AeroElectric-List Digest Archive

Fri 11/26/10


Total Messages Posted: 1



Today's Message Index:
----------------------
 
     1. 06:52 AM - Re: Re: Z13/8 Rev Q comments (Robert L. Nuckolls, III)
 
 
 


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    Time: 06:52:39 AM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Z13/8 Rev Q comments
    At 11:07 PM 11/25/2010, you wrote: > >> Okay, 20AWG and no fuses it is. > >So assuming all these wires are 6" or less, should I use 20awg and no >fuses on both the diode and the relay path to the Endurance bus ? I WAS speaking of just the normal feed path through the diode . . . and it occurs to me that the "6-inch rule" would be speaking to TOTAL current pathway at risk . . . so strict observance of the rule would call for very short 20AWG conductors totalling 6" or less to wire the diode up between the main and e-bus. But then, that "rule" was never codified in any regulatory document I recall . . . but that doesn't mean it didn't show up on some FAA offices "green sheets". My citation of that practices goes back a long way. I think I first recall discussing it at Cessna when somebody was contemplating the permanent wiring of a fat zener (50W stud mounted) to the main bus as a transient suppressor. This was before the zener market gave birth to the Transorb. Is the sum total of wire from battery bus to e-bus through the relay must surely be longer. Further, it's primary reason for existence is to power a bus from a battery not being charged by an alternator so we'll not want to squander energy in voltage drops. But it seems that the pathway would benefit from the conventional protection methods at BOTH ends since that wire can be SOURCED either from the main bus or the battery bus. Bob . . .




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