AeroElectric-List Digest Archive

Fri 10/04/13


Total Messages Posted: 18



Today's Message Index:
----------------------
 
     1. 02:41 AM - Re: ROTAX 912ULS ALT flicker..... Help?! (SIDESLIP)
     2. 04:33 AM - Re: Re: ROTAX 912ULS ALT flicker..... Help?! (Robert L. Nuckolls, III)
     3. 07:35 AM - Re: De-Slumpifier, Voltage Buffer to Prevent Brownout (user9253)
     4. 07:36 AM - Re: Dual voltage output from fuel quantity senders (Robert L. Nuckolls, III)
     5. 07:37 AM - Re: Re: De-Slumpifier, Voltage Buffer to Prevent Brownout (Robert L. Nuckolls, III)
     6. 08:06 AM - Electric System architecture (Robert L. Nuckolls, III)
     7. 08:11 AM - Re: Charging the Aux Battery (Robert L. Nuckolls, III)
     8. 08:11 AM - Re: Dual voltage output from fuel quantity senders (Bill Putney)
     9. 08:44 AM - Re: Re: Electric System architecture  (Carlos Trigo)
    10. 09:00 AM - Re: Charging the Aux Battery (Carlos Trigo)
    11. 09:18 AM - FW: VP-X Pro manual (Carlos Trigo)
    12. 09:58 AM - Re: Multiplexing 7-segment LED displays (TravisBryant)
    13. 10:52 AM - Re: ROTAX 912ULS ALT flicker..... Help?! (Eric M. Jones)
    14. 11:13 AM - Re: Dual voltage output from fuel quantity senders (Eric M. Jones)
    15. 12:43 PM - Re: Re: Dual voltage output from fuel quantity senders (Peter Pengilly)
    16. 02:51 PM - Re: FW: VP-X Pro manual (Robert L. Nuckolls, III)
    17. 04:01 PM - Re: FW: VP-X Pro manual (Peter Pengilly)
    18. 10:56 PM - test (Fred Klein)
 
 
 


Message 1


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    Time: 02:41:54 AM PST US
    Subject: Re: ROTAX 912ULS ALT flicker..... Help?!
    From: "SIDESLIP" <Chad2007@rogers.com>
    Thanks Bob! How do I go about getting one from Eric Jones? Chad -------- C-GYXQ. 912ULS. 601XL-B Read this topic online here: http://forums.matronics.com/viewtopic.php?p=409818#409818


    Message 2


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    Time: 04:33:28 AM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: ROTAX 912ULS ALT flicker..... Help?!
    At 04:40 AM 10/4/2013, you wrote: > >Thanks Bob! How do I go about getting one from Eric Jones? > >Chad See http://tinyurl.com/ngumthf Bob . . .


    Message 3


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    Time: 07:35:55 AM PST US
    Subject: Re: De-Slumpifier, Voltage Buffer to Prevent Brownout
    From: "user9253" <fransew@gmail.com>
    Eric sent me his prototype DeSlumpifier for testing on my RV-12. Prior to intalling it, I cranked the engine a few times with the ignition switches shut off. With no internal backup battery, the D-180 re-booted each time the engine was cranked. Next I installed the DeSlumpifier in series with pin 1 of the Dynon D-180 (Master Power). During engine cranking, the D-180 did not re-boot. It continued to operate normally. I repeated the test several times, cranking the engine for two seconds, waiting for 10 seconds, then repeating. In each case, the D-180 continued to operate without re-booting. Next on the agenda is actual starting of the engine and flight testing. Joe -------- Joe Gores Read this topic online here: http://forums.matronics.com/viewtopic.php?p=409833#409833


