The invention relates to a wing for an aircraft, a trailing edge high lift assembly and the aircraft. The wing includes a main wing and a trailing edge high lift assembly movably arranged at a trailing edge of the main wing, the trailing edge high lift assembly including a flap and a connection assembly movably mounting the flap to the main wing such that the flap is movable between a retracted position and at least one extended position, the connection assembly includes an actuator unit that moves a flap between a retracted position and at least one extended position, the flap including a leading edge portion and a trailing edge portion pivotally mounted to the leading edge portion about a pivot axis. The object of providing a wing with a trailing edge high lift assembly having a simplified actuation concept is achieved in that the actuator unit is coupled to the leading edge portion via a first linkage and to the trailing edge portion via a second linkage, and the actuator unit is configured to move the leading edge portion via the first link mechanism and the trailing edge portion via the second link mechanism.
本发明涉及用于飞行器的机翼、后缘高升力组件、以及飞行器。机翼包括主机翼和以可移动的方式布置在主机翼的后缘处的后缘高升力组件,后缘高升力组件包括襟翼和将襟翼以可移动的方式安装至主机翼、使得襟翼能够在缩回位置与至少一个伸出位置之间移动的连接组件,连接组件包括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,襟翼包括前缘部分和以能够围绕枢转轴线枢转的方式安装至前缘部分的后缘部分。提供具有简化致动概念的后缘高升力组件的机翼的目的是这样实现的,致动器单元经由第一连杆机构联接至前缘部分并经由第二连杆机构联接至后缘部分,且致动器单元配置成经由第一连杆机构使前缘部分移动并经由第二连杆机构使后缘部分移动。
Wing for aircraft, trailing edge high lift assembly and aircraft
用于飞行器的机翼、后缘高升力组件、以及飞行器
2023-10-17
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
Aircraft wing, trailing edge high lift assembly and aircraft
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