The invention provides a streamline type quick-launching trajectory six-rotor aircraft. The streamline type quick-launching trajectory six-rotor aircraft comprises an aircraft body and a trajectory launching device, the aircraft body comprises a central rigid body, a plurality of aircraft arms, undercarriages and propellers, one ends of the aircraft arms are mounted on the central rigid body, the propellers facing downwards are mounted at the other ends of the aircraft arms, and the undercarriages are mounted at the bottom of the central rigid body; mounting plates are respectively arranged at the middle upper part and the bottom of the central rigid body, and all parts of the central rigid body are connected through supporting columns. The pneumatic catapulting mechanism has the beneficial effects that a pneumatic catapulting mode is adopted, and the catapulting mechanism is stable, reliable, controllable, low in cost and extremely high in applicability and practicability; the transition of the aircraft arms from the folded state to the unfolded state is realized by the control of the designed spring slide block release mechanism, the flight resistance can be effectively reduced, the folding undercarriage is adopted to replace a fixed undercarriage, and the anti-interference capability of the six-rotor aircraft is improved.

    本发明创造提供一种流线型快速发射弹道六旋翼飞行器,包括机体和弹道发射装置;所述机体包括中心刚体、若干根机臂、起落架和螺旋桨,所述机臂的一端安装在所述中心刚体上,所述机臂的另一端安装方向朝下的螺旋桨,所述起落架安装在所述中心刚体底部;所述中心刚体的中上部和底部分别设置有安装板,所述中心刚体的各个部分通过支撑柱连接。本发明创造的有益效果是:本发明采用气动弹射方式,该种弹射机构稳定、可靠、可控而且成本低,具有极强的适用性和实用性;飞行器机臂从折叠状态到展开状态的过渡由设计的弹簧滑块释放机构控制来实现,可以有效地减少飞行阻力,采用折叠式起落架代替固定式起落架,提高了六旋翼飞行器抗干扰能力。


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    Title :

    Streamline type rapid launching trajectory six-rotor aircraft


    Additional title:

    一种流线型快速发射弹道六旋翼飞行器


    Contributors:
    WU TAO (author) / XIAO HAIJIAN (author) / YANG CHUNKAI (author) / DING ZIHANG (author) / LI JIANFENG (author) / ZHANG XINZE (author) / ZHENG YUCHEN (author) / XING KONGRUI (author) / LIU XINGLONG (author) / SONG TIANQIN (author)

    Publication date :

    2024-06-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U



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