Generator drive control system

Electricity: single generator systems – With physical starting and/or stopping of the generator – Connecting and/or disconnecting generator and driving means

Patent

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Details

192 67R, 192114R, 244194, 307 84, F16D 1322, H02P 906

Patent

active

041676955

ABSTRACT:
The system is intended primarily for use in multi-engined aircraft although it has great utility in any installation having an engine and a generator driven thereby. A kit for each engine includes a generator drive train connected to the engine to be driven thereby, a driving formation for connection to a generator, and a coupling or clutch in the drive train to decouple the generator in case of mechanical or electrical failure. Signal means may be located in the cockpit in the pilot's field of view to indicate generator failure. A switch operable by the pilot in response to the failure signal acts to remotely cause decoupling of the generator. The active signal operates means to deactivate any other decoupling switch to prevent mistakenly decoupling a properly functioning generator. Cross-connection switch means are connected to all engines and generators and may be actuated to electrically connect an active generator to the engine having the decoupled generator.

REFERENCES:
patent: 2482812 (1949-09-01), Treseder
patent: 2700124 (1955-01-01), Fritz
patent: 2803323 (1957-08-01), Newell
patent: 3080031 (1963-03-01), Young
patent: 3723750 (1973-03-01), Dixon et al.

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