The invention relates to a wing (3) for an aircraft (1), comprising a main wing (5), a slat (7), and a connecting assembly (9) movably connecting the slat (7) to the main wing (5), such that the slat (7) is movable between a retracted position and at least one extended position, wherein the connecting assembly (9) comprises a slat track (11) and a roller bearing (13), wherein a front section (17) of the slat track (11) is mounted to the slat (7), wherein a rear section (19) and an intermediate section (21) of the slat track (11) are mounted to the main wing (5) via the roller bearing (13), wherein the roller bearing (13) comprises a guide rail (23) mounted to the main wing (5) and a first roller (27), wherein the first roller (27) is rotatably mounted to the rear section (19) of the slat track (11), wherein the first roller (27) engages a first engagement surface (33) formed by the guide rail (23), wherein the roller bearing (13) comprises a second roller (31), wherein the second roller (31) is rotatably mounted to the main wing (5), wherein the second roller (31) engages a second engagement surface (35) formed by the intermediate section (21) of the slat track (11), wherein the first engagement surface (33) comprises a first section (45), which is straight or is curved with a first radius of curvature (51) and a first center of curvature (53), and the second engagement surface (35) comprises a second section (49), which is straight or is curved with a second radius of curvature (55) and a second center of curvature, wherein, when both the first section (45) and the second section (49) are curved, the first center of curvature (53) and the second center of curvature are spaced from each other.

    本发明涉及一种用于飞行器(1)的机翼(3),包括:主翼(5);缝翼(7);以及连接组件(9),连接组件将缝翼(7)以可移动的方式连接至主翼(5),使得缝翼(7)能够在缩回位置与至少一个伸出位置之间移动,其中,连接组件(9)包括缝翼轨道(11)和滚子支承件(13),其中,缝翼轨道(11)的前部部段(17)安装至缝翼(7),其中,缝翼轨道(11)的后部部段(19)和中间部段(21)经由滚子支承件(13)安装至主翼(5),其中,滚子支承件(13)包括安装至主翼(5)的导引轨道(23)以及第一滚子(27),其中,第一滚子(27)以可旋转的方式安装至缝翼轨道(11)的后部部段(19),其中,第一滚子(27)接合由导引轨道(23)形成的第一接合表面(33),其中,滚子支承件(13)包括第二滚子(31),其中,第二滚子(31)以可旋转的方式安装至主翼(5),其中,第二滚子(31)接合由缝翼轨道(11)的中间部段(21)形成的第二接合表面(35),其中,第一接合表面(33)包括第一部段(45),第一部段是直的或者弯曲成具有第一曲率半径(51)和第一曲率中心(53),并且第二接合表面(35)包括第二部段(49),第二部段是直的或者弯曲成具有第二曲率半径(55)和第二曲率中心,其中,当第一部段(45)和第二部段(49)两者都是弯曲的时,第一曲率中心(53)与第二曲率中心彼此间隔开。


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    Titel :

    CONNECTING ASSEMBLY FOR AN AIRCRAFT WING SLAT


    Weitere Titelangaben:

    用于飞行器机翼缝翼的连接组件


    Beteiligte:
    DAANDELS DORT (Autor:in) / SCHLIPF BERNHARD (Autor:in)

    Erscheinungsdatum :

    2022-02-22


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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