A steel plate is connected to a flapping-wing aircraft, the flapping-wing aircraft launcher comprises a base, a release rod and an angle adjusting assembly, the base comprises a vertical rod, the release rod comprises an electromagnet used for the steel plate, and the angle adjusting assembly is used for adjusting the launching angle of the flapping-wing aircraft. The angle adjusting assembly comprises an angle adjusting rod and two angle adjusting plates, the two sides of the angle adjusting rod are connected with the two angle adjusting plates in an elastic mode respectively, one angle adjusting plate is connected with the vertical rod, and the other angle adjusting plate is connected with the release rod. On the basis that the weight of the aircraft is not obviously increased and the structure of the aircraft is not changed, flexible control of adjustable launching angles is achieved, the requirement for conciseness of the launching process is met, and the method can be suitable for the ornithopters of most sizes and weights.

    本发明涉及扑翼飞行器发射架,其中连接扑翼飞行器设置有钢板,其包括底座,释放杆和角度调节组件,底座包括立杆,释放杆包括用于钢板的电磁铁,角度调节组件用于调节扑翼飞行器发射角,角度调节组件包括角度调节杆和两个角度调节板,角度调节杆的两侧分别与两个角度调节板可松紧连接,其中一个角度调节板与立杆连接,另一个角度调节板与释放杆连接。本发明在没有飞行器明显增加重量及改变结构的基础上,实现发射角可调节的灵活操控,且有利于满足发射流程的简洁性,以及可适用于大多数尺寸和重量的扑翼飞行器。


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    Titel :

    Flapping wing aircraft launcher


    Weitere Titelangaben:

    一种扑翼飞行器发射架


    Beteiligte:
    XU WENFU (Autor:in) / WANG HAOYU (Autor:in) / LI QINGYANG (Autor:in) / PAN ERZHEN (Autor:in)

    Erscheinungsdatum :

    30.01.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U



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