POWER SYSTEM

A power system for an aircraft comprises: a first motor-generator component; a second motor-generator component; a common shaft, wherein the first and second motor-generator components are connected to the common shaft in series; and a de-coupler operable to disconnect the first motor-generator comp...

Ausführliche Beschreibung

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Bibliographische Detailangaben
1. Verfasser:	TATE, David James
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	A power system for an aircraft comprises: a first motor-generator component; a second motor-generator component; a common shaft, wherein the first and second motor-generator components are connected to the common shaft in series; and a de-coupler operable to disconnect the first motor-generator component from the common shaft.