FIELD: electricity.
SUBSTANCE: electric circuits of distribution for loads of high capacity specific for an aircraft of a "tap lead free" type, and electric circuits of distribution for regular loads, including technical loads, aviation electronic equipment, lighting, fuel pumps and commercial loads, are separated and receive supply from separate generators (SG-B, SG-Y; SG-G1, SG-G2), driven by engines of the aircraft (Eng1, Eng2).
EFFECT: simplification and lightening of energy distribution system design.
29 cl, 6 dwg
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Authors
Dates
2012-10-20—Published
2007-10-25—Filed