The invention discloses a method for eliminating the icing phenomenon of aircraft wings through laser heating, and relates to the field of aircraft wing deicing, and the method comprises a fixed housing which is used for limiting the range of light emitted by a light source; the cylindrical lens is located in the middle of one end of the fixed shell; the laser source is located in the middle of the inner side of the fixed shell; the installation fixing mechanisms are located at the upper and lower ends of the cylindrical lens. The device has the beneficial effects that the wing icing phenomenon in the flight process of an aircraft can be effectively removed and prevented, the device is rapid and effective and is not affected by the environment, the structure is easy and convenient to operate, the deicing efficiency is higher than that of a traditional wind power deicing system, the deicing effect is obvious, no dead angle is left, the structure is not affected by the environment, the application range is wide, and the application range is wide. The overall weight of the aircraft can be reduced conveniently due to small size and light weight, and normal flight cannot be affected.

    本发明公开了一种通过激光加热消除飞机机翼结冰现象的方法,涉及飞机机翼消冰领域,包括:固定外壳,用于对光源发出的光线进行范围限定;柱面透镜,位于固定外壳一端的中部;激光光源,位于固定外壳内侧的中部;安装固定机构,位于柱面透镜的上下两端。本发明有益效果是:可有效去除和预防飞机飞行过程中机翼结冰的现象,快捷有效并且不受环境影响,该结构操作简便,除冰效率相较于传统的风力除冰系统要高,除冰效果明显且不留死角,该结构不受环境影响,使用范围广,体积小重量低便于减轻飞机的整体重量,不会影响正常飞行。


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    Titel :

    Method for eliminating icing phenomenon of aircraft wing through laser heating


    Weitere Titelangaben:

    一种通过激光加热消除飞机机翼结冰现象的方法


    Beteiligte:
    ZHANG CHENG (Autor:in)

    Erscheinungsdatum :

    22.11.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    H01S Vorrichtungen, die stimulierte Emission verwenden , DEVICES USING STIMULATED EMISSION / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT




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