The disclosure relates to a component tail end structure and a preparation method thereof, an aircraft and an aircraft component. The component tail end structure comprises an upper paving layer structure and a lower paving layer structure, the upper paving layer structure comprises an upper paving layer tail end structure and an upper paving layer front end structure, the upper paving layer tailend structure is a metal edge covering structure, and the upper paving layer front end structure is a composite material laminated plate. The component tail end structure has the composite material lightning stroke 1B area protection capability, and can bear the 1B area lightning stroke without influencing the noise reduction function and the weight without being damaged.

    本公开涉及一种部件末端结构及其制备方法、飞行器和飞行器部件。该部件末端结构包括:上铺层结构和下铺层结构,其中,上铺层结构包括上铺层末端结构和上铺层前端结构,其中,上铺层末端结构为金属包边结构,上铺层前端结构为复合材料层合板。本公开部件末端结构具有复合材料雷击1B区防护能力,可在不影响降噪功能和重量的情况下承受1B区雷击而不被破坏。


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    Title :

    Component tail end structure and preparation method thereof, aircraft and aircraft component


    Additional title:

    部件末端结构及其制备方法、飞行器和飞行器部件


    Contributors:
    ZHAO TIAN (author)

    Publication date :

    2021-01-12


    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 / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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