Disclosed is a method for operating a wing (5) for an aircraft (1) including a foldable wing tip portion (11). The object, to improve and simplify locking of the arresting unit, is achieved by the following steps: - Providing a wing (5) for an aircraft (1), the wing (5) comprising a fixed wing (9), a foldable wing tip portion (11) mounted to the fixed wing (9) pivotally between an extended position and a folded position, an actuation unit (13) for actuating movement of the foldable wing tip portion (11), and an arresting unit (15) for locking the foldable wing tip portion (11) in the extended position and/or in the folded position, - Controlling the actuation unit (13) to move the foldable wing tip portion (11) either to the extended position or to the folded position until the foldable wing tip portion (11) or the actuation unit (13) contacts a stop element (28), - Continuing actuation until the actuation unit (13) reaches a stall condition, - Detecting the stall condition of the actuation unit (13), - Locking the arresting unit (15) upon detection of the stall condition.


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    Titel :

    СПОСОБ ЭКСПЛУАТАЦИИ КОНСОЛИ КРЫЛА ЛЕТАТЕЛЬНОГО АППАРАТА, СОДЕРЖАЩЕЙ СКЛАДЫВАЕМУЮ КОНЦЕВУЮ ЧАСТЬ КОНСОЛИ КРЫЛА


    Erscheinungsdatum :

    2020-05-18


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Russisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge