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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    Titel :

    Sealing structure used between flaps of airplane


    Weitere Titelangaben:

    一种用于飞机的襟翼之间的密封结构


    Beteiligte:
    YANG YINGHAO (Autor:in) / ZHANG JIASEN (Autor:in) / YUAN XIUQI (Autor:in) / CHEN YIN (Autor:in) / LI CHENXI (Autor:in)

    Erscheinungsdatum :

    2023-12-08


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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