The invention relates to the field of aircraft structure design, in particular to a bird impact resisting device applied to aircraft wings, which comprises a bird separating device and an energy absorbing device, the bird separating device is of an isosceles triangle structure, the tip of the bird separating device faces the bird impact direction to divide a bird body, and the energy absorbing device is arranged at one end, away from the tip, of the bird separating device. The two sides, corresponding to the bird separating device, of the energy absorption device protrude outwards in an arc shape so as to absorb kinetic energy of bird bodies. The technical effect of improving the bird impact resistance of the airplane is achieved.

    本申请涉及飞机结构设计领域,为一种应用于飞机机翼的抗鸟撞装置,包括分鸟装置和吸能装置,所述分鸟装置呈等腰三角形结构并且尖端朝向鸟撞击方向以分割鸟体,所述吸能装置设于分鸟装置远离尖端的一端,所述吸能装置对应分鸟装置的两侧向外呈弧形凸起以吸收鸟体动能。具有提高飞机抗鸟撞能力的技术效果。


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    Title :

    Bird impact resisting device applied to aircraft wings


    Additional title:

    一种应用于飞机机翼的抗鸟撞装置


    Contributors:
    GUO JUN (author) / LIU XIAOCHUAN (author) / HUI XULONG (author)

    Publication date :

    2022-01-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

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



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