POWER DISTRIBUTION SYSTEM FOR AN AIRCRAFT
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United States of America Patent
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Oct 4, 2013
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Oct 4, 2013
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Abstract
An aircraft power distribution system (22) includes at least one DC power source, a first DC power distribution bus and a second DC power distribution bus (36), a tie bus (33) coupling the at least one DC power source, first DC power distribution bus, and second DC distribution bus, wherein the first or second DC power distribution buses are selectively coupled and decoupled to the tie bus by means of a solid-state poer controller (SSPC) (46, 48, 62, 64, 66).
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