Propulsion unit for an aircraft and its control procedure
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United States of America Patent
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-
Dec 21, 1999
Grant Date -
N/A
app pub date -
Oct 3, 1997
filing date -
Oct 4, 1996
priority date (Note) -
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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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