B - Operations – Transporting – 64 – D
Patent
B - Operations, Transporting
64
D
B64D 41/00 (2006.01)
Patent
CA 2741382
An electrical power distribution system (21) for an aircraft comprises a power source (12) electrically connected to an electrical load (14) and at least one circuit interruption device for interrupting current in the power distribution system (21). A distinguishing device (23) is connected to the system (21) for distinguishing a transient electrical event (15) in the system from a steady-state level of electrical activity in the system, wherein the transient electrical event (15) induces a potential difference across all or part of the distinguishing device (23). The circuit interruption device is operable to interrupt current flowing through the power distribution system (21) if the potential difference across the distinguishing device (23) exceeds a threshold voltage.
Craig Wilson And Company
Ge Aviation Systems Limited
LandOfFree
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