Power management system and control for hybrid electric aircraft

A hybrid gas turbine engine for use on board an aircraft includes a motor/generator and a gas turbine engine placed in parallel power communication with a rotating blade component, such as an aircraft propeller, through a combination gearbox. A motor/generator may be used to power the propeller. The...

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Bibliographische Detailangaben

Hauptverfasser:	GRAZIANO KEVIN RICHARD, KUMAR VINOD
Format:	Patent
Sprache:	chi ; eng
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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