A composite multi-spar aircraft lifting surface comprising an integral torsion box (1) comprising: a first partial skin (3.1) continuous on a second surface (1.2) from a right wingtip (4.1) to a left wingtip (4.2); a second part skin (3.2) continuous from the right wingtip (4.1) to the first central part (5) on the lateral right side (1.3) of the first face (1.1); a third part skin (3.3) continuous from the left wingtip (4.2) to the second central part (6) on a lateral left side (1.4) of the first face (1.1); a cover (7) spanning between the first central portion (5) and the second central portion (6). The spar (2), the first part skin (3.1), the second part skin (3.2) and the third part skin (3.3) are integrated multi-unit components.

    一种复合多翼梁飞行器升力面,包括一体化的扭转箱(1),所述扭转箱包括:第一部分蒙皮(3.1),在第二面(1.2)上从右翼尖(4.1)到左翼尖(4.2)连续;第二部分蒙皮(3.2),在第一面(1.1)的横向右侧(1.3)上从右翼尖(4.1)到第一中心部分(5)连续;第三部分蒙皮(3.3),在第一面(1.1)的横向左侧(1.4)上从左翼尖(4.2)到第二中心部分(6)连续;覆盖件(7),横跨第一中心部分(5)和第二中心部分(6)之间。翼梁(2)、第一部分蒙皮(3.1)、第二部分蒙皮(3.2)和第三部分蒙皮(3.3)是一体化多单元部件。


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    Title :

    Composite multi-spar aircraft lifting surface


    Additional title:

    复合多翼梁飞行器升力面



    Publication date :

    2024-01-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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