The invention relates to a wing for an aircraft, a high lift assembly, a roller unit, and an aircraft. The wing comprises a main wing and a high-lift assembly, and the high-lift assembly comprises a high-lift body and a connecting assembly. A connection assembly connects the high lift body to the main wing such that the high lift body is movable between a retracted position and an extended position. The connection assembly includes an elongate rail extending along a rail longitudinal axis between a first end and a second end and having an intermediate portion between the first end and the second end. The first end and/or intermediate portion is mounted to the high lift body and the second end and/or intermediate portion is mounted to the main wing by a roller support such that the track is movable along the track longitudinal axis. The roller support device includes a roller unit mounted to the main wing and having a circumferential roller surface that engages an engagement surface provided at the track. The roller unit includes a resilient support that allows the roller surface to adjust its orientation or form.
本发明涉及用于飞行器的机翼、高升力组件、滚子单元、以及飞行器。机翼包括主机翼和高升力组件,高升力组件包括高升力本体和连接组件。连接组件将高升力本体连接至主机翼,使得高升力本体能够在缩回位置与伸出位置之间移动。连接组件包括长形轨道,其沿着轨道纵向轴线在第一端部与第二端部之间延伸且具有位于第一端部与第二端部之间的中间部分。第一端部和/或中间部分安装至高升力本体,第二端部和/或中间部分通过滚子支承装置安装至主机翼,使得轨道能够沿着轨道纵向轴线移动。滚子支承装置包括滚子单元,其安装至主机翼且具有与设置在轨道处的接合表面接合的周向滚子表面。滚子单元包括弹性支承件,弹性支承件允许滚子表面调整其取向或形式。
Wing for aircraft, high-lift assembly, roller unit and aircraft
用于飞行器的机翼、高升力组件、滚子单元以及飞行器
2025-01-14
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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