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US 4,466,526 AGranted
Helicopter engine control with rotor speed decay anticipator
AssigneeChandler Evans Inc.
InventorsJames J. Howlett, Raymond D. Zagranski
Life of this patent
Estimating the term…
Abstract
The speed (54, 56) of the free turbine (40) of a helicopter engine (20) is compared (103) with the speed (105, 106) of the helicopter rotor (10) to indicate (101, 102) autorotation, and the deceleration (108) of the rotor above a threshold magnitude (110) is utilized (81, 68, 69) to increase fuel flow (72) to the engine in anticipation of rotor speed droop which would otherwise occur during recovery from the autorotation maneuver.
Claims3
A helicopter, comprising:
- a rotor;
- an engine;
- rotor drive means including an overrunning clutch for connecting said rotor to said engine whenever the speed of said rotor does not exceed the speed of said engine;
- and
- engine control means for providing an engine speed signal indicative of the rotary speed of said engine, for providing a fuel command signal indicative of fuel flow required for desired engine operation, and for metering fuel flow to said engine in response to said fuel command signal;
- characterized by:
- rotor speed means for providing a rotor speed signal indicative of the rotary speed of said rotor;
- and
- said engine control means comprising means for providing, in response to said rotor speed signal, a rotor deceleration signal indicative of the deceleration of said rotor in excess of a predetermined threshold deceleration, for providing an autorotation signal indicative of said rotor being declutched from said engine, and for providing said fuel command signal with a fuel increase-indicating component in response to said rotor deceleration signal.
6 more elements
A helicopter, comprising:
- a rotor;
- an engine;
- rotor drive means including an overrunning clutch for connecting said rotor to said engine whenever the speed of said rotor does not exceed the speed of said engine;
- and
- engine control means for providing an engine speed signal indicative of the rotary speed of said engine, for providing a fuel command signal indicative of fuel flow required for desired engine operation, and for metering fuel flow to said engine in response to said fuel command signal;
- characterized by:
- rotor speed means for providing a rotor speed signal indicative of the rotary speed of said rotor;
- and
- said engine control means comprising means for providing, in response to said rotor speed signal, a rotor deceleration signal indicative of the deceleration of said rotor in excess of a predetermined threshold deceleration, for providing an autorotation signal indicative of said rotor being declutched from said engine, and for providing said fuel command signal with a fuel increase-indicating component in response to said rotor deceleration signal in the presence of said autorotation signal and continuing thereafter until the rotor deceleration signal is nearly zero.
6 more elements
Dependencies are inferred from the claim text.