The invention relates to a movable leading edge flap (16) comprising an aerodynamic component (19) and at least one drive and guide rail system (42) comprising two guide rails (44), each extending along the entire length of said guide rail system, an intermediate reinforcement (46) being provided with a toothed drive track, the guide rail being mounted between the two guide rails (44), in the direction in which the three separate components are stacked, rail fixing elements (52) are used to fix each rail to the intermediate reinforcement (46), and each of the two rails (44) has a substantially C-shaped cross-section, the two C-shaped cross-sections being arranged back to back, the grooves (58) of which open in the span-wise direction (17), the grooves (58) being defined by the substantially C-shaped cross-sections of the rails, and the grooves (58) being formed in the cross-section of the cross-sections of the rails (44) in the cross-section of the cross-sections of the cross-sections of the cross-sections of the cross-sections of the cross-sections of the cross-sections of the cross-sections of the cross-sections of the cross-sections. The device is used for receiving an assembly for guiding a movable flap.
本发明涉及一种可移动的前缘襟翼(16)包括空气动力学部件(19)和至少一个驱动和导轨系统(42),该系统包括两条导轨(44),每条导轨均沿所述导轨系统的整个长度延伸,一个中间加强件(46)设有齿形驱动轨道,该导轨安装在两个导轨(44)之间,在这三个独立组件堆叠的方向上,导轨固定元件(52)用于将将每条导轨固定到中间加强件(46)上,并且两条轨道(44)中的每一条都具有一个大致呈C形的截面,两个C背靠背排列,其凹槽(58)沿展向(17)打开,凹槽(58)由导轨的大致呈C形定义,用于接收用于引导可移动襟翼的组件。
Movable leading edge flap with multiple force flow paths
具有多力流动路径的可移动前缘襟翼
2024-08-23
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
AIRCRAFT LEADING EDGE FLAP AND METHOD TO DEPLOY A LEADING EDGE FLAP
European Patent Office | 2024
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