The present invention relates to a wing (2) for an aircraft (1), comprising: a main wing (4) having an outer skin (6) defining an interior space (8) of the main wing, a slat (10), and a connection assembly (12) for movably connecting the slat to the main wing, such that the slat is movable in a predefined motion between a retracted position and at least one extended position, wherein the connection assembly comprises an elongate and curved slat track (18), wherein a first end section (20) of the slat track is connected to the slat, wherein the connection assembly comprises a first bearing (16), which is at least partly arranged outside the interior space of the main wing, wherein the connection assembly comprises a second bearing (14), which is spaced apart from the first bearing and arranged within the interior space of the main wing, and wherein the slat track is movably and rotatably supported on the main wing by the first and second bearing, such that the first and second bearing support the predefined motion. The present invention further relates to an aircraft comprising such a wing (2) as well as to a connection assembly as such.


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    Titel :

    КОНСОЛЬ КРЫЛА ДЛЯ ЛЕТАТЕЛЬНОГО АППАРАТА


    Erscheinungsdatum :

    2021-05-28


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Russisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge