The aircraft wing with the good anti-icing effect comprises a wing body and an icebreaking mechanism, the icebreaking mechanism comprises a containing groove, a pneumatic belt, a connector, an inflation pump, a bottom plate and a first fixing bolt, the icebreaking mechanism is arranged on the upper surface of the wing body, and a deicing mechanism is arranged on the upper surface of the wing body. When the wing needs to be deiced, a first placement groove is formed in the upper surface of the wing, a pneumatic belt is fixedly connected to the inner side surface of the first placement groove and can be completely stored in the first placement groove, a connector is fixedly connected to the surface of one end of the pneumatic belt, and gas can be input into the pneumatic belt through the connector; the surface of one end of the connector is fixedly connected with an inflator pump, air can be conveyed to the pneumatic belt by starting the inflator pump, the surface of one side of the inflator pump is fixedly connected with a bottom plate, and the inflator pump and the wing are fixed together by rotating a first fixing bolt, so that the deicing effect on the wing is achieved.

    本发明提供一种防冰效果好的飞机机翼,包括有机翼和破冰机构,其中破冰机构包括有放置槽、气动带、接口、充气泵、底板和第一固定螺栓,所述机翼的上方表面设置有破冰机构,所述机翼的上方表面设置除冰机构。当机翼需要除冰时,机翼的上方表面开设有第一放置槽,第一放置槽的内侧表面固定连接有气动带,气动带可以完全收纳在第一放置槽内部,气动带的一端表面固定连接有接口,可以通过接口对气动带输入气体,接口的一端表面固定连接有充气泵,开启充气泵可以对气动带进行输气,充气泵的一侧表面固定连接有底板,旋转第一固定螺栓将充气泵与机翼固定在一起,这样就完成了对机翼的除冰效果。


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    Titel :

    Aircraft wing with good anti-icing effect


    Weitere Titelangaben:

    一种防冰效果好的飞机机翼


    Beteiligte:
    LIU XIAOGANG (Autor:in) / YANG DINGMING (Autor:in) / ZHAO CHENXI (Autor:in) / WANG ZHONGYI (Autor:in)

    Erscheinungsdatum :

    2023-08-08


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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




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