The invention relates to a leading edge assembly (9) for a wing (3). The leading edge assembly comprises a housing (11) configured to be connectable to a fixed wing section (59) of the wing (3) and in which a first opening (19) connecting an exterior (45) of the housing (11) with an interior (47) of the housing (11) is formed, and an actuating element (13) movably connected to the housing (11), the actuating element (13) extends through the first opening (19) and comprises a first section (49) arranged in the interior (47) of the housing (11) and a second section (51) arranged in the exterior (45) of the housing (11) and configured to be connectable to a high-lift device, such that the actuating element (13) is movable between a first position and at least one second position, in which the actuating element (13) extends through the first opening (19) and comprises a first section (49) arranged in the interior (47) of the housing (11) and a second section (51) arranged in the exterior (45) of the housing (11).
本发明涉及一种用于机翼(3)的前缘组件(9)。前缘组件包括壳体(11)和致动元件(13),该壳体构造成能够连接至机翼(3)的固定机翼部段(59),并且在该壳体中形成有将壳体(11)的外部(45)与壳体(11)的内部(47)连接的第一开口(19),致动元件以可移动的方式连接至壳体(11),使得致动元件(13)能够在第一位置与至少一个第二位置之间移动,其中,致动元件(13)延伸穿过第一开口(19)并且包括第一部段(49)和第二部段(51),第一部段布置在壳体(11)的内部(47)中,第二部段布置在壳体(11)的外部(45)中并且第二部段构造成能够连接至高升力装置。
Leading edge assembly, wing and aircraft
前缘组件、机翼和飞行器
2022-03-11
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |