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

An aircraft high lift airfoil arrangement guiding element includes a first part configured to be fixed to a first edge member or rib of the airfoil arrangement, and a second part including a track support element to movably support a track device of a second edge member or slat of the airfoil arrangement. The second part is mounted to the first part to move from a first to a second position. A biasing device biases the track support element in the spanwise direction towards the track device. The airfoil arrangement is produced by providing the first edge member or rib, rigidly attaching thereto guiding elements to guide the movable track device supporting the second edge member or slat, and attaching the track device to the first edge member. During installation, a surface of the track device is pressed against a movable track support element biased against the track device.
机译:飞机高升降机翼型布置引导元件包括配置成固定到翼型装置的第一边缘构件或肋的第一部分,以及包括轨道支撑元件的第二部分,以可移动地支撑第二边缘构件或板块的轨道装置 翼型装置。 第二部分安装到第一部分以从第一到第二位置移动。 偏置装置将轨道支撑元件朝向轨道装置偏置。 翼型装置通过提供第一边缘构件或肋,刚性地附接到其引导元件以引导支撑第二边缘构件或板条的可移动轨道装置,并将轨道装置附接到第一边缘构件。 在安装过程中,轨道装置的表面被压靠在抵靠轨道装置的可移动轨道支撑元件上。

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