The invention relates to the technical field of manned aircrafts, in particular to a pure electric short-distance take-off and landing manned folding soft flapping wing aircraft which comprises an aircraft body, a cockpit, two foldable main flapping wings, two auxiliary flapping wings, an empennage, two side rotor wings, two rear rotor wings and a ground traveling device. And the ground running device runs by adopting rollers, and the power system is purely electrically driven. The unmanned aerial vehicle is reasonable and compact in structure, convenient to operate and convenient for short-distance flying and landing, the main flapping wings are folded in the left-right direction, occupied space is reduced, a pure electric power system is adopted, energy consumption is reduced, clean energy is adopted, and environmental protection is facilitated.

    本发明涉及载人飞行器技术领域,具体是指一种纯电动短距起降可载人的折收软性扑翼飞行器,包括机身、驾驶舱、两个能够折叠的主扑翼、两个副扑翼、尾翼、两个侧旋翼、两个后旋翼和地面行驶装置,主扑翼能够上下扑动,也能够在左右方向上实现收折,地面行驶装置采用滚轮行驶,动力系统采用纯电驱动。本发明结构合理,结构紧凑,运行方便,便于短距离飞降,主扑翼在左右方向上收折设计,减少空间占用,采用纯电动力系统,节省能耗,采用清洁能源,有利于环境保护。


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    Title :

    Pure electric short-distance take-off and landing manned folding soft flapping wing aircraft


    Additional title:

    一种纯电动短距起降可载人的折收软性扑翼飞行器


    Contributors:
    LI AOFAN (author) / LI YIPING (author)

    Publication date :

    2024-08-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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