AeroElectric-List Digest Archive

Sat 09/23/23


Total Messages Posted: 5



Today's Message Index:
----------------------
 
     1. 03:15 PM - Re: Potential for Overvoltage Issue (Robert L. Nuckolls, III)
     2. 03:33 PM - Re: OVM14 MkIII, rev P1 (user9253)
     3. 04:49 PM - Re: Re: OVM14 MkIII, rev P1 (Robert L. Nuckolls, III)
     4. 04:52 PM - Re: Re: OVM-14 MkIII (Robert L. Nuckolls, III)
     5. 04:54 PM - Re: Re: Practical data acquisition (Robert L. Nuckolls, III)
 
 
 


Message 1


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    Time: 03:15:47 PM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Potential for Overvoltage Issue
    At 03:39 PM 9/22/2023, you wrote: >I've been luring on this list for years and this is my first post. >I've recently completed my plane (Tailwind) and have if flying. >I used the previous version of the OVM crowbar circuit and I have >modified an automotive alternator to use an external Ford-type >voltage regulator. >All is working well. But, in going through a FMEA in my mind I have >identified a potential issue: I modified the alternator using the >method in Kitplanes, November 2019. >In this method one of the brush terminals is isolated with >insulating washers and an insulating sleeve. In my case I have >grounded the other brush to case ground. The issue is that if ever >the insulating washer or sleeve were breached the B--lead would >directly feed the field through the brush and an overvoltage would >result that the crowbar could not shut down. Turning off the master >switch would disconnect the battery but the run away alternator >would still be feeding the bus. >I post this in case anyone else has this setup. Yes they do . . . along with about every single engine airplane since 1968 or so. FMEA also takes into account probability of any particular event. Many potentially catastrophic events in aviation are statistically or demonstrably so small as to be ignored in process of crafting a plan-b, or redesigning to remove potential for the fault entirely. Number one failure of a wiring pathway is disconnect. Wire breaks, stud nut is works loose, wire pulls out of terminal crimp, etc. Another root cause for failure is short to ground due to compromised wire insulation (chaffing or mechanical damage). The probability of an wire becoming disconnected followed by a low-impedance, re-positioning of that wire to a robust power source is really TWO failures happening simultaneously. Original structural failure followed by misadventurous 'wandering' of that same wire to a hazardous source of power. This combination of events is so remote that it has not been treated as potentially hazardous in hundreds of thousands of airplanes from Super Cubs to Gulfstream V's You are to be commended for considering the scenario and asking the question. Be assured that the question has been considered and discounted countless times before. Bob . . . //// (o o) ===========o00o=(_)=o00o======== < Go ahead, make my day . . . > < show me where I'm wrong. > ================================ In the interest of creative evolution of the-best-we-know-how-to-do based on physics and good practice.


    Message 2


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    Time: 03:33:31 PM PST US
    Subject: Re: OVM14 MkIII, rev P1
    From: "user9253" <fransew@gmail.com>
    I think that most people would expect the crowbar overvoltage device to trip the breaker when the push-to-test button is pressed, regardless of whether the alternator is running or not, especially during an annual condition inspection by a mechanic or new owner. -------- Joe Gores Read this topic online here: http://forums.matronics.com/viewtopic.php?p=511479#511479


    Message 3


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    Time: 04:49:09 PM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: OVM14 MkIII, rev P1
    At 05:33 PM 9/23/2023, you wrote: > >I think that most people would expect the crowbar overvoltage device to trip >the breaker when the push-to-test button is pressed, regardless of whether >the alternator is running or not, especially during an annual >condition inspection >by a mechanic or new owner. The product would be supplied with instructions calling out a procedure for validating continued airworthiness. Leave the button off if you will. Do not label it anything. At a propitious time verification procedures say, join the two wires together. Start the engine leaving alternator OFF. Field breaker should remain closed. Turn alternator ON. Breaker should open. Shut down engine. Disconnect the two wires and secure for service. The procedure not only verifies gross functionality but makes a good ball- park check of calibration. A push button precludes inadvertently leaving them together . . . but you'd know about it early on when the alternator fails to stay on line . . . so it's pretty much fail-passive either way. Bob . . . //// (o o) ===========o00o=(_)=o00o======== < Go ahead, make my day . . . > < show me where I'm wrong. > ================================ In the interest of creative evolution of the-best-we-know-how-to-do based on physics and good practice.


    Message 4


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    Time: 04:52:43 PM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: OVM-14 MkIII
    >I looked at the proposed circuit, but didn=99t >study it, and in not studying, didn=99t grok it >' I can look at the simplest of scchematics for >an eternity and still not get it.=C2 Not pairing >the words with the proposed schematic, I >imagined one light, multiple functions (I seem >to remember a device (LR3x, maybe?) =C2 that could >set a lamp ON for over-voltage, blinking for low voltage). Does it really do that? All the data I have here says that light is ALWAYS flashed and ONLY in response to a detected low voltage. Due to the nature of LR3 crowbar ov protection, an OV event is followed milliseconds later by a LV event. There would not be any time to sense, display and perceive an OV condition. Bob . . . //// (o o) ===========o00o=(_)=o00o======= = < Go ahead, make my day . . . > < show me where I'm wrong. > ======================== ======== In the interest of creative evolution of the-best-we-know-how-to-do based on physics and good practice.


    Message 5


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    Time: 04:54:54 PM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Practical data acquisition
    >> >> . . >Thanks Bob. But let me start a new thread (subject) when I've pulled >the cowling and taken some pictures. > >Finn Found the Kitplanes piece. I understand at least some of your concerns. I have a lengthy reply in process. Those DIY open loop current sensors are problematic. Economical manufactured alternatives are available. Watch this space. Bob . . . //// (o o) ===========o00o=(_)=o00o======== < Go ahead, make my day . . . > < show me where I'm wrong. > ================================ In the interest of creative evolution of the-best-we-know-how-to-do based on physics and good practice.




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