The present invention relates to a slat (108) for the leading edge of a swept aircraft wing. The slat comprises slat tracks (114) that dictate the path of movement of the slat as it moves from a retracted position (FIG. 7) to a fully deployed position (FIG. 15). Each slat track (114) has a shape that follows a helical path. The motion of the slat thus includes a component of rotation about a firstaxis, which may be perpendicular to the line of flight (120) and a component of translational movement parallel to the first axis. When viewed from above the slat may move predominantly in a direction parallel to the line of flight (120).

    本发明涉及一种用于扫掠式飞行器机翼的前缘的缝翼(108),该缝翼包括缝翼轨道(114),缝翼轨道(114)决定当缝翼从缩回位置(图7)运动至完全展开位置(图15)时缝翼的运动路径。每个缝翼轨道(114)具有依循螺旋路径的形状。因此,缝翼的运动包括围绕可垂直于飞行航线(120)第一轴线的旋转分量以及平行于第一轴线的平移运动分量。当从上方观察时,缝翼可主要在平行于飞行航线(120)的方向上运动。


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    Title :

    Slat for an aircraft wing


    Additional title:

    用于飞行器机翼的缝翼


    Contributors:

    Publication date :

    2020-09-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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