首页> 外国专利> GUIDING ELEMENT FOR A HIGH LIFT AIRFOIL ARRANGEMENT OF AN AIRCRAFT, HIGH LIFT AIRFOIL ARRANGEMENT AND PRODUCTION METHOD

GUIDING ELEMENT FOR A HIGH LIFT AIRFOIL ARRANGEMENT OF AN AIRCRAFT, HIGH LIFT AIRFOIL ARRANGEMENT AND PRODUCTION METHOD

机译:用于飞机的高升降机翼型布置的引导元件,高升降机翼型布置和生产方法

摘要

A guiding element (60) for a high lift airfoil arrangement of an aircraft comprises a first part (62) configured for being fixed to a first edge member or rib (34) of a high lift airfoil arrangement, and a second part (63) comprising at least one track support element (66) for movably supporting a track device (28) of a second edge member or slat (16) of the airfoil arrangement. The second part (63) is movably mounted to the first part (62) and configured for moving from a first position to a second position. A biasing device (73) is configured for biasing the track support element (66) in the spanwise direction towards the track device (28). A high lift airfoil arrangement is produced by providing a first edge member or rib (34), rigidly attaching thereto guiding elements for guiding a movable track device supporting a second edge member or slat (16), and attaching the track device (28) to the first edge member. During installation of the track device (28), a surface (29) of the track device (28) is pressed against a movable track support element (66) which is biased against the track device (28).
机译:用于飞机的高升降机翼型装置的引导元件(60)包括配置用于固定到高升降机翼型装置的第一边缘构件或肋(34)的第一部分(62),以及第二部分(63)包括至少一个轨道支撑元件(66),用于可移动地支撑翼型装置的第二边缘构件或板条(16)的轨道装置(28)。第二部分(63)可移动地安装到第一部分(62)并且被配置用于从第一位置移动到第二位置。偏置装置(73)被配置用于将轨道支撑元件(66)朝向轨道装置(28)偏置。通过提供第一边缘构件或肋(34)来制造高升降翼型装置,刚性地附接到其引导元件,用于引导支撑第二边缘构件或板条(16)的可移动轨道装置,并将轨道装置(28)附接到第一边缘构件。在轨道装置(28)的安装期间,轨道装置(28)的表面(29)被压靠在可移动轨道支撑元件(66)上,所述可移动轨道支撑元件(66)偏置在轨道装置(28)上。

著录项

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号