AeroElectric-List Digest Archive

Sun 07/07/19


Total Messages Posted: 25



Today's Message Index:
----------------------
 
     1. 04:38 AM - Re: Y splitter (Alec Myers)
     2. 07:00 AM - Limiting Current to a Battery (Jared Yates)
     3. 07:25 AM - Re: Limiting Current to a Battery (Ken Ryan)
     4. 08:06 AM - Re: Limiting Current to a Battery (user9253)
     5. 08:26 AM - Overvoltage protection (Joe Dubner)
     6. 08:46 AM - Re: Limiting Current to a Battery (Charlie England)
     7. 09:43 AM - Re: Limiting Current to a Battery (Alec Myers)
     8. 09:48 AM - Re: Overvoltage protection (Robert L. Nuckolls, III)
     9. 09:56 AM - Re: Y splitter (John Tipton)
    10. 10:03 AM - Re: Limiting Current to a Battery (David Saylor)
    11. 10:35 AM - Re: Limiting Current to a Battery (Charlie England)
    12. 11:04 AM - Re: Overvoltage protection (Robert L. Nuckolls, III)
    13. 11:14 AM - Re: Limiting Current to a Battery (David Saylor)
    14. 11:23 AM - Re: Limiting Current to a Battery (Alec Myers)
    15. 11:28 AM - Re: Limiting Current to a Battery (Charlie England)
    16. 12:26 PM - Re: Limiting Current to a Battery (Jared Yates)
    17. 01:46 PM - Re: Overvoltage protection (Joe Dubner)
    18. 01:47 PM - Re: Limiting Current to a Battery (Robert L. Nuckolls, III)
    19. 01:53 PM - Re: Limiting Current to a Battery (Robert L. Nuckolls, III)
    20. 02:22 PM - Re: Limiting Current to a Battery (Charlie England)
    21. 06:17 PM - Re: Y splitter (Argonaut36)
    22. 07:11 PM - Re: Limiting Current to a Battery (Robert L. Nuckolls, III)
    23. 07:29 PM - Re: Limiting Current to a Battery (Robert L. Nuckolls, III)
    24. 07:33 PM - Re: Limiting Current to a Battery (Robert L. Nuckolls, III)
    25. 08:00 PM - Speaking of well loaded wires . . . (Robert L. Nuckolls, III)
 
 
 


Message 1


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    Time: 04:38:57 AM PST US
    From: Alec Myers <alec@alecmyers.com>
    Subject: Re: Y splitter
    See: http://www.aeroelectric.com/articles/multiplewires/multiplewires.html See also: https://www.te.com/content/dam/te-com/documents/industrial-automation-and-control/global/1773464-1_QRG_PIDG.pdf FREQUENTLY ASKED QUESTIONS: Can wires be combined in PIDG terminals & splices? Yes they can as long total CMA (Circular Mil Area) and insulation diameter fall within specification. Also, per NASA-STD-8739.4A Section 19.9: Crimping wires into contacts or crimp ferrules is a method for splicing wires together without soldering. When crimping multiple wires into a contact or ferrule, the total circular-mil-area (CMA) of all the wires must be calculated into an Equivalent Wire Size (EWS) in order to select the properly sized contact or ferrule. 19.9.1 The following requirements apply for crimped splices: a. The tooling verification process and the completed termination shall comply with all the requirements of this document for a crimp termination except as specified herein for jiffy junction devices. b. The contact/wires size and crimp tool setting combination shall be developed and verified using the same requirements as for any machined contact (see 12.3.5). c. The crimp ferrule or contact shall be sized equivalently with the calculated Equivalent Wire Size (EWS) or the next larger EWS if the calculated value does not exactly match a single wire size. Dont twist the wires together, they should go into the barrel parallel. I believe when you double area of a wire, the AWG goes down by three. So 2 x 20 gauge wires would be 17 gauge. On Jul 6, 2019, at 11:09 PM, Argonaut36 <fmlibrino@msn.com> wrote: I was wondering if the practice of twisting 2 wires together and crimping the resulting wire in a ring terminal can be considered acceptable, even for standard certificate airplanes, for making a Y splitter. If so, assuming that 2 wires to be twisted together are size 20#, should a red or blue ring terminal be used? Thanks Read this topic online here: http://forums.matronics.com/viewtopic.php?p=490084#490084


