The invention relates to a hinge assembly for an aircraft component, an aircraft component, a wing and an aircraft. The present invention relates to a hinge assembly (8a) for an aircraft component, in particular to a hinge assembly (8a) for an aircraft component, the hinge assembly (8a) comprising a first hinge plate (9) and a second hinge plate (10), each hinge plate comprising a plurality of fingers (13) to (17). The fingers of the first hinge plate and the fingers of the second hinge plate are staggered. A sealing assembly (28) to (32) is provided between at least some of the fingers. The provision of a hinge including inserted fingers allows for the manufacture of a hinge assembly having a complex aerodynamic profile while performing a sealing function by a seal filling the gaps between the fingers.

    本发明涉及用于飞行器部件的铰链组件、飞行器部件、机翼及飞行器。特别地,涉及一种用于飞行器部件的铰链组件(8a),该铰链组件(8a)包括第一铰链板(9)和第二铰链板(10),每个铰链板包括多个指状部(13)至(17)。第一铰链板的指状部和第二铰链板的指状部交错。在指状部中的至少一些指状部之间提供有密封组件(28)至(32)。包括插入的指状部的铰链的提供允许制造具有复杂空气动力学轮廓的铰链组件,同时通过填充指状部之间的间隙的密封件来执行密封功能。


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    Title :

    Hinge assembly for aircraft component, aircraft component, wing and aircraft


    Additional title:

    用于飞行器部件的铰链组件、飞行器部件、机翼及飞行器


    Contributors:

    Publication date :

    2022-06-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    F16C SHAFTS , Wellen / B64C AEROPLANES , Flugzeuge



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