    Message 4


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    Time: 07:36:21 AM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Dual voltage output from fuel quantity senders
    At 03:26 PM 10/3/2013, you wrote: ><peter@sportingaero.com> > >I have 2 fuel gauges in my airplane that work on 12v and 5v, and >only one (resistance type) sender. I am trying to figure out how to >get both gauges to work and be accurate. The 12v gauge is a straight >analogue device with a pointer. The 5v gauge is part of an EFIS. At >present I am using the analogue gauge only and the EFIS is >continually upset at having no fuel quantity input. > >I have looked into a solution using an Arduino, sampling the data in >doesn't seem to be too difficult, using the analogue input and a >voltage divider circuit to drop the input voltage. I think I can get >the Arduino to drive something like a MCP41100 8 bit dual digital >potentiometer as an output device, with the 2 channels one for each >of the 12v & 5v circuits. However these devices work at 5v and low current. > >So my question to the smart people here is how to I use the output >of these digipots to look to the gauges as though they are a 30-240 >ohm fuel quantity sender? Assumptions: The input to your EFIS is 0-5 volts, high impedance with zero volts = zero fuel. The 30-240 ohm sender is minimum resistance at full fuel. The characteristics of your steam gauge are unknown but it's certain that the gauge is not a 'sensitive' voltmeter (i.e. movement that reads micro-amps). You need to hook it up on the bench like this and take some measurements: Emacs! Make a chart of instrument current draw, S-terminal voltage, and 'Sender' resistance for zero fuel, 1/4 fuel, 1/2 fuel, 3/4 fuel, and full fuel. I'm pretty sure you can do all that needs to be done with analog components (op amps etc) but we first need to characterize the steam guage . . . this is a bit like the game where somebody hands you a little box with 2 or more terminals on it. You get to 'probe' the box by measuring at the external terminals. The challenge is to describe what's inside the box. This task is a little simpler, we only need to know the DC characteristics of the guage for indications it THINKS are coming from the companion sensor end the tank. Yeah, that 10v supply is on purpose, we'll endeavor to regulate power to the guage for better prediction of the design. In fact, do the experiment twice, the second time with say 8 volts applied to the guage and see what those numbers are too. Bob . . .


    Message 5


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    Time: 07:37:38 AM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: De-Slumpifier, Voltage Buffer to Prevent
    Brownout At 09:34 AM 10/4/2013, you wrote: > >Eric sent me his prototype DeSlumpifier for testing on my >RV-12. Prior to intalling it, I cranked the engine a few times with >the ignition switches shut off. With no internal backup battery, >the D-180 re-booted each time the engine was cranked. Next I >installed the DeSlumpifier in series with pin 1 of the Dynon D-180 >(Master Power). During engine cranking, the D-180 did not >re-boot. It continued to operate normally. I repeated the test >several times, cranking the engine for two seconds, waiting for 10 >seconds, then repeating. In each case, the D-180 continued to >operate without re-booting. Next on the agenda is actual starting >of the engine and flight testing. >Joe > >-------- >Joe Gores > Good data sir. Thanks! Did you sent me the DC/DC converter you tried the first time? Bob . . .


    Message 6


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    Time: 08:06:21 AM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Electric System architecture
    At 03:34 PM 10/3/2013, you wrote: >Bob & Carlos, > >What a great, and insightful, exchange of information and facts. >Clear, concise, and easily readable. Since Carlos has a Vertical Power product in his airplane, this won't be a design study starting from a clean piece of paper but discussions for integrating accessories around the Vertical Power architecture can still be shared. I'm contemplating an article for KitPlanes that will describe the clean piece of paper approach to system architecture in an OBAM aircraft. This is a pretty strange idea for most pilots. The vast majority of OBAM aircraft emulate the architectures of TC aircraft. At the same time, TC aircraft are very cookie-cutter like in their design and manufacture. It's a whole new idea to flip through the z-figures (or a Vertical Power catalog) and contemplate the opportunities traded off with personal design goals. Too many builders have their battery, alternator and switches already attached to the airplane before they get serious about how they'll all work with each other to meet design goals not yet formalized. Getting the cart so far in front of the horse is not a high risk activity but it does limit opportunities to have a system that the builder understands because it's designed it to a goal as opposed to a collection of cherry-picked ideas thrown into a basket before the best possible recipe for success is discovered. I'll try to bring some of the thought processes proven useful in TC aviation for decades to what has become the real leading edge in light aircraft design and fabrication. The ideal evolution of a project has the recipe 98% defined before the first hole is drilled. Not a really big deal . . . most electrical bad days in the cockpit are the product of poor craftsmanship and/or maintenance as opposed to selection of components and architecture. Very rarely do we hear of an instance where architecture was the driving force for a bad day in the airplane. I'm still waiting for permission to share the data from one such case that is now settled. The folks who paid my exorbitant fees to analyze the event own the work product. I hope to have some videos and other documents to share. In any event, one does not have to 'bake somebody else's cookies' to avoid serious error. That's what we do here on the List. Carlos is putting the frosting and chocolate sprinkles on a recipe with a proven track record so our imaginings are already bounded . . . and that's okay. Bob . . .


