The invention relates to the field of ornithopters, in particular to a pure electric vertical take-off and landing high-capacity aircraft with foldable double flapping wings, which comprises a fuselage, a cockpit is arranged at the top of the front end of the fuselage, double rows of flapping wings are arranged on two sides of the top of the fuselage in a front-back manner, and a plurality of side rotors are arranged on two sides of the fuselage and positioned below the flapping wings. A plurality of tail rotors are arranged at the tail end of the fuselage, and a walking device is arranged below the fuselage. The aircraft is reasonable in structure, large in capacity, large in space and high in loading capacity, the aircraft body is made of light materials such as titanium alloy and carbon fibers, the dead weight can be effectively reduced, the loading capacity can be effectively improved, the double-row flapping wings fully utilize aerodynamic force, multiple functions of flight are improved, the flight efficiency is improved, and the double-row flapping wings are folded, so that the aircraft is more convenient to fold and unfold.
本发明涉及扑翼飞行器领域,具体是指一种具有可折叠双扑翼的纯电动垂直起降大容量飞行器,包括机身,所述机身的前端顶部设有驾驶舱,所述机身顶部两侧设有前后设置的双排扑翼,所述机身两侧位于扑翼下方设有若干侧旋翼,所述机身的尾端设有若干尾旋翼,所述机身下方设有行走装置。本发明结构合理,大容量,大空间,载重能力强,机体采用钛合金、碳纤维等轻质材料,能够有效减少自重,提高载重,双排扑翼充分地利用空气动力,提高了飞行多项功能及提高了飞行效率,双排扑翼折叠,使得收放更为方便。
Pure electric vertical take-off and landing high-capacity aircraft with double foldable flapping wings
一种具有可折叠双扑翼的纯电动垂直起降大容量飞行器
30.08.2024
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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