SPEED GOVERNOR OF TURBOJET ENGINE ROTOR WITH AIRCRAFT FLIGHT SPEED CORRECTOR Russian patent published in 1997 - IPC

Abstract RU 2094327 C1

FIELD: aviation; control of number-two flying vehicle provided with TURBOJET engines. SUBSTANCE: speed governor of turbojet engine rotor includes mechanical centrifugal weights, spring, pendulum partially covering the nozzle, piston, metering cock, profiled cam, lever and pusher. Actuator connected with on-board computer is connected to channel through which signal from engine control lever passes to profiled cam. EFFECT: enhanced reliability. 4 dwg

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RU 2 094 327 C1

Authors

Karavaev Jurij Andreevich

Tarmaev Anatolij Anatol'Evich

Dates

1997-10-27—Published

1994-06-10—Filed