An aircraft comprising an airframe; a rotor system mounted to the airframe, the rotor system including a plurality of rotor blades, each of the plurality of rotor blades including a root portion extending to a tip portion through an airfoil portion, the airfoil portion having a leading edge and a trailing edge; at least one control surface mounted within the airfoil portion of at least one of the plurality of rotor blades; at least one actuator configured to actuate the at least one control surface; and at least one actuator configured to pitch at least one of the plurality of rotor blades about a blade pitch axis


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    Titel :

    REDUCED POWER INDIVIDUAL BLADE CONTROL SYSTEM ON A ROTORCRAFT


    Weitere Titelangaben:

    INDIVIDUELLES BLATTSTEUERUNGSSYSTEM MIT REDUZIERTER LEISTUNG AUF EINEM DREHFLÜGLER
    SYSTÈME DE COMMANDE DES PALES INDIVIDUELLES À PUISSANCE RÉDUITE SUR UN GIRAVION


    Beteiligte:

    Erscheinungsdatum :

    2020-01-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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