    Message 7


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    Time: 08:11:08 AM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Charging the Aux Battery
    At 01:46 PM 9/29/2013, you wrote: > >Bob and all > >This is probably a dumb question but I will make it anyway. >In a Dual battery electric system architecture, like Z-14 for >example, the Aux Battery will not be charging in flight unless the >aux batt. Switch is flipped On (thus closing the Aux Batt contactor), right? Carlos, Now that the edges of the sandbox have been discovered, how do you envision that a second battery would be integrated into a V-P system and how would it fit into your plans for dealing with failure? Are you considering a second alternator of ANY size on the vacuum pump pad? As I recall, V-P attends to second alternator and/or battery . . . does their installation literature speak to these options? Bob . . .


    Message 8


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    Time: 08:11:22 AM PST US
    From: Bill Putney <billp@wwpc.com>
    Subject: Re: Dual voltage output from fuel quantity senders


    Message 9


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    Time: 08:44:40 AM PST US
    From: "Carlos Trigo" <trigo@mail.telepac.pt>
    Subject: RE: Electric System architecture
    Bob Please don't be demotivated by the VP-X word... That box is not much more than an encapsulated Buss, with some electronic features allowing things to be seen in a screen (instead of V & A indicators and a bunch of colored lights of an annunciator panel) .. :-) I still have to decide about the architecture ... batteries, alternators, power source ... protection Carlos -----Mensagem original----- De: owner-aeroelectric-list-server@matronics.com [mailto:owner-aeroelectric-list-server@matronics.com] Em nome de Robert L. Nuckolls, III Enviada: 3 de outubro de 2013 21:22 Para: aeroelectric-list@matronics.com Assunto: Re: AeroElectric-List: RE: Electric System architecture (was Charging the Aux Battery) --> <nuckolls.bob@aeroelectric.com> > > > Do any of these accessories feature built in > back up batteries and/or connections brought > out for dual power sourcing? >Yes, the EFIS will be dual power sourcing. >I am using a VP-X Pro box. Oopa . . . okay, there's not much I can do for you in terms of architecture . . . that's pretty much carved in stone. We can certainly continue to discuss application and suitability of various parts, but I'm not sure there's much I can contribute for architecture decisions that are not pre-determined out of the box. Bob . . .


    Message 10


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    Time: 09:00:09 AM PST US
    From: "Carlos Trigo" <trigo@mail.telepac.pt>
    Subject: Charging the Aux Battery
    Please see answers below -----Mensagem original----- De: owner-aeroelectric-list-server@matronics.com [mailto:owner-aeroelectric-list-server@matronics.com] Em nome de Robert L. Nuckolls, III Enviada: 4 de outubro de 2013 16:11 Para: aeroelectric-list@matronics.com Assunto: Re: AeroElectric-List: Charging the Aux Battery --> < <mailto:nuckolls.bob@aeroelectric.com> nuckolls.bob@aeroelectric.com> At 01:46 PM 9/29/2013, you wrote: >--> < <mailto:trigo@mail.telepac.pt> trigo@mail.telepac.pt> > >Bob and all > >This is probably a dumb question but I will make it anyway. >In a Dual battery electric system architecture, like Z-14 for example, >the Aux Battery will not be charging in flight unless the aux batt. >Switch is flipped On (thus closing the Aux Batt contactor), right? Carlos, Now that the edges of the sandbox have been discovered, how do you envision that a second battery would be integrated into a V-P system and how would it fit into your plans for dealing with failure? There are several objectives I am trying to reach with the decision of including a second battery: (I mean objectives directly related with electric features, because there are the side consequences in weight - bad for the Total weight of the bird, but perhaps good for the W & B calculations when travelling alone.) - Spare juice for the starter cranking power - Back-up power for the VP-X box and features - Back-up power for the EFIS and radio - Back-up power for the fuel pump - Are you considering a second alternator of ANY size on the vacuum pump pad? I am considering an SD-8 or an SD-20, but I am not sure it will be overkill to have 2 batteries and 2 alternators (even considering the big bunch of electron consumers aboard the modern OBAM aircraft.) As I recall, V-P attends to second alternator and/or battery . . . does their installation literature speak to these options? Yes it does. I am at my job place right now, and the manual is at home, but I will try to find it online and copy paste the competent pages Regards Carlos


