The present invention includes: a slat 3; and a position adjustment mechanism that adjusts an attachment position of the slat 3 to a main wing 1 by causing the slat 3 to swing, the position adjustment mechanism including: a pivot shaft S1 as a center of the swing motion of the slat 3; and a driving shaft S2 that is rotatably supported on a rail 12, and induces the swing motion of the slat 3. The driving shaft S2 includes: a main shaft 30 that causes the slat 3 to swing by acting thereon; an inner-side eccentric bushing 31 that is fixed to the main shaft 30, and eccentric with respect to the main shaft 30; and an outer-side eccentric bushing 32 that is eccentric with respect to the inner-side eccentric bushing 31, rotatably arranged therearound, and supported rotatably with respect to the rail 12.


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    Titel :

    Slat of aircraft, method for adjusting attachment position of slat, and aircraft


    Beteiligte:
    OKABE YOSHINORI (Autor:in) / ISHIHARA KENYA (Autor:in)

    Erscheinungsdatum :

    16.08.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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