METHOD OF AUTOMATIC CONTROL OF TURBO-PROP ENGINE Russian patent published in 1994 - IPC

Abstract SU 1759070 A1

FIELD: aviation. SUBSTANCE: control of fuel consumption of the engine transitional modes of operation is exercised under condition, that given reading of turbine compressor rotor acceleration is maintained and control of blade of propeller setting angle is exercised provided, that given pace of thrust change is being kept. EFFECT: method is used to control turbo-prop engines operations automatically. 1 dwg

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SU 1 759 070 A1

Authors

Kulikov G.G.

Fatikov V.S.

Svitskij O.L.

Pisarenko A.V.

Karimov I.A.

Khasanov V.A.

Dates

1994-07-15—Published

1989-07-10—Filed