POWER CONTROL UNIT, HYDRAULIC SYSTEM AND AIRCRAFT USING THE SAME

A power control unit configured to supply hydraulic pressure and mechanical torque. To this end, the power control unit includes an electric motor coupled to a differential output transmission and a hydraulic pump. A switchable transmission device allows the torque of the motor to be redirected eith...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	LAMOUSSIERE, Xavier, FLEDDERMANN, Andreas, DIDEY, Arnaud
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
Online-Zugang:	Volltext bestellen
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