The invention provides an aircraft wing (10, Fig 1), comprising a fixed wing (14, Fig 1) and a wing tip device (12, Fig 1) at the tip. The wing tip device is configurable between a locked flight configuration for use during flight and a ground configuration for use during ground-based operations. The wing further comprises a locking mechanism for locking the folding wing tip device in the locked flight configuration. A rotatable locking member 22 is associated with one of the folding wing tip device and the fixed wing, and a locking pin 32 is associated with the other. The rotatable locking member comprises a guide surface (30, Fig 2) to guide the locking pin to a locked configuration, in which the guide surface is shaped such that the locking pin is urged toward the rotation axis X of the rotatable locking member by a camming action of the guide surface on the locking pin, thereby preloading the locking mechanism.


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    Titel :

    Folding wing tip and rotating locking device


    Beteiligte:
    CHETAN KORYA (Autor:in) / ANTHONY BRYANT (Autor:in) / MATTHEW HARDING (Autor:in) / DAVID BRAKES (Autor:in)

    Erscheinungsdatum :

    2016-11-16


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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