The present invention relates to an aircraft assembly. The aircraft assembly includes a wingtip device connected to a wingtip of a wing by a first connector, a second connector, and a third connector. The wingtip device includes a front device spar and a back device spar. The first connector is combined with the back device spar. The second connector is spaced apart in a front chord direction of the first connector, and the third connector is spaced apart in a back chord direction of the first connector. The third connector includes a spigot mounting shape part.

    본 발명은 항공기 조립체에 관한 것이다. 항공기 조립체는 제1 커넥터, 제2 커넥터 및 제3 커넥터에 의해 날개의 윙팁에 연결되는 윙팁 장치를 갖는다. 윙팁 장치는 전방 장치 스파와 수방 장치 스파를 포함한다. 제1 커넥터는 후방 장치 스파와 결합된다. 제2 커넥터는 제1 커넥터의 전향 시위 방향으로 이격되어 있고, 제3 커넥터는 제1 커넥터의 후향 시위 방향으로 이격되어 있다. 제3 커넥터는 스피곳 장착 형태부를 포함한다.


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    Titel :

    AN AIRCRAFT ASSEMBLY INCLUDING A WINGTIP DEVICE


    Weitere Titelangaben:

    윙팁 장치를 포함하는 항공기 조립체


    Beteiligte:
    STEADMAN CLIVE (Autor:in) / LIVERSAGE DAVID (Autor:in) / SMITH BEN (Autor:in) / PULLAN RUTH (Autor:in)

    Erscheinungsdatum :

    29.04.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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