Wing structure of fixed-wing vertical take-off and landing electric aircraft and aircraft

The utility model discloses a wing structure of a fixed wing vertical take-off and landing electric aircraft, which comprises a skin, a plurality of wing rib plates, tubular beams and support rods, through holes with the same number are formed in the wing rib plates, the tubular beams penetrate thro...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	LI JUNJUN, TANG XIAOMING, LYU JINZE, FANG YIWU, CHEN XIUXIAN, PEI JIANXUN, LI SHICHUN
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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