    Message 2


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    Time: 07:00:35 AM PST US
    From: Jared Yates <email@jaredyates.com>
    Subject: Limiting Current to a Battery
    I have a question that's only somewhat applicable to E/AB aviation, apologies in advance. But I think it points out a hole in my electrical understanding. The characteristics of the lithium iron battery I'm running allow it to draw lots of current really fast after the engine starts. If it has been a little while since the last flight, the alternator is at max output for several minutes. The alternator puts out all it can give, and it's less than the battery wants to take. Stepping out of the hangar, my tow vehicle circuitry includes a wire in the 7-pin connector that provides alternator voltage to the trailer, intending to charge a small battery for a breakaway emergency brake. If I install a larger battery for other purposes, perhaps one like what is in the airplane, and connect it to that line coming from the truck, it seems like it would almost certainly open the fuse on that circuit during that initial high-draw stage. These two scenarios had me thinking, what methods would one have to limit a hungry battery's draw? I'm imagining some type of circuit that takes in 12-14 volts, and puts out almost the same, but only at some specified number of amps. Almost like a DC-powered battery charging circuit, rather than just putting the battery on the bus directly. Surely this has been solved in some off-the-shelf widget, but I haven't figured out the words to google yet.


    Message 3


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    Time: 07:25:11 AM PST US
    From: Ken Ryan <keninalaska@gmail.com>
    Subject: Re: Limiting Current to a Battery
    Jared, my holes in electrical knowledge are wide and vast, so don't do this without confirmation. But I think you might be able to regulate the amount of current by playing with the length of the cable, with a longer cable offering more resistance. I was instructed to do this once by a manufacturer of "battery isolator" for a camper battery, to keep my large alternator from frying the 70 amp isolator <http://hellroaring.com/products.php>. It seemed like an odd approach at the time, but I followed instructions and it worked okay. I'm not at all certain this would work for your particular problem, but I throw out the idea for discussion. On my next camper I went to a battery combiner <https://www.waytekwire.com/item/77051/Cole-Hersee-48530-Smart-Battery-Isolator-200A-/>and big double ought cables to maximize the charging of the camper battery, and also to allow use of the camper battery as an auxiliary starting battery. I don't have a lithium battery in the camper, so the highest draw I have ever seen was 80 amps. --Ken On Sun, Jul 7, 2019 at 6:05 AM Jared Yates <email@jaredyates.com> wrote: > I have a question that's only somewhat applicable to E/AB aviation, > apologies in advance. But I think it points out a hole in my electrical > understanding. > > The characteristics of the lithium iron battery I'm running allow it to > draw lots of current really fast after the engine starts. If it has been a > little while since the last flight, the alternator is at max output for > several minutes. The alternator puts out all it can give, and it's less > than the battery wants to take. > > Stepping out of the hangar, my tow vehicle circuitry includes a wire in > the 7-pin connector that provides alternator voltage to the trailer, > intending to charge a small battery for a breakaway emergency brake. If I > install a larger battery for other purposes, perhaps one like what is in > the airplane, and connect it to that line coming from the truck, it seems > like it would almost certainly open the fuse on that circuit during that > initial high-draw stage. > > These two scenarios had me thinking, what methods would one have to limit > a hungry battery's draw? I'm imagining some type of circuit that takes in > 12-14 volts, and puts out almost the same, but only at some specified > number of amps. Almost like a DC-powered battery charging circuit, rather > than just putting the battery on the bus directly. > > Surely this has been solved in some off-the-shelf widget, but I haven't > figured out the words to google yet. >


    Message 4


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    Time: 08:06:39 AM PST US
    Subject: Re: Limiting Current to a Battery
    From: "user9253" <fransew@gmail.com>
    The easy solution is to put a diode in series with the wire going to the trailer Lithium battery. The voltage drop across the diode will reduce charging current. Read this: https://earthxbatteries.com/dual-bus-lithium-battery-design -------- Joe Gores Read this topic online here: http://forums.matronics.com/viewtopic.php?p=490095#490095


    Message 5


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    Time: 08:26:26 AM PST US
    From: Joe Dubner <jdubner@yahoo.com>
    Subject: Overvoltage protection
    A friend is working on a Grumman Tiger in which the alternator field circuit breaker was found tripped. Upon digging in the manual, he found the overvoltage protection was simply a Zener diode wired from the output of the field breaker to ground. The diode was found to be shorted, which would easily trip the breaker. I can only find a "house number" on the Zener. The diode was removed, the old regulator was replaced with a Zeftronics with integral overvoltage protection, the split rocker switch was replaced with a new one, and all seems well -- except that one electrical instrument is inoperative (possibly due to an overvoltage event). My questions are as follows: can a physically small Zener diode (similar in size to a 1N5401 diode) handle the amount of energy required to trip a 5A breaker, even one time? Can the Zener always be counted upon to fail shorted and not open? Thanks, Joe


