항공기 윙은 메인 고정 윙 부와 그 팁에 윙 팁 장치를 구비한다. 윙 팁 장치는 비행 형태와 지상 형태 사이에 구성 가능하며, 지상 형태에서 윙 팁 장치는 항공기 윙의 스팬이 감소되도록 비행 형태로부터 멀어지도록 이동된다. 힌지 배열체는 메인 고정 윙 부와 윙 팁 장치를 연결하고, 윙 팁 장치가 지상 형태와 비행 형태 사이에서 회전할 수 있도록 한다. 힌지 배열체는 메인 고정 윙 부와 윙 팁 장치의 외부 표면을 넘어 돌출된다. 페어링은 윙의 적어도 흡입 측 상에서 힌지 배열체의 적어도 일부를 덮는다.

    An aircraft wing has a main fixed wing portion and a wing tip device at a tip thereof. The wing tip device is configurable between a flight configuration and a ground configuration, in which ground configuration the wing tip device is moved away from the flight configuration such that the span of the aircraft wing is reduced. A hinge arrangement connects the main fixed wing portion and the wing tip device and enables the wing tip device to rotate between the ground configuration and the flight configuration. The hinge arrangement protrudes beyond an outer surface of the main fixed wing portion and wing tip device. A fairing covers at least part of the hinge arrangement on at least a suction side of the wing.


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    Title :

    FAIRING FOR FOLDING WING TIP


    Additional title:

    접이식 윙 팁을 위한 페어링


    Contributors:
    FAMILY OLIVER (author) / MILLS ROBERT (author) / GRAY CHRIS (author) / WILSON THOMAS (author)

    Publication date :

    2024-03-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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