A wing (3) for an aircraft (1), a trailing edge high lift assembly and an aircraft are described, in particular, the wing comprising a main wing (5) and a trailing edge high lift assembly (9) arranged in a movable manner at the trailing edge of the main wing (5), the trailing edge high lift assembly (9) comprising a flap (11) and a connecting assembly (13) mounting the flap (11) in a movable manner to the main wing (5), the connection assembly (13) is configured such that the flap (11) can be moved between a retracted position (15) and at least one extended position (17), and wherein the connection assembly (13) is configured such that the flap (11) can be moved linearly and/or rotationally relative to the main wing (5). The aim of providing a wing with a trailing edge high lift assembly allowing the shape of the wing to be adjusted more freely is achieved in that the connecting assembly (13) is configured such that the flap (11) can be moved in a separate linear manner and in a rotational manner relative to the main wing (5).
描述了一种用于飞行器(1)的机翼(3)、后缘高升力组件及飞行器,特别地,该机翼包括主机翼(5)和以可移动的方式布置在主机翼(5)的后缘处的后缘高升力组件(9),该后缘高升力组件(9)包括襟翼(11)和连接组件(13),该连接组件将襟翼(11)以可移动的方式安装至主机翼(5),使得襟翼(11)能够在缩回位置(15)与至少一个延伸位置(17)之间移动,其中,连接组件(13)构造成使得襟翼(11)能够相对于主机翼(5)以线性和/或旋转的方式移动。实现了提供一种具有允许更自由地调节机翼形状的后缘高升力组件的机翼的目的,因为连接组件(13)构造成使得襟翼(11)能够相对于主机翼(5)以分离式的线性的方式和旋转的方式移动。
Aircraft wing, trailing edge high lift assembly and aircraft
用于飞行器的机翼、后缘高升力组件及飞行器
2023-08-29
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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