    Message 6


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    Time: 08:46:45 AM PST US
    Subject: Re: Limiting Current to a Battery
    From: Charlie England <ceengland7@gmail.com>
    On 7/7/2019 9:01 AM, Jared Yates wrote: > I have a question that's only somewhat applicable to E/AB aviation, > apologies in advance. But I think it points out a hole in my > electrical understanding. > > The characteristics of the lithium iron battery I'm running allow it > to draw lots of current really fast after the engine starts. If it has > been a little while since the last flight, the alternator is at max > output for several minutes. The alternator puts out all it can give, > and it's less than the battery wants to take. > > Stepping out of the hangar, my tow vehicle circuitry includes a wire > in the 7-pin connector that provides alternator voltage to the > trailer, intending to charge a small battery for a breakaway emergency > brake. If I install a larger battery for other purposes, perhaps one > like what is in the airplane, and connect it to that line coming from > the truck, it seems like it would almost certainly open the fuse on > that circuit during that initial high-draw stage. > > These two scenarios had me thinking, what methods would one have to > limit a hungry battery's draw? I'm imagining some type of circuit that > takes in 12-14 volts, and puts out almost the same, but only at some > specified number of amps. Almost like a DC-powered battery charging > circuit, rather than just putting the battery on the bus directly. > > Surely this has been solved in some off-the-shelf widget, but I > haven't figured out the words to google yet. Yeah, it could be solved. Which begs the question of why the big X didn't incorporate it into their management module. The simplest (rather inelegant) path would be a boost/buck regulator with current adjustment intended to operate from a DC source. https://www.amazon.com/s?k=current+regulator&ref=nb_sb_noss_1 Purchase a version that can't overload the wiring to the trailer connector. Feed the regulator from the alternator feed in the trailer connector. Set its output voltage to a level that can't harm the battery. Set its output current to a level that won't endanger the wiring from the alternator to the trailer connector. Charlie --- This email has been checked for viruses by Avast antivirus software. https://www.avast.com/antivirus


    Message 7


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    Time: 09:43:56 AM PST US
    From: Alec Myers <alec@alecmyers.com>
    Subject: Re: Limiting Current to a Battery
    On Jul 7, 2019, at 10:23 AM, Ken Ryan <keninalaska@gmail.com> wrote: ...But I think it points out a hole in my electrical understanding. . I'm imagining some type of circuit that takes in 12-14 volts, and puts out almost the same, but only at some specified number of amps. Remember a battery is a two terminal device. It functions like you pick the voltage across the terminals, Ill pick the current, or, equivalently you pick the current, Ill pick the voltage. You cant pick both the voltage across the terminals and the current through the battery, independently. You could put some kind of negative temperature coefficient thermistor in series with the battery, and shunt that with a fat diode so as not to limit the current withdrawable from the battery?


    Message 8


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    Time: 09:48:13 AM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Overvoltage protection
    At 10:25 AM 7/7/2019, you wrote: > >A friend is working on a Grumman Tiger in which the alternator field >circuit breaker was found tripped. Upon digging in the manual, he >found the overvoltage protection was simply a Zener diode wired from >the output of the field breaker to ground. The diode was found to >be shorted, which would easily trip the breaker. Yup. A stone simple ov protection scheme that made it onto a TC aircraft. Wrote about this for SA back in '93 . . . https://tinyurl.com/y38og7he Discovered later that the idea was not 'bad' as originally implemented. The design called for a GLASS, 1N4745, 1W zener tied to ground downstream of a 5A FUSE. Emacs! I did some testing on various zeners and found that only GLASS enclosed could be depended upon to fail shorted . . . plastics would occasionally split and fail to burn the fuse. Emacs! This is why the zener could only be 'legally' replaced with the Grumman house part number to make sure that the part was GLASS encased. Some airplanes were modified to replace cartridge fuses with breakers but left the zener in place . . . risky because the I(squared)t operation numbers for a breaker are larger than the fuse. >I can only find a "house number" on the Zener. The diode was >removed, the old regulator was replaced with a Zeftronics with >integral overvoltage protection, the split rocker switch was >replaced with a new one, and all seems well -- except that one >electrical instrument is inoperative (possibly due to an overvoltage event). Once the regulator is replaced with one that INCLUDES ov protection, the zener should be removed. >My questions are as follows: can a physically small Zener diode >(similar in size to a 1N5401 diode) handle the amount of energy >required to trip a 5A breaker, even one time? Can the Zener always >be counted upon to fail shorted and not open? Good question but moot after the regulator is replaced. Bob . . .


