regulator and
>> routes the bypassed fuel back to the pump inlet. In later models, the same
>> device functions as a check valve, allowing the engine's mechanical pump to
>> 'suck' fuel around the electric pump itself. Earlier models had a separate
>> check valve, IIRC.
>>
>> Charlie
>>
>
Virus-free.
www.avast.com
<#DAB4FAD8-2DD7-40BB-A1B8-4E2AA1F9FDF2>
________________________________________________________________________________
| From: | Jeff Luckey <jluckey(at)pacbell.net> |
| Subject: | Trouble with Image Attachment |
I'm trying to include a picture with a posting to the List by including as
an attachment.=C2- However I get an error message from the Matronics serv
er that says "Non supported enclosure type..".=C2-
The file is a 3 Mb .jpeg.=C2- The error message lists .jpeg=C2- as a va
lid attachment type.
What am I doing wrong?
-Jeff
________________________________________________________________________________
| From: | "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com> |
| Subject: | Re: Trouble with Image Attachment |
At 11:48 AM 10/12/2020, you wrote:
>I'm trying to include a picture with a posting to the List by
>including as an attachment. However I get an error message from the
>Matronics server that says "Non supported enclosure type..".
>
>The file is a 3 Mb .jpeg. The error message lists .jpeg as a valid
>attachment type.
>
>What am I doing wrong?
Hmmmm . . . try resizing the image
to 1Mb or less.
Bob . . .
________________________________________________________________________________
| From: | William Daniell <wdaniell.longport(at)gmail.com> |
| Subject: | In line fuseholder |
I have a Z 16 which includes the fusible link between the capacitor and the
starter contactor. However in a recent thread I saw that the 16
awg fuselink must be 8 inches - mine is about 4 inches. Also In the same
thread I understood that fuselink could be replaced with a time delay fuse.
Can I replace the 16awg fuselink with a 30A time delay maxi fuse?
thanks
Will
William Daniell
LONGPORT
+1 786 878 0246
________________________________________________________________________________
| From: | Jeff Luckey <jluckey(at)pacbell.net> |
| Subject: | Cinch Box Termina Block |
Are these "cinch box" connectors considered gas-tight.=C2- I have to imag
ine they are since the terminal block is UL & CSA, etc approved.
However, I don't see them used very much on aviation devices.=C2- Is ther
e a reason for that?
Please see the attached photo.
Thx,
Jeff Luckey
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September 26, 2020 - October 12, 2020
AeroElectric-Archive.digest.vol-pt