The invention relates to a sealing arrangement for use between flaps of an aircraft, the sealing arrangement comprising a first sealing portion and a second sealing portion, the first and second sealing portions interfacing one another between the flaps, where the first sealing portion comprises a plurality of discrete first seals, and the second sealing portion comprises a plurality of discrete second seals. And the second sealing portion includes a plurality of discrete second seals. The sealing structure with the separated design is more suitable for the situation of scissors difference between the inner flap and the outer flap.

    本发明涉及一种用于飞机的襟翼之间的密封结构,这种密封结构包括第一密封部分和第二密封部分,第一密封部分和第二密封部分在襟翼之间彼此对接,其中,第一密封部分包括多个离散的第一密封件,并且第二密封部分包括多个离散的第二密封件。这种分离式设计的密封结构更适用于内外襟翼间剪刀差的情形。


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    Title :

    Sealing structure used between flaps of airplane


    Additional title:

    一种用于飞机的襟翼之间的密封结构


    Contributors:
    YANG YINGHAO (author) / ZHANG JIASEN (author) / YUAN XIUQI (author) / CHEN YIN (author) / LI CHENXI (author)

    Publication date :

    2023-12-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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