    Message 11


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    Time: 09:18:50 AM PST US
    From: "Carlos Trigo" <trigo@mail.telepac.pt>
    Subject: VP-X Pro manual
    Here You can find the VP-X Pro installation and operation manual here http://verticalpower.com/docs/Install_Ops_Manual_VP-X_P_S.pdf Information about the Dual Buss feature, but only with one energy source, is on pages 9 and 10 - paragraph 4.4 Information about using a 2nd alternator is on page 28 - paragraphs 5.9c and 5.9d Information about wiring back-up circuits is on pages 43 to 46 - paragraph 5.24 and 5.24a through 5.24e Information about using a 2nd battery is on pages 47 to 49 - paragraphs 5.26 and 5.27 Hope this helps Carlos De: Carlos Trigo [mailto:trigo@mail.telepac.pt] Enviada: 4 de outubro de 2013 17:03 Para: 'aeroelectric-list@matronics.com' Assunto: RE: AeroElectric-List: Charging the Aux Battery Please see answers below -----Mensagem original----- De: owner-aeroelectric-list-server@matronics.com <mailto:owner-aeroelectric-list-server@matronics.com> [mailto:owner-aeroelectric-list-server@matronics.com] Em nome de Robert L. Nuckolls, III Enviada: 4 de outubro de 2013 16:11 Para: aeroelectric-list@matronics.com <mailto:aeroelectric-list@matronics.com> Assunto: Re: AeroElectric-List: Charging the Aux Battery --> < <mailto:nuckolls.bob@aeroelectric.com> nuckolls.bob@aeroelectric.com> At 01:46 PM 9/29/2013, you wrote: >--> < <mailto:trigo@mail.telepac.pt> trigo@mail.telepac.pt> > >Bob and all > >This is probably a dumb question but I will make it anyway. >In a Dual battery electric system architecture, like Z-14 for example, >the Aux Battery will not be charging in flight unless the aux batt. >Switch is flipped On (thus closing the Aux Batt contactor), right? Carlos, Now that the edges of the sandbox have been discovered, how do you envision that a second battery would be integrated into a V-P system and how would it fit into your plans for dealing with failure? There are several objectives I am trying to reach with the decision of including a second battery: (I mean objectives directly related with electric features, because there are the side consequences in weight - bad for the Total weight of the bird, but perhaps good for the W & B calculations when travelling alone.) - Spare juice for the starter cranking power - Back-up power for the VP-X box and features - Back-up power for the EFIS and radio - Back-up power for the fuel pump - Are you considering a second alternator of ANY size on the vacuum pump pad? I am considering an SD-8 or an SD-20, but I am not sure it will be overkill to have 2 batteries and 2 alternators (even considering the big bunch of electron consumers aboard the modern OBAM aircraft.) As I recall, V-P attends to second alternator and/or battery . . . does their installation literature speak to these options? Yes it does. I am at my job place right now, and the manual is at home, but I will try to find it online and copy paste the competent pages Regards Carlos


    Message 12


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    Time: 09:58:07 AM PST US
    Subject: Re: Multiplexing 7-segment LED displays
    From: "TravisBryant" <christopher55@buyhidkits.com>
    [quote="james(at)etravel.org"]I'm wondering if anyone can answer this question: I'd like to build a new fuel gauge based around 7-segment LED displays, driven by a PIC / Arduino, etc. Instead of running dozens of IO lines, I'd like to multiplex the displays so that the total number of lines is 7 + (no. of digits). The idea would be to switch on a common line for each digit in turn, and set the state for the seven segment lines for the digit that's currently lit. I hope that makes sense. Anyway, I'm sure the software will be straightforward enough (he says!) but it's the circuitry with which I need some help. Can anyone recommend a few components to drive the LED displays from the PIC, along with a circuit diagram? I have a bunch of resistors and general purpose transistors in my electronics kit. I'd probably test this on a PIC18F4680, because I have a neat little prototype board with this particular chip, along with HDSP-315E 7-segment digits, which is acommon anode type. Happy to share my findings with anyone who's interested! Many thanks, James > [b] Very interesting information.. Can you share more details about the project as I would like to work on it Read this topic online here: http://forums.matronics.com/viewtopic.php?p=409851#409851


