Energy optimization configuration method and device of aircraft hybrid electric propulsion system

The embodiment of the invention discloses an energy optimization configuration method and device of an aircraft hybrid electric propulsion system. The method comprises the following steps: setting a flight condition based on an aircraft hybrid electric propulsion system architecture, and establishin...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	ZHANG XIAOBIN, WANG RUNLONG, SONG LINA, LEI TAO, ZHANG XINGYU
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	CALCULATING COMPUTING COUNTING ELECTRIC DIGITAL DATA PROCESSING PHYSICS
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