A ducted-rotor aircraft may include a fuselage and first and second ducts that are coupled to the fuselage at respective first and second locations. The first location may be on a first side of a fuselage of the aircraft and spaced from a nominal yaw axis of the aircraft. The second location may be on an opposed second side of the fuselage and spaced from the nominal yaw axis. Each duct may include a rotor that is disposed in an opening that extends through the duct. Each rotor may include a plurality of blades. Each duct may further include a control vane that is mounted aft of the plurality of blades and that is pivotable about a vane axis that is oriented toward the nominal yaw axis.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    CONTROL VANE ORIENTATION FOR DUCTED-ROTOR AIRCRAFT


    Beteiligte:

    Erscheinungsdatum :

    2021-07-01


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Control vane orientation for ducted-rotor aircraft

    SCHROEDER KARL / AMANTE WILLIAM ANTHONY / CAMPBELL KIP GREGORY | Europäisches Patentamt | 2022

    Freier Zugriff

    Duct for ducted-rotor aircraft

    SCHROEDER KARL / AMANTE WILLIAM ANTHONY / CARPENTER JR JOSEPH RICHARD et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    DUCT FOR DUCTED-ROTOR AIRCRAFT

    SCHROEDER KARL / AMANTE WILLIAM ANTHONY / CARPENTER JR JOSEPH RICHARD et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    SPAR FOR DUCTED-ROTOR AIRCRAFT

    SCHROEDER KARL / AMANTE WILLIAM ANTHONY / CARPENTER JR JOSEPH RICHARD et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    BONDED SKINS FOR DUCTED-ROTOR AIRCRAFT

    SCHROEDER KARL / CARR TIMOTHY BRIAN / CARLSON DAVID G et al. | Europäisches Patentamt | 2021

    Freier Zugriff