nuckolls.bob(at)aeroelect Guest
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Posted: Thu May 13, 2021 7:26 pm Post subject: Primary and B/U Alt Fields on Master Bus |
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At 04:43 PM 5/13/2021, you wrote:
Figure Z-13 shows the optimal application of
the diminutive SD-8 into a two alternator
system. On of the design goals was to
eliminate the battery contactor load of
approx 0.6 to 0.8 amps when flying on
battery only. Eliminating that load was
also useful for maximizing available
energy from the SD-8.
If you're not going to have an e-bus,
the tie both alternators to the main bus
as depicted in Z-12.
Have you done a load analysis of the
easily anticipated failure conditions
for formulate your plan-b
flight configuration?
Bob . . .
Un impeachable logic: George Carlin asked, "If black boxes
survive crashes, why don't they make the whole airplane
out of that stuff?"
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