    Message 9


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    Time: 09:56:28 AM PST US
    From: John Tipton <john@tiptonuk.eu>
    Subject: Re: Y splitter
    And you still fuse for the the wire size ;(22awg - 3amp) although your using two 22awg wires that could be carrying 5/7amps John Sent from my iPad ----x--O--x---- > On 7 Jul 2019, at 12:37 pm, Alec Myers <alec@alecmyers.com> wrote: > > > See: > http://www.aeroelectric.com/articles/multiplewires/multiplewires.html > > > > See also: > https://www.te.com/content/dam/te-com/documents/industrial-automation-and-control/global/1773464-1_QRG_PIDG.pdf > FREQUENTLY ASKED QUESTIONS: > Can wires be combined in PIDG terminals & splices? Yes they can as long total CMA (Circular Mil Area) and insulation diameter fall within specification. > > > > Also, per NASA-STD-8739.4A Section 19.9: > > Crimping wires into contacts or crimp ferrules is a method for splicing wires together without soldering. When crimping multiple wires into a contact or ferrule, the total circular-mil-area (CMA) of all the wires must be calculated into an Equivalent Wire Size (EWS) in order to select the properly sized contact or ferrule. > > 19.9.1 The following requirements apply for crimped splices: > > a. The tooling verification process and the completed termination shall comply with all the requirements of this document for a crimp termination except as specified herein for jiffy junction devices. > > b. The contact/wires size and crimp tool setting combination shall be developed and verified using the same requirements as for any machined contact (see 12.3.5). > > c. The crimp ferrule or contact shall be sized equivalently with the calculated Equivalent Wire Size (EWS) or the next larger EWS if the calculated value does not exactly match a single wire size. > > > > > Dont twist the wires together, they should go into the barrel parallel. I believe when you double area of a wire, the AWG goes down by three. So 2 x 20 gauge wires would be 17 gauge. > > > > > > > > On Jul 6, 2019, at 11:09 PM, Argonaut36 <fmlibrino@msn.com> wrote: > > > I was wondering if the practice of twisting 2 wires together and crimping the resulting wire in a ring terminal can be considered acceptable, even for standard certificate airplanes, for making a Y splitter. If so, assuming that 2 wires to be twisted together are size 20#, should a red or blue ring terminal be used? > Thanks > > > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=490084#490084 > > > > > > > > > > > > > >


    Message 10


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    Time: 10:03:29 AM PST US
    From: David Saylor <saylor.dave@gmail.com>
    Subject: Re: Limiting Current to a Battery
    Would it be a DC-DC battery charger? https://www.renogy.com/renogy-12v-dc-to-dc-on-board-battery-charger/?gclid=CjwKCAjwsIbpBRBNEiwAZF8-z-TrUeFYygbwZh7wrFUpKO_RhdCJkW-vJ-BFwYS_IZjlu9G8uAMNcxoCgBoQAvD_BwE On Sun, Jul 7, 2019 at 7:05 AM Jared Yates <email@jaredyates.com> wrote: > I have a question that's only somewhat applicable to E/AB aviation, > apologies in advance. But I think it points out a hole in my electrical > understanding. > > The characteristics of the lithium iron battery I'm running allow it to > draw lots of current really fast after the engine starts. If it has been a > little while since the last flight, the alternator is at max output for > several minutes. The alternator puts out all it can give, and it's less > than the battery wants to take. > > Stepping out of the hangar, my tow vehicle circuitry includes a wire in > the 7-pin connector that provides alternator voltage to the trailer, > intending to charge a small battery for a breakaway emergency brake. If I > install a larger battery for other purposes, perhaps one like what is in > the airplane, and connect it to that line coming from the truck, it seems > like it would almost certainly open the fuse on that circuit during that > initial high-draw stage. > > These two scenarios had me thinking, what methods would one have to limit > a hungry battery's draw? I'm imagining some type of circuit that takes in > 12-14 volts, and puts out almost the same, but only at some specified > number of amps. Almost like a DC-powered battery charging circuit, rather > than just putting the battery on the bus directly. > > Surely this has been solved in some off-the-shelf widget, but I haven't > figured out the words to google yet. >


