Propulsion unit for an aircraft and its control procedure

Fluid reaction surfaces (i.e. – impellers) – Interrelated controls for impeller and drive means – Pitch adjustment and throttle regulation with condition...

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416 27, 416 28, 416 29, 416 36, 416 37, 416 38, 416 47, 416 48, 416157R, B63H 310

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active

06004098&

ABSTRACT:
An engine plant for aircraft comprising a multicylinder internal combustion engine (1) whose crankshaft drives an adjustable pitch propeller (5), mechanisms for adjusting the engine speed and a common power stick (4) that controls the operation of the engine and of the adjustment mechanisms, characterized in that said engine is a compression ignition engine (1) that cooperates with an electronic control system (3) controlling the quantity of the fuel injected.

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patent: 5810560 (1998-09-01), Tanaka

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