The invention provides an aircraft comprising a fuselage provided with a first wing with a curved wingtip above a second wing provided with the curved wingtip. The rotor assembly is located between the bent wingtips of the first wing and the second wing, can provide vertical thrust for vertical take-off of the aircraft, and can also automatically rotate to generate electric energy to charge an airborne power supply. The first wing may be V-shaped, and the rotatable canard may be provided with an additional rotor assembly to provide forward and vertical thrust to the aircraft.
本发明提供了一种飞行器,包括机身,该机身设有第一机翼,带有弯曲翼尖,位于设有弯曲翼尖的第二机翼上方。转子组件位于第一机翼和第二机翼的弯曲翼尖之间,既可为飞行器垂直起飞提供垂直推力,也可自动旋转以产生电能,为机载电源充电。第一机翼可为V形,可旋转的鸭翼上可以设有额外的转子组件,向飞行器提供向前和垂直推力。
Aircraft with wing tip-located propellers
带有位于翼尖的螺旋桨的飞行器
2022-09-30
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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