The invention relates to the technical field of aviation, in particular to an aircraft wing with a deicing function and a deicing method thereof, and the aircraft wing comprises a wing assembly, a cam and a driving assembly; the wing assembly comprises a first wing, a second wing and a rotating shaft assembly, the rotating shaft assembly is connected with the first wing and the second wing, the driving assembly is connected with the second wing, and the output end of the driving assembly is connected with the cam; a cam groove is formed in the first wing, and the cam is arranged in the cam groove; when the driving assembly drives the cam to rotate in the cam groove, the first wing moves around the rotating shaft assembly, so that an ice layer on the wing assembly is removed. The unmanned aerial vehicle has the advantages that the cam is driven by the driving assembly, so that the first wing generates fluctuating vibration, and shearing force and vibration force generated by the vibration can rapidly break an ice layer attached to the wing assembly.

    本发明涉及航空技术领域,尤其涉及一种具有除冰功能的飞行器机翼及其除冰方法,飞行器机翼包括机翼组件、凸轮和驱动组件;机翼组件包括第一机翼、第二机翼和转动轴组件,转动轴组件连接第一机翼和第二机翼,驱动组件与第二机翼相连,驱动组件的输出端与凸轮相连;第一机翼内设有凸轮槽,凸轮设置于凸轮槽内;当驱动组件驱动凸轮在凸轮槽内转动时,第一机翼绕转动轴组件运动,从而去除机翼组件上的冰层。本发明的优点在于,通过驱动组件驱动凸轮,使第一机翼产生起伏震动,这种震动产生的剪力和震动力能够迅速破碎结在机翼组件上的冰层。


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    Title :

    Aircraft wing with deicing function and deicing method thereof


    Additional title:

    具有除冰功能的飞行器机翼及其除冰方法


    Contributors:
    WANG YUEHAO (author) / BAI YUE (author) / XU JIAHUI (author) / PEI XINBIAO (author) / FU YUTONG (author) / CHEN DIANXIN (author)

    Publication date :

    2025-04-25


    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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