AeroElectric-List Digest Archive

Sun 07/10/22


Total Messages Posted: 4



Today's Message Index:
----------------------
 
     1. 10:17 AM - Re: Re: Thermocouples: grounded or ungrounded (Robert L. Nuckolls, III)
     2. 10:37 AM - Re: OAT Probes for Garmin Transponder (Robert L. Nuckolls, III)
     3. 01:03 PM - Re: OAT Probes for Garmin Transponder (andymeyer)
     4. 05:52 PM - Re: Re: OAT Probes for Garmin Transponder (Jared Yates)
 
 
 


Message 1


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    Time: 10:17:39 AM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Thermocouples: grounded or ungrounded
    At 04:04 PM 7/8/2022, you wrote: >Bob >I agree with what you are saying concerning the >ideal method of monitoring the coils. >However I need to work with what I have and I >don't think I can monitor 12 individual >coils with the tools at my disposal. Previous examples of failure involved but a single coil of the 5. Correct me if I'm wrong, but I seem to recall that Revmaster presently splits the TEN alternator stator poles into two groups . . . rated at 18A each. Okay, this is the first photo I recall seeing of a total-toasting of all 5 coils on the Revmaster alternator. This suggest a different failure mode. Bad R/R? Too much system loads? Probably something different than conditions the precipitates a single pole conflagration. The difference in coil failures suggests at least two, different operational stresses. It would be interesting to know the rational behind the 'dual alternator' decision. History shows us that capability of the individual half-alternators is marginal. Has anyone considered a single winding spread over all ten pole pieces wound with fewer turns of heavier wire to produce a single alternator of say 20, 25A . . . or more? If the two existing windings are reasonably matched, they could be operated in parallel as a single winding. Watts dissipated is proportional to I(squared) x R. So dropping current in each winding by one half reduces heat generated in that winding by 75%. That offers greater value in stress reduction than adding cooling air. I do plan on using your idea of the rotary switch and I appreciate the schematic.=C2 I thought all might be interested in a picture of the stator after removal.=C2 The one coil suffered catastrophic damage with the phenolic spacer completely destroyed by the heat.=C2 I have machined the case to allow more ventilation and will add two blast tubes directly at the coils.=C2 And hope for the best. Bob . . . Un impeachable logic: George Carlin asked, "If black boxes survive crashes, why don't they make the whole airplane out of that stuff?"


    Message 2


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    Time: 10:37:34 AM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: OAT Probes for Garmin Transponder
    At 09:06 PM 7/9/2022, you wrote: >I've been working with a Garmin GTX 335 transponder installation. >There is an optional outside air temp probe that enables a handy >density altitude feature. > >I found one reference that says the transponder is looking for this: >OUTSIDE AIR TEMPERATURE PROBE STANDARD 2-WIRE THERMOCOUPLE WITH 1 >MICRO-AMP PER 1 DEGREE KELVIN RESPONSE. SUITABLE MODELS ARE: EDMO >655 AND DAVTRON C307PS. > >I tried an extra Dynon OAT probe that I had sitting around, and it >indicated 175 degrees F. So I can rule out that one. > >The extra transponder feature is cool but not really cool enough to >spend $150 on one of the above probes. Does anyone know what kind of >thermocouple will produce 1 microamp per degree kelvin? Seems like >making something up might be a fun experiment. I believe those probes are based on the Analog Devices AD590 temperature to current sensor chip. https://tinyurl.com/2mqyzbtj You can probably craft a substitute probe from one of these available from Digikey and elsewhere Bob . . . Un impeachable logic: George Carlin asked, "If black boxes survive crashes, why don't they make the whole airplane out of that stuff?"


    Message 3


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    Time: 01:03:31 PM PST US
    Subject: Re: OAT Probes for Garmin Transponder
    From: "andymeyer" <meyerkc135@gmail.com>
    Use this: AD592 from Mouser https://www.mouser.com/ProductDetail/584-AD592CNZ or https://www.mouser.com/ProductDetail/584-AD592ANZ Much less expensive and higher accuracy component - newer version of the AD590. It has three terminals, but only two are used. I've used these with my GTX330ES and my uAvionix AV30E with excellent effect - both accuracy and weight of my wallet! On my LongEZ, The probe is wrapped in 2 layers of heat shrink and RTV'd in the gear well with about 3/4" protrusion. ANZ is +/- 2.5C, BNZ is +/- 1.0C and the CNZ is +/- .5C. The Davtron probe is +/- 2.5C (AD590KH) Andy Read this topic online here: http://forums.matronics.com/viewtopic.php?p=507438#507438


    Message 4


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    Time: 05:52:47 PM PST US
    From: Jared Yates <email@jaredyates.com>
    Subject: Re: OAT Probes for Garmin Transponder
    Thanks everybody, this is a big help! I read further and found that the Dynon probe is resistive, whereas these little ICs are a current source. On July 10, 2022 16:07:12 "andymeyer" <meyerkc135@gmail.com> wrote: > > Use this: AD592 from Mouser > https://www.mouser.com/ProductDetail/584-AD592CNZ or > https://www.mouser.com/ProductDetail/584-AD592ANZ > > Much less expensive and higher accuracy component - newer version of the > AD590. It has three terminals, but only two are used. I've used these with > my GTX330ES and my uAvionix AV30E with excellent effect - both accuracy and > weight of my wallet! > > On my LongEZ, The probe is wrapped in 2 layers of heat shrink and RTV'd in > the gear well with about 3/4" protrusion. > > ANZ is +/- 2.5C, BNZ is +/- 1.0C and the CNZ is +/- .5C. > The Davtron probe is +/- 2.5C (AD590KH) > > Andy > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=507438#507438 > >




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