Security electrical power distribution systems for light aircraf

Details Security electrical power distribution systems for light aircraf Security electrical power distribution systems for light aircraf

1982-01-20

1983-12-06

Moose, Jr., Harry E.

Electrical transmission or interconnection systems

Vehicle mounted systems

307 18, 361 66, H02J 906

Patent

active

044195885

ABSTRACT:
A security electrical power distribution system for light aircraft equipped for flight on instruments and having at least one navigation system comprising a main instrument and a standby instrument, comprises a battery and a generator. A battery bus and a generator bus are connected to respective instruments of the or each navigation system. A remote-controlled circuit-breaker interconnects these buses. A fault detector has two control inputs connected to respective terminals of the circuit-breaker. It also has one power feed input connected to the battery and another power feed input connected to the generator. The system also includes a single fault indicator and a module monitoring the generator output voltage. The fault indicator is operative in response to input from the fault detector or the monitor module.

REFERENCES:
patent: 2832896 (1958-04-01), Stineman et al.
patent: 3041465 (1962-06-01), Ayre
patent: 3379893 (1968-04-01), Cavanaugh

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