    Message 13


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    Time: 10:52:09 AM PST US
    Subject: Re: ROTAX 912ULS ALT flicker..... Help?!
    From: "Eric M. Jones" <emjones@charter.net>
    Newer alternators probably have electronics that illuminate a red LED to warn of low voltage. But for almost a century the low voltage lamp was a little incandescent lamp. Swapping it with an LED is not stone simple, since the internal regulator might depend on the characteristics of the incandescent lamp. So here is an LED that "looks like" an incandescent lamp. Attached. http://www.jimcotest.com/docs/JIMCO%20Alternator%20Test%20Lead%20Picture%20Guide.pdf -------- Eric M. Jones www.PerihelionDesign.com 113 Brentwood Drive Southbridge, MA 01550 (508) 764-2072 emjones(at)charter.net Read this topic online here: http://forums.matronics.com/viewtopic.php?p=409855#409855 Attachments: http://forums.matronics.com//files/alternator_led_170.pdf


    Message 14


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    Time: 11:13:43 AM PST US
    Subject: Re: Dual voltage output from fuel quantity senders
    From: "Eric M. Jones" <emjones@charter.net>
    > I have 2 fuel gauges in my airplane that work on 12v and 5v, and only > one (resistance type) sender. I am trying to figure out how to get both > gauges to work and be accurate. The 12v gauge is a straight analogue > device with a pointer. The 5v gauge is part of an EFIS. At present I am > using the analogue gauge only and the EFIS is continually upset at > having no fuel quantity input. > > I have looked into a solution using an Arduino, sampling the data in > doesn't seem to be too difficult, using the analogue input and a voltage > divider circuit to drop the input voltage. I think I can get the Arduino > to drive something like a MCP41100 8 bit dual digital potentiometer as > an output device, with the 2 channels one for each of the 12v & 5v > circuits. However these devices work at 5v and low current. > > So my question to the smart people here is how to I use the output of > these digipots to look to the gauges as though they are a 30-240 ohm > fuel quantity sender? > > Regards, Peter > sampling the data in doesn't seem to be too difficult, using the analogue input and a voltage divider circuit to drop the input voltage So Peter, why not run that output into the Efis? Or if this won't do, then reduce the 12V ratiometric voltage with an op amp. I think your approach is getting way too complicated to start adding an Arduino. What am I missing? -------- Eric M. Jones www.PerihelionDesign.com 113 Brentwood Drive Southbridge, MA 01550 (508) 764-2072 emjones(at)charter.net Read this topic online here: http://forums.matronics.com/viewtopic.php?p=409857#409857


    Message 15


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    Time: 12:43:55 PM PST US
    From: Peter Pengilly <peter@sportingaero.com>
    Subject: Re: Dual voltage output from fuel quantity senders
    > So Peter, why not run that output into the Efis? Or if this won't do, then reduce the 12V ratiometric voltage with an op amp. I think your approach is getting way too complicated to start adding an Arduino. What am I missing? Perhaps nothing!! I just don't know very much about analogue electronics. If I could avoid the Arduino that would be great. I will find out about what the EFIS is expecting and try to characterise the steam gauge as Bob suggested. It may take a few days, but thanks both for the pointers. Peter On 04/10/2013 19:13, Eric M. Jones wrote: > > >> I have 2 fuel gauges in my airplane that work on 12v and 5v, and only >> one (resistance type) sender. I am trying to figure out how to get both >> gauges to work and be accurate. The 12v gauge is a straight analogue >> device with a pointer. The 5v gauge is part of an EFIS. At present I am >> using the analogue gauge only and the EFIS is continually upset at >> having no fuel quantity input. >> >> I have looked into a solution using an Arduino, sampling the data in >> doesn't seem to be too difficult, using the analogue input and a voltage >> divider circuit to drop the input voltage. I think I can get the Arduino >> to drive something like a MCP41100 8 bit dual digital potentiometer as >> an output device, with the 2 channels one for each of the 12v & 5v >> circuits. However these devices work at 5v and low current. >> >> So my question to the smart people here is how to I use the output of >> these digipots to look to the gauges as though they are a 30-240 ohm >> fuel quantity sender? >> >> Regards, Peter > > >> sampling the data in doesn't seem to be too difficult, using the analogue input and a voltage divider circuit to drop the input voltage > > So Peter, why not run that output into the Efis? Or if this won't do, then reduce the 12V ratiometric voltage with an op amp. I think your approach is getting way too complicated to start adding an Arduino. > > What am I missing? > > -------- > Eric M. Jones > www.PerihelionDesign.com > 113 Brentwood Drive > Southbridge, MA 01550 > (508) 764-2072 > emjones(at)charter.net > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=409857#409857 > >


