Hybrid control system across multiple operating modes

A lever for adjusting an output of a hybrid power device of an aircraft includes a lever configured to move over an overall range of positions. Movement of the lever adjusts an output of the hybrid power device between at least two modes of operation. In a first subset of positions within the overal...

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Bibliographische Detailangaben

Hauptverfasser:	CURRIER PAUL, SANTA CRUZ XAVIER GEORGE, ANDERSON RICHARD PAUL, WILSON GREGG, SPITZER, DAVID, N
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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