Speed control unit for an aircraft generator

Details Speed control unit for an aircraft generator Speed control unit for an aircraft generator

1986-09-19

1988-03-22

Hickey, R. J.

Electricity: single generator systems

With physical starting and/or stopping of the generator

322 29, 322 40, H02P 1500

Patent

active

047331550

ABSTRACT:
A speed control unit for an aircraft generator includes a continuously variable gear ratio drive device through which the generator is driven by a shaft of the engine and which is responsive to an error signal indicative of a difference between desired and sensed generator speeds. A control circuit prevents the error signal from being applied to the drive device until a predetermined speed of the generator is reached and a ramp generating circuit increases the rise time of the error signal after the generator has reached the predetermined speed.

REFERENCES:
patent: 4278928 (1981-07-01), Griffiths et al.
patent: 4439720 (1984-03-01), Georges
patent: 4572961 (1986-02-01), Borger

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