    Message 11


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    Time: 10:35:22 AM PST US
    Subject: Re: Limiting Current to a Battery
    From: Charlie England <ceengland7@gmail.com>
    That device won't limit current pulled through his feed to the trailer connector. While that device might work for its intended purpose, one of its claims is nonsense: * Overcomes voltage drop caused by long cable runs Unless its some corollary of a perpetual motion machine. Charlie On 7/7/2019 12:02 PM, David Saylor wrote: > Would it be a DC-DC battery charger? > > https://www.renogy.com/renogy-12v-dc-to-dc-on-board-battery-charger/?gclid=CjwKCAjwsIbpBRBNEiwAZF8-z-TrUeFYygbwZh7wrFUpKO_RhdCJkW-vJ-BFwYS_IZjlu9G8uAMNcxoCgBoQAvD_BwE > > > On Sun, Jul 7, 2019 at 7:05 AM Jared Yates <email@jaredyates.com > <mailto:email@jaredyates.com>> wrote: > > I have a question that's only somewhat applicable to E/AB > aviation, apologies in advance. But I think it points out a hole > in my electrical understanding. > > The characteristics of the lithium iron battery I'm running allow > it to draw lots of current really fast after the engine starts. If > it has been a little while since the last flight, the alternator > is at max output for several minutes. The alternator puts out all > it can give, and it's less than the battery wants to take. > > Stepping out of the hangar, my tow vehicle circuitry includes a > wire in the 7-pin connector that provides alternator voltage to > the trailer, intending to charge a small battery for a breakaway > emergency brake. If I install a larger battery for other purposes, > perhaps one like what is in the airplane, and connect it to that > line coming from the truck, it seems like it would almost > certainly open the fuse on that circuit during that initial > high-draw stage. > > These two scenarios had me thinking, what methods would one have > to limit a hungry battery's draw? I'm imagining some type of > circuit that takes in 12-14 volts, and puts out almost the same, > but only at some specified number of amps. Almost like a > DC-powered battery charging circuit, rather than just putting the > battery on the bus directly. > > Surely this has been solved in some off-the-shelf widget, but I > haven't figured out the words to google yet. > --- This email has been checked for viruses by Avast antivirus software. https://www.avast.com/antivirus


    Message 12


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    Time: 11:04:38 AM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Overvoltage protection
    At 10:25 AM 7/7/2019, you wrote: > >A friend is working on a Grumman Tiger in which the alternator field >circuit breaker was found tripped. Upon digging in the manual, he >found the overvoltage protection was simply a Zener diode wired from >the output of the field breaker to ground. The diode was found to >be shorted, which would easily trip the breaker. Yup. A stone simple ov protection scheme that made it onto a TC aircraft. Wrote about this for SA back in '93 . . . https://tinyurl.com/y38og7he Discovered later that the idea was not 'bad' as originally implemented. The design called for a GLASS, 1N4745, 1W zener tied to ground downstream of a 5A FUSE. The thing was designed to be a single event operator . . . IF you experienced an ov condition, the zener was expected to short, the fuse was expected to open. You would have to investigate and fix root cause of the ov condtion, then replace the zener and fuse before flying upward and onward. Emacs! I did some testing on various zeners and found that only GLASS enclosed could be depended upon to fail shorted . . . plastics would occasionally split apart and fail to burn the fuse. Emacs! This is why the zener could only be 'legally' replaced with the Grumman house part number to make sure that the part was GLASS encased. Some airplanes were modified to replace cartridge fuses with breakers but left the zener in place . . . risky because the I(squared)t operation numbers for the breaker are larger than a fuse. >I can only find a "house number" on the Zener. The diode was >removed, the old regulator was replaced with a Zeftronics with >integral overvoltage protection, the split rocker switch was >replaced with a new one, and all seems well -- except that one >electrical instrument is inoperative (possibly due to an overvoltage event). Once the regulator is replaced with one that INCLUDES ov protection, the zener should be removed. >My questions are as follows: can a physically small Zener diode >(similar in size to a 1N5401 diode) handle the amount of energy >required to trip a 5A breaker, even one time? Can the Zener always >be counted upon to fail shorted and not open? Good question but moot after the regulator is replaced. Bob . . .


    Message 13


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    Time: 11:14:37 AM PST US
    From: David Saylor <saylor.dave@gmail.com>
    Subject: Re: Limiting Current to a Battery
    >>That device won't limit current pulled through his feed to the trailer connector.<< If the 20A model was mounted to the truck, the feed would be limited to 20A. If it was mounted to the trailer, the feed would be limited to something more than 20A. >>While that device might work for its intended purpose, one of its claims is nonsense: - Overcomes voltage drop caused by long cable runs Unless its some corollary of a perpetual motion machine. << As someone mentioned earlier, long cable runs have been suggested as a solution. But since that's really just a resistor, you'd also get a voltage drop. This gizmo looks like it limits the current sent to the battery being charged without dropping the voltage. So it overcomes the voltage drop caused by the long cable run solution. I don't think they're suggesting that it makes magical energy. >


    Message 14


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    Time: 11:23:10 AM PST US
    From: Alec Myers <alec@alecmyers.com>
    Subject: Re: Limiting Current to a Battery
    The only way to limit the current drawn by a battery is to limit the voltage. On Jul 7, 2019, at 2:13 PM, David Saylor <saylor.dave@gmail.com> wrote: This gizmo looks like it limits the current sent to the battery being charged without dropping the voltage.


