The invention relates to a wing for an aircraft, a trailing edge high lift assembly and the aircraft. A wing of an aircraft includes a main wing and a trailing edge high lift assembly movably arranged at a trailing edge of the main wing, including a flap and a connection assembly movably mounting the flap to the main wing, where the connection assembly includes an actuator unit for moving the flap between a retracted position and at least one extended position, where the actuator unit is configured to move the flap between the retracted position and the at least one extended position. The flap includes a leading edge portion and a trailing edge portion pivotally mounted to the leading edge portion about a pivot axis. The trailing edge high lift assembly allows for reduced weight and cost of the wing because the actuator unit is configured for moving the trailing edge portion relative to the leading edge portion independently of moving the flap between a retracted position and at least one extended position, and/or configured for moving the flap between the retracted position and the at least one extended position independently of moving the trailing edge portion relative to the leading edge portion.

    本发明涉及用于飞行器的机翼、后缘高升力组件及飞行器。飞行器的机翼包括主机翼和可移动地布置在主机翼的后缘处的后缘高升力组件,其包括襟翼和将襟翼可移动地安装至主机翼的连接组件,其中,连接组件包括用于使襟翼在缩回位置与至少一个伸出位置之间移动的致动器单元,其中,襟翼包括前缘部分和以能够绕枢转轴线枢转的方式安装至前缘部分的后缘部分。后缘高升力组件允许降低机翼的重量和成本,因为致动器单元构造成用于使后缘部分相对于前缘部分以独立于使襟翼在缩回位置与至少一个伸展位置之间移动的方式移动,并且/或者构造成用于使襟翼在缩回位置与至少一个伸出位置之间以独立于使后缘部分相对于前缘部分移动的方式移动。


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    Title :

    Aircraft wing, trailing edge high lift assembly and aircraft


    Additional title:

    用于飞行器的机翼、后缘高升力组件及飞行器


    Contributors:

    Publication date :

    2024-01-30


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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