A rotary actuated high lift gapped aileron linkage (304) is presented. A high lift gapped aileron (306) couples to an airfoil at a hinge line (418) and changes a camber of the airfoil. A rotary actuator (312) coupled to the high lift gapped aileron produces a rotary motion of the high lift gapped aileron in response to an actuation command. A droop panel (308) positioned over the hinge line enhances lift of the high lift gapped aileron. A cove lip door (310) positioned under the hinge line provides an airflow over the high lift gapped aileron. The deployment linkage mechanism coupled to the high lift gapped aileron positions the droop panel and the cove lip door in response to the rotary motion.


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    Titel :

    Rotary actuated high lift gapped aileron


    Weitere Titelangaben:

    Drehbar betätigtes Hochauftriebspaltquerruder
    Aileron à entrefer de portance élevée actionné par rotation


    Beteiligte:
    KORDEL JAN A (Autor:in) / SAKURAI SEIYA (Autor:in)

    Erscheinungsdatum :

    06.10.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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