The invention discloses an aircraft wing, which comprises a main wing spar, a right side wing and a left side wing, wherein the main wing spar comprises a right side portion, a left side portion and acombination section, the right side wing is arranged on the right side portion, the left side wing is arranged on the left side portion, the combination section is arranged on a containing groove inthe top of an aircraft body of the aircraft, and a top cover and the aircraft body are combined to seal the containing groove. Therefore, the assembling time for assembling the wings can be effectively saved, the assembling procedures can be reduced, errors generated in the assembling process are reduced, and the aircraft has higher safety in the flying process.

    一种飞机的机翼,包括一主翼梁、一右侧翼及一左侧翼,该主翼梁包括一右侧部、一左侧部及一结合段,右侧翼设置于右侧部,左侧翼设置于左侧部,该结合段设置在飞机之机身顶部一容置槽,用一顶盖和机身结合,以封闭该容置槽;藉此可有效节省组装机翼的组装时间,亦可减少组装程序,以降低组装时所产生的误差,使飞机在飞行时有更高的安全性。


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    Titel :

    Aircraft wing


    Weitere Titelangaben:

    飞机的机翼


    Beteiligte:
    XU LIANG (Autor:in)

    Erscheinungsdatum :

    2020-10-30


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    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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