    Message 15


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    Time: 11:28:01 AM PST US
    Subject: Re: Limiting Current to a Battery
    From: Charlie England <ceengland7@gmail.com>
    On 7/7/2019 1:13 PM, David Saylor wrote: > >>That device won't limit current pulled through his feed to the > trailer connector.<< > > If the 20A model was mounted to the truck, the feed would be limited > to 20A. If it was mounted to the trailer, the feed would be limited > to something more than 20A. > > >>While that device might work for its intended purpose, one of its > claims is nonsense: > > * Overcomes voltage drop caused by long cable runs > > Unless its some corollary of a perpetual motion machine.<< > > As someone mentioned earlier, long cable runs have been suggested as a > solution. But since that's really just a resistor, you'd also get a > voltage drop. This gizmo looks like it limits the current sent to the > battery being charged without dropping the voltage. So it overcomes > the voltage drop caused by the long cable run solution. I don't think > they're suggesting that it makes magical energy. > P(ower)=V(oltage) / I (current) The only way to do what you suggest is...magical energy. To restore charge voltage *at the same current* after a voltage drop caused by a long cable run, you *must* increase current, to satisfy the power equation. How? --- This email has been checked for viruses by Avast antivirus software. https://www.avast.com/antivirus


    Message 16


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    Time: 12:26:15 PM PST US
    From: Jared Yates <email@jaredyates.com>
    Subject: Re: Limiting Current to a Battery
    Thank you everyone for the tips, I have ordered a power supply circuit to test and will report back. It includes an adjustment for the max current. On July 7, 2019 13:08:34 David Saylor <saylor.dave@gmail.com> wrote: > Would it be a DC-DC battery charger? > > https://www.renogy.com/renogy-12v-dc-to-dc-on-board-battery-charger/?gclid=CjwKCAjwsIbpBRBNEiwAZF8-z-TrUeFYygbwZh7wrFUpKO_RhdCJkW-vJ-BFwYS_IZjlu9G8uAMNcxoCgBoQAvD_BwE > > > On Sun, Jul 7, 2019 at 7:05 AM Jared Yates <email@jaredyates.com> wrote: > >> I have a question that's only somewhat applicable to E/AB aviation, >> apologies in advance. But I think it points out a hole in my electrical >> understanding. >> >> The characteristics of the lithium iron battery I'm running allow it to >> draw lots of current really fast after the engine starts. If it has been a >> little while since the last flight, the alternator is at max output for >> several minutes. The alternator puts out all it can give, and it's less >> than the battery wants to take. >> >> Stepping out of the hangar, my tow vehicle circuitry includes a wire in >> the 7-pin connector that provides alternator voltage to the trailer, >> intending to charge a small battery for a breakaway emergency brake. If I >> install a larger battery for other purposes, perhaps one like what is in >> the airplane, and connect it to that line coming from the truck, it seems >> like it would almost certainly open the fuse on that circuit during that >> initial high-draw stage. >> >> These two scenarios had me thinking, what methods would one have to limit >> a hungry battery's draw? I'm imagining some type of circuit that takes in >> 12-14 volts, and puts out almost the same, but only at some specified >> number of amps. Almost like a DC-powered battery charging circuit, rather >> than just putting the battery on the bus directly. >> >> Surely this has been solved in some off-the-shelf widget, but I haven't >> figured out the words to google yet. >>


    Message 17


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    Time: 01:46:20 PM PST US
    From: Joe Dubner <jdubner@yahoo.com>
    Subject: Re: Overvoltage protection
    Thank you, Bob. Mystery solved! You nailed it with this information and in the article you wrote for S.A. in 1993. But it's the first time I've heard of such a thing and was somewhat bewildered at a design depending on an unspecified parameter in this way. Thanks for the history and explanation. BTW, the diode we removed appeared to be plastic (like the one in your second attached image), not glass. But as you conclude (and we do too): it's moot after the regulator is replaced with one containing over-voltage regulation. Thanks again, Joe Robert L. Nuckolls, III wrote, On 7/7/2019 09:45: > At 10:25 AM 7/7/2019, you wrote: >> >> A friend is working on a Grumman Tiger in which the alternator field >> circuit breaker was found tripped. Upon digging in the manual, he >> found the overvoltage protection was simply a Zener diode wired from >> the output of the field breaker to ground. The diode was found to be >> shorted, which would easily trip the breaker. > > Yup. A stone simple ov protection scheme > that made it onto a TC aircraft. Wrote about > this for SA back in '93 . . . > > https://tinyurl.com/y38og7he > > Discovered later that the idea was not > 'bad' as originally implemented. The > design called for a GLASS, 1N4745, 1W zener > tied to ground downstream of a 5A > FUSE. > > > Emacs! > > > > > I did some testing on various > zeners and found that only GLASS enclosed > could be depended upon to fail shorted . . . > plastics would occasionally split > and fail to burn the fuse. > Emacs! > > > > This is why the zener could only be > 'legally' replaced with the Grumman house > part number to make sure that the part > was GLASS encased. > > Some airplanes were modified to replace > cartridge fuses with breakers but left > the zener in place . . . risky because > the I(squared)t operation numbers > for a breaker are larger than the fuse. > > >> I can only find a "house number" on the Zener. The diode was removed, >> the old regulator was replaced with a Zeftronics with integral >> overvoltage protection, the split rocker switch was replaced with a >> new one, and all seems well -- except that one electrical instrument >> is inoperative (possibly due to an overvoltage event). > > Once the regulator is replaced with one > that INCLUDES ov protection, the zener > should be removed. > > >> My questions are as follows: can a physically small Zener diode >> (similar in size to a 1N5401 diode) handle the amount of energy >> required to trip a 5A breaker, even one time? Can the Zener always be >> counted upon to fail shorted and not open? > > Good question but moot after the > regulator is replaced. > > > > Bob . . .


