AeroElectric-List Digest Archive

Tue 07/27/04


Total Messages Posted: 3



Today's Message Index:
----------------------
 
     1. 08:05 AM - Re: Possible OV condition with Z 16 diagram (Robert L. Nuckolls, III)
     2. 11:39 AM - Strobe lamp wiring question ()
     3. 11:00 PM - handheld and intercom (Jim and Lucy)
 
 
 


Message 1


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    Time: 08:05:50 AM PST US
    From: "Robert L. Nuckolls, III" <rnuckolls@aeroelectric.com> ?
    Subject: Re: Possible OV condition with Z 16 diagram
    ? --> AeroElectric-List message posted by: "Robert L. Nuckolls, III" <rnuckolls@aeroelectric.com> ? At 10:08 PM 7/24/2004 +0200, you wrote: >--> AeroElectric-List message posted by: > >Hi Bob and all, > >The completion of our four seater is not far now, and the time will come for >the first start up. >We have a Rotax 914 wired as per fig Z 16 with dual battery. Some fellow >builders have already flown their own projects, and have been aware of a >possible snag with the OV wiring and the Rotax regulator as well as the >Schicke GR4 regulator. They have been experiencing alarming OV conditions on >shutdown. How do they know there has been an OV condition? >Scenario : >According to fig Z 16 the regulator "sense" wire (C wire) is connected to >the bus through the S700-2-10 master switch. When one opens the master or >the OV module fires, the sense wire sees zero volt. >The regulator then throws the full alternator output at the capacitor >through the wires B and R. The capacitor is rated for 25 volts and could >suffer from the 60-100 volts. Have they measured a 60-volt plus event? >The scenario is quite similar with the Schicke regulator. Are they turning the switch off during high engine rpm operation? Those PM alternators don't put out much at idle and the alternator switch not normally operated at high rpms. This is a situation similar to that which precipitated the great load-dump investigation a few months ago. If switches are operated like you would 99.99% of the time preflighting or parking the airplane, there is little or no risk of the even happening. >To prevent this condition one could connect the sense wire (C wire) directly >to the capacitor, and not to the master switch. Thus the regulator always >sees a load and no ill effect is produced when the master is opened. > >What is your opinion about this variation on the Z 16 theme ? Doable, not >doable ? Give it a try. I don't think there's any risk to the hardware but given that perhaps a hundred plus airplane are flying with Figure Z-16 wiring, I'm interested in figuring out the details of the observed event and deducing why it took so long to surface. In conversations with Rotax ten years ago I was told that opening the "C" lead shuts the alternator OFF. Precipitation of a high voltage event was not mentioned. We need to explore this. Perhaps something about your regulator is different than the original regulators supplied with the Rotax. Bob . . . ---


    Message 2


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    Time: 11:39:20 AM PST US
    From: <chaztuna@adelphia.net>
    Subject: Strobe lamp wiring question
    --> AeroElectric-List message posted by: <chaztuna@adelphia.net> Bob & Listers, What is your opinion of the shielded strobe lamp to power supply wire which was supplied with my Nova strobe system? This shielded 3 lead wire harness is listed as 60 degree Centigrade (140 F) rated wire. The number E129931 is imprinted on the outer casing. Is this wire's temp rating adequate for use in hot climates? Is there any advantage to replacing this wire with MIL 27500 wire? (I have both) Is there any practical advantage with regards to shielding, of one of these wire types as opposed to the other? Charlie Kuss RV-8A cockpit wiring & systems Boca Raton, Fl.


    Message 3


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    Time: 11:00:37 PM PST US
    From: Jim and Lucy <jpollard@mnsi.net>
    Subject: handheld and intercom
    --> AeroElectric-List message posted by: Jim and Lucy <jpollard@mnsi.net> Looking through the installation manual for a NAT intercom,It shows the push to talk switch grounds one of the pins on the intercom which grounds one of the pins on the radio to put it into the transmit mode. If I use a handheld radio in place of a panel mount radio, do these handhelds work the same?? Is the airframe ground the same as the handheld ground to activate the transmitter? If the handheld was operating off internal batteries I don't see how it could be. I have not picked out a handheld radio yet but that is the way I would like to go. thanks Jim Pollard ch601hds wireing and plumbing




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