The invention discloses an independent suspension damping device of an unmanned aerial vehicle nozzle, comprising a wing and a nozzle. A fixing assembly is arranged at the bottom of the wing. One sideof the fixing assembly is sleeved with a fixing cylinder. The nozzle is arranged in the fixing cylinder. The fixing assembly is composed of flexible fixing parts and a clamping part which are weldedto each other. A square groove is formed in the bottom of the wing, and the clamping part is movably connected with the square groove. Inflatable deformation pipes are evenly arranged in the fixing cylinder. External threads are arranged on the flexible fixing parts, internal threads are arranged at the ends of the fixing cylinder, and the external threads and the internal threads are connected ina threaded mode. The inflatable deformation pipes are arranged between the two flexible fixing parts and connected with an external air source. Air bag extrusion grooves are evenly formed in the fixing cylinder, and air bags are arranged in the inflatable deformation pipes in a folded mode. The independent suspension damping device has the advantages of being diversified in function and capable of preventing rollover.

    本发明公开了一种无人机喷管的独立悬挂减震装置,包括机翼和喷管,所述机翼的底部设置有固定组件,所述固定组件的一侧套接有固定筒体,所述喷管设置在固定筒体的内部,所述固定组件由相互焊接的柔性固定部和卡接部组成,所述机翼的底部开设有方形槽,所述卡接部与方形槽活动连接,所述固定筒体的内部均匀设置有充气变形管,所述柔性固定部上设置有外螺纹,所述固定筒体的端部设置有内螺纹,所述外螺纹与所述内螺纹相互螺接,所述充气变形管设置在两个柔性固定部之间,所述充气变形管与外界气源连接,所述固定筒体上均匀开设有气囊挤出槽,充气变形管的内部呈折叠状设置有气囊,本发明,具有功能多样和防止侧翻的特点。


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    Title :

    Independent suspension damping device of unmanned aerial vehicle nozzle


    Additional title:

    一种无人机喷管的独立悬挂减震装置


    Contributors:
    YU SHUN (author)

    Publication date :

    2020-04-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

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




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