    Message 18


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    Time: 01:47:57 PM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Limiting Current to a Battery
    At 12:34 PM 7/7/2019, you wrote: >That device won't limit current pulled through his feed to the >trailer connector. > >While that device might work for its intended purpose, one of its >claims is nonsense: > * Overcomes voltage drop caused by long cable runs >Unless its some corollary of a perpetual motion machine. Don't think current through the connector was the problem . . . the 'high current' issue centers on the discharged battery's willingness to accept a replacement current greater than what is healthy for its physics. Hence, taking care of the battery calls for a constant voltage/constant current charging supply that is battery friendly . . . which is what this product would do . . . EXCEPT PERHAPS . . . that the specifications do not call out an 'adjustable' constant current range. It's basically a dc/dc converter with a full performance input range of 8-16 volts where the output would be held steady at specified charging/maintaining\ levels and a max current of 20A. The specs do not say that it's electronically limited to 20A although I suspect it would be. If the trailer battery is happy at 20A max charge current, then this critter would do the job . . . However, under a 20A output load, current through the trailer connector WILL be higher because of voltage drops being compensated for by the charger's electronics. Bob . . .


    Message 19


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    Time: 01:53:28 PM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Limiting Current to a Battery
    > Hence, taking care of the battery calls for > a constant voltage/constant current charging > supply that is battery friendly . . . which > is what this product would do . . . EXCEPT PERHAPS > . . . that the specifications do not call out > an 'adjustable' constant current range. Here's a less expensive device in the same power class. No "battery charging smarts" but it does have user adjustable voltage and current limits: https://tinyurl.com/y4qson88 Perhaps quite suited to the task . . . Bob . . .


    Message 20


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    Time: 02:22:32 PM PST US
    Subject: Re: Limiting Current to a Battery
    From: Charlie England <ceengland7@gmail.com>
    On 7/7/2019 3:46 PM, Robert L. Nuckolls, III wrote: > At 12:34 PM 7/7/2019, you wrote: >> That device won't limit current pulled through his feed to the >> trailer connector. >> >> While that device might work for its intended purpose, one of its >> claims is nonsense: >> >> * Overcomes voltage drop caused by long cable runs >> >> Unless its some corollary of a perpetual motion machine. > > Don't think current through the connector > was the problem . . . the 'high current' > issue centers on the discharged battery's > willingness to accept a replacement > current greater than what is healthy for its physics. > > Hence, taking care of the battery calls for > a constant voltage/constant current charging > supply that is battery friendly . . . which > is what this product would do . . . EXCEPT PERHAPS > . . . that the specifications do not call out > an 'adjustable' constant current range. > > It's basically a dc/dc converter with > a full performance input range of 8-16 > volts where the output would be held > steady at specified charging/maintaining\ > levels and a max current of 20A. > The specs do not say that it's electronically > limited to 20A although I suspect it would > be. > > If the trailer battery is happy at 20A max > charge current, then this critter would do > the job . . . However, under a 20A output > load, current through the trailer connector > WILL be higher because of voltage > drops being compensated for by the charger's > electronics. > > > Bob . . . > Bob, his question indicated an issue with limited current capacity of his wiring in the tow vehicle ('feed to the connector'). As I read his question, the issue in his specific situation is not with hurting the battery, but with overloading the supply circuit wiring ('open the fuse on that circuit during that initial high-draw stage'). Hence, my recommendation of a boost/buck power supply with current adjust. Charlie --- This email has been checked for viruses by Avast antivirus software. https://www.avast.com/antivirus


    Message 21


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    Time: 06:17:16 PM PST US
    Subject: Re: Y splitter
    From: "Argonaut36" <fmlibrino@msn.com>
    Thanks to All for the very good information provided! Read this topic online here: http://forums.matronics.com/viewtopic.php?p=490122#490122


