The invention relates to the technical field of manned aircrafts, in particular to a pure electric manned short-distance take-off and landing bionic flapping-wing aircraft which comprises an aircraft body, two foldable main flapping wings, two auxiliary flapping wings, an empennage, two side rotor wings, two rear rotor wings, a cockpit and a ground traveling device. Rotor wing cabins are arranged on side rotor wings on the fuselage, the ground traveling device adopts rollers to travel and is provided with roller retracting cabins, and the power system is purely electrically driven. The invention has the advantages of reasonable and compact structure, convenience in operation, convenience in short-distance flying and landing, folding design of the main flapping wings, reduction of space occupation, adoption of a pure electric power system, energy consumption saving, adoption of clean energy and facilitation of environmental protection.

    本发明涉及载人飞行器技术领域,具体是指一种纯电动可载人短距起降的仿生扑翼飞行器,包括机身、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、驾驶舱和地面行驶装置,机身上侧旋翼配置有旋翼舱、地面行驶装置采用滚轮行驶并配置有滚轮收放舱,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,主扑翼折叠设计,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 manned bionic flapping wing aircraft capable of taking off and landing in short distance


    Additional title:

    一种纯电动可载人短距起降的仿生扑翼飞行器


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

    Publication date :

    2024-05-31


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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