SYSTEM AND METHOD FOR AIRCRAFT PROPELLER CONTROL

A system (100) and method (500) for controlling an aircraft propeller (30) are provided. In anticipation of a condition in which a parameter related to an angle of a plurality of blades of the propeller (30) reaches a value beyond a predetermined threshold, a first control signal is output comprisin...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	JARVO, James, PEDRAMI, Reza
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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