A fairing arrangement for a high-lift mechanism for an aircraft is disclosed including a flap to be arranged at a trailing edge of an aircraft wing, and a mounting and guiding mechanism for the flap. The fairing arrangement includes a flap side fairing unit and a wing side fairing unit. The flap side fairing unit includes a flap side fairing for covering an aft part of the mounting and guiding mechanism and a flap side fairing mount for mounting the flap side fairing to the flap. The wing side fairing unit includes a wing side fairing for covering a forward part of the mounting and guiding mechanism, and a wing side fairing mount for mounting the wing side fairing to the wing. The wing side fairing mount is configured for movably connecting the wing side fairing to the wing such that the wing side fairing is rotatable around an axis directed at least partially in a vertical direction.


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    Title :

    FAIRING ARRANGEMENT FOR A HIGH-LIFT MECHANISM OF AN AIRCRAFT


    Contributors:

    Publication date :

    2024-10-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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