The invention relates to a wing, a high-lift assembly, a universal frame assembly 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 movably connects the high lift body to the main wing such that the high lift body is movable between a retracted position and at least one 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. A first end and/or intermediate portion of the track is mounted to the high lift body and a second end and/or intermediate portion is mounted to the main wing by a roller bearing such that the track is movable along the track longitudinal axis. The roller bearing comprises at least one roller unit mounted to the main wing and engaging an engagement surface provided at the track, which is universally mounted to the main wing such that the roller unit can adjust its tilt position relative to the engagement surface.
本发明涉及机翼、高升力组件、万向框架组件及飞行器。机翼包括主机翼和高升力组件,高升力组件包括高升力体和连接组件。连接组件将高升力体以可移动的方式连接至主机翼,使得高升力体能够在缩回位置与至少一个伸出位置之间移动。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并具有位于第一端部与第二端部之间的中间部分。轨道的第一端部和/或中间部分安装至高升力体,并且第二端部和/或中间部分通过滚子轴承安装至主机翼,使得轨道能够沿着轨道纵向轴线移动。滚子轴承包括安装至主机翼并且接合设置在轨道处的接合表面的至少一个滚子单元,其以万向方式安装至主机翼,使得滚子单元能够相对于接合表面调整其倾斜位置。
Wing, high-lift assembly, universal frame assembly and aircraft
机翼、高升力组件、万向框架组件及飞行器
2024-08-30
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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