    Message 22


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    Time: 07:11:15 PM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Limiting Current to a Battery
    >Bob, his question indicated an issue with limited current capacity >of his wiring in the tow vehicle ('feed to the connector'). As I >read his question, the issue in his specific situation is not with >hurting the battery, but with overloading the supply circuit wiring >('open the fuse on that circuit during that initial high-draw >stage'). Hence, my recommendation of a boost/buck power supply with >current adjust. > >Charlie Well fooey . . . got mentally snarled up in another discussion from years past . . . but I think I had this same discussion with a builder back in the Compuserve AvSig days. Not yet Dr. Dee and I were still running the airport . . . We fiddled with some current limiting schemes involving lengths of 10AWG wire (0.001 ohm/foot), a small contactor and a comparator to sense when drop across the resistor fell below a user adjustable level. The idea was to have additional resistance in the line to the discharged trailer battery that would be bypassed at some adjustable preset. That proved pretty messy. He decided to up-size his trailer connector to handle 6AWG battery feeders. I think it was this one: https://tinyurl.com/y48u7znv The mated pair of connectors was really cheaper than the bill of materials to do the fancy hat-dance with an electronically modulated current limiter. Since there was a battery on both ends of the feeder, I think he put an ANL35 on both ends. Thanks for the heads-up Charlie . . . Bob . . .


    Message 23


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    Time: 07:29:21 PM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Limiting Current to a Battery
    >Bob, his question indicated an issue with limited current capacity >of his wiring in the tow vehicle ('feed to the connector'). As I >read his question, the issue in his specific situation is not with >hurting the battery, but with overloading the supply circuit wiring >('open the fuse on that circuit during that initial high-draw >stage'). Hence, my recommendation of a boost/buck power supply with >current adjust. > >Charlie Well fooey . . . got mentally snarled up in another discussion from years past . . . but I think I had this same discussion with a builder back in the Compuserve AvSig days. Not yet Dr. Dee and I were still running the airport . . . We fiddled with some current limiting schemes involving lengths of 10AWG wire (0.001 ohm/foot), a small contactor and a comparator to sense when drop across the resistor fell below a user adjustable level. The idea was to have additional resistance in the line to the discharged trailer battery that would be bypassed at some adjustable preset. That proved pretty messy. He decided to up-size his trailer connector to handle 6AWG battery feeders. I think it was this one: https://tinyurl.com/y48u7znv The mated pair of connectors was really cheaper than the bill of materials to do the fancy hat-dance with an electronically modulated current limiter. Since there was a battery on both ends of the feeder, I think he put an ANL35 on both ends. Thanks for the heads-up Charlie . . . Bob . . .


    Message 24


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    Time: 07:33:32 PM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Limiting Current to a Battery
    > The mated pair of connectors was really > cheaper than the bill of materials to > do the fancy hat-dance with an > electronically modulated current > limiter. The link I offered for the connectors was to Waytek Wire who has a really comprehensive catalog of wiring products. Interested Listers are invited to download a copy of their catalog here: http://www.aeroelectric.com/Mfgr_Data/Misc/Waytek/waytek_catalog231.pdf Back in the days when we were selling a lot of materials, tools and supplies, we ordered quite a bit of stuff from Waytek. Bob . . .


    Message 25


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    Time: 08:00:03 PM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Speaking of well loaded wires . . .
    The a/c quit on the Barber Co homestead a couple days ago. Pulled of the covers and found a wire burned off the dual motor run capacitor. Emacs! The failure started in the Fast-On crimp and pretty well toasted the wire and it's mating capacitor tab before parting. I didn't think to save the carcass . . . While working the replacement, the wire fell out of the terminal on the FAN side of the capacitor! The terminal on the capacitor COMMON lead carries nearly the same current (~20A) as the COMPRESSOR side, but it was in good shape. HOWEVER . . . the other end of the capacitor COMMON wire attaching to the run contactor was starting to show stress . . . not in the crimp but on the Fast-On grips. Emacs! In the case cited above, the terminals were under-crimped. I'd replaced that same capacitor in years past but didn't see a problem with the terminals. But these were in service for over 10 years in a pretty unfriendly environment. This time, ALL the PIDG devices in the condenser wiring got replaced with a fine, ratchet-handled mash-tool. Even tho the catalogs offer a yellow PIDG for up to 10AWG wire, I think it prudent NOT to push this technology that hard in aircraft. 7A or so continuous in blue PIDG Fast-Ons have a track record of good performance. If you must push into yellow terminal territory, make sure they're 'real' TE Connectivity PIDG and use the ratchet-handled tool. Bob . . .




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