A system is provided for controlling the pitch of blades of a rotor, the system comprising an actuator for each blade, each actuator being configured for selective control of the pitch of an associated blade about a pitch axis. Sensors are configured for determining aerodynamic forces acting on the rotor, and a flