Method for generating hydraulic power in an aircraft, use of a hybrid power control unit and drive system

A method for generating hydraulic power in an aircraft, the aircraft having a drive system comprising at least one transmission shaft connected to a power control unit, the power control unit having an electric motor and a hydraulic displacement machine connected to a differential gear unit for driv...

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Bibliographische Detailangaben
Hauptverfasser: HEINTJES MARK, FLEDDERMANN ANDREAS
Format: Patent
Sprache:eng
Schlagworte:
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