AN OPEN-CLOSE WING STRUCTURE OF A COMBINATION-DRIVE FLAPPING-WING AIRCRAFT

The present invention discloses an open-close wing structure of a combination-drive flapping-wing aircraft, comprising a wing body and a primary feather blade group and a secondary feather blade group disposed on the same side of the wing body, wherein each of the primary feather blade group and the...

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Bibliographische Detailangaben
Hauptverfasser:	LI Yibin, XIE Fa, JI Bing, ZHU Qiaolin, SONG Rui, LI Yushuai
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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