An aircraft wing (700) includes a fixed structure (102) and a linear hydraulic slat actuator (104) attached to the fixed structure (102). The linear hydraulic slat actuator (104) is oriented spanwise along the aircraft wing (700). The aircraft wing (700) also includes an actuator output link (108) and a slat (710) attached to the actuator output link (108). The aircraft wing (700) also includes a bell-crank (106) coupled to the linear hydraulic slat actuator (104) and to the actuator output link (108). In response to spanwise movement of the linear hydraulic slat actuator (104), the bell-crank (106) is configured to move the actuator output link (108) in a different direction that enables the slat (710) to move between a retracted position and an extended position.


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    Titel :

    VARIABLE SLAT DISPLACEMENT USING SPANWISE ACTUATOR


    Weitere Titelangaben:

    VARIABLE VORFLÜGELVERSCHIEBUNG MIT SPANNWEITIGEM AKTUATOR
    DÉPLACEMENT VARIABLE DE LATTES À L'AIDE D'UN ACTIONNEUR DANS LE SENS DE L'ENVERGURE


    Beteiligte:
    KAMILA ERIC S (Autor:in) / BURIN RAMON A (Autor:in) / STANDLEY JOHN A (Autor:in)

    Erscheinungsdatum :

    12.03.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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