Disclosed is a wing (5) for an aircraft (1), comprising a main wing (11), a leading edge high lift assembly (13) comprising a leading edge high lift body (15), and a connection assembly (17) movably connecting the leading edge high lift body (15) to the main wing (11), wherein the connection assembly (17) comprises a drive system (25) that is mounted to the main wing (11) and connected to the leading edge high lift body (15) for driving the leading edge high lift body (15) between the retracted position and the extended position, wherein the drive system (25) comprises a first drive unit (27) and a second drive unit (29), wherein the first drive unit (27) has a first input section (31) coupled to a drive shaft (33), a first gear unit (35) and a first output section (37) coupled to a first connection element (19) and comprising a first output wheel (45), and wherein the second drive unit (29) has a second input section (39) coupled to the drive shaft (33), a second gear unit (41), and a second output section (43) coupled to a second connection element (21) and comprising a second output wheel (47). The object to prevent skew cases of the leading edge high lift body, is achieved in that the drive system (25) comprises a sync arrangement (57) coupling the first output section (37) to the second output section (43) for sync movement of the first and second output sections (37, 43). The sync arrangement (57) comprises a first sync wheel (59), a second sync wheel (61), and a sync shaft (63) fixedly connecting the first sync wheel (59) to the second sync wheel (61), the first sync wheel (59) is configured to engage the first output wheel (45) and the second sync wheel (61) is configured to engage the second output wheel (47).


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    Title :

    LEADING EDGE HIGH LIFT ASSEMBLY


    Additional title:

    ANORDNUNG FÜR EINE HOCHAUFTRIEBSVORRICHTUNG EINER TRAGFLÄCHENVORDERKANTE
    ENSEMBLE DE DISPOSITIF HYPERSUSTENTATEUR DE BORD D'ATTAQUE


    Contributors:

    Publication date :

    2024-10-30


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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