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Wing for an aircraft having a simplified movable aerodynamic surface and a flexible sealing

机译:具有简化的可移动空气动力学表面和柔性密封的飞机机翼

摘要

A wing for an aircraft includes a wing structure attachable to a body of an aircraft, at least one high lift body movably supported at the wing structure, a drive unit coupled with the wing structure and the high lift body and adapted to move the high lift body relative to the wing structure in a chordwise direction between a retracted position and an extended position, and a sealing device coupled with the high lift body and the wing structure. The high lift body comprises at least one outer edge facing to the wing structure, which at least one outer edge creates a gap to the wing structure at least in an extended position. The sealing device includes a flexible sealing body, which seals the intermediate space between the high lift body and the wing structure in extended positions of the high lift body.
机译:用于飞机的机翼包括可附接到飞机的机体的机翼结构,可移动地支撑在机翼结构上的至少一个高升力体,与机翼结构和高升力体耦接并适于移动高升力的驱动单元相对于机翼结构在回缩位置和伸出位置之间在弦向方向上相对于机翼结构,以及与高升力机体和机翼结构连接的密封装置。高升力体包括至少一个面向机翼结构的外边缘,该至少一个外边缘至少在延伸位置中为机翼结构形成间隙。密封装置包括柔性密封体,其在高升程体的延伸位置中密封高升程体与机翼结构之间的中间空间。

著录项

  • 公开/公告号US10618626B2

    专利类型

  • 公开/公告日2020-04-14

    原文格式PDF

  • 申请/专利权人 AIRBUS OPERATIONS GMBH;

    申请/专利号US201715718974

  • 发明设计人 BERNHARD SCHLIPF;DORT DAANDELS;

    申请日2017-09-28

  • 分类号B64C9/02;B64C9/14;

  • 国家 US

  • 入库时间 2022-08-21 11:30:55

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