    Message 16


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    Time: 02:51:45 PM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: VP-X Pro manual
    At 11:21 AM 10/4/2013, you wrote: >Here > >You can find the VP-X Pro installation and operation manual here > ><http://verticalpower.com/docs/Install_Ops_Manual_VP-X_P_S.pdf>http://verti calpower.com/docs/Install_Ops_Manual_VP-X_P_S.pdf > >Information about the Dual Buss feature, but >only with one energy source, is on pages 9 and 10 ' paragraph 4.4 >Information about using a 2nd alternator is on >page 28 ' paragraphs 5.9c and 5.9d >Information about wiring back-up circuits is on >pages 43 to 46 ' paragraph 5.24 and 5.24a through 5.24e >Information about using a 2nd battery is on >pages 47 to 49 ' paragraphs 5.26 and 5.27 > >Hope this helps I'll need to sit down with a brew and pray over this for a bit . . . Bob . . .


    Message 17


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    Time: 04:01:59 PM PST US
    From: Peter Pengilly <peter@sportingaero.com>
    Subject: Re: VP-X Pro manual
    I have two problems with devices such as the VP-X. One of the basic tenents it is designed around is that electrics are difficult, and so its worth paying $$$ for a box to do the job. We know that is not true, but if it were, I don't think the box is smart enough. Second, you are required to hand over pretty much all control of the system to a software intensive box where the manufacturer is reluctant to disclose the standards to which the hardware and software are designed and tested - which to me is not a great idea. It is marketed very well, but I'm not at all sure it provides value for money. The website talks about electronic circuit breakers, and the critical importance of monitoring the status of your electrical system. To me neither are really important. Circuit breakers are just a mechanical means of meeting a requirement to prevent services drawing more current than the wiring can support. I assume the electronic circuit breakers in a VP-X are really current monitors - so I guess what is really happening is the box monitors the expected current draw, compares the actual draw and disconnects the circuit if the current draw is greater. Its rather condescending to call these 'electronic circuit breakers', implying that they are an automatic disconnection function, why not call them what they are , something like an active current monitor. The box must be fully up and running for the current monitoring functions to work. So if the box really is smart can't it do something else than just switch off the circuit? Circuit protection is important, but breakers are yesterday's way of achieving the aim. Do we really need to know the status of the electrical system? In a conventional system we will know if a fuse blows as the service will not work. Current monitoring is straight forward, and voltage monitoring is something that just about every box does now. What additional benefit does the VP-X offer? It does offer other facilities, such as wig-wags, trim protection and flap protection. But I don't really want to hand over control of flight controls (ie the trim) to an unknown box of software. It also claims to disable the flaps above a certain airspeed - but how is that airspeed sensed and communicated? Unless that function is implemented in some fairly high integrity way I would not be too happy to rely on it - would failure at high airspeed mean that the flaps would deploy at way over the limit speed with potentially serious results? I think that using a system such as this would demand a completely separate endurance bus, probably supported by its own alternator - I see no merit in hooking 2 alternators into one VP-X box. For me its too many eggs in one box of unknown fragility. Apologies for the rather negative post. Peter On 04/10/2013 22:50, Robert L. Nuckolls, III wrote: > At 11:21 AM 10/4/2013, you wrote: >> Here >> >> You can find the VP-X Pro installation and operation manual here >> >> http://verticalpower.com/docs/Install_Ops_Manual_VP-X_P_S.pdf >> <http://verticalpower.com/docs/Install_Ops_Manual_VP-X_P_S.pdf> >> >> Information about the Dual Buss feature, but only with one energy >> source, is on pages 9 and 10 -- paragraph 4.4 >> Information about using a 2^nd alternator is on page 28 -- paragraphs >> 5.9c and 5.9d >> Information about wiring back-up circuits is on pages 43 to 46 -- >> paragraph 5.24 and 5.24a through 5.24e >> Information about using a 2^nd battery is on pages 47 to 49 -- >> paragraphs 5.26 and 5.27 >> >> Hope this helps > > I'll need to sit down with a brew and pray over > this for a bit . . . > > > Bob . . . > > * > > > *


    Message 18


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    Time: 10:56:36 PM PST US
    From: Fred Klein <fklein@orcasonline.com>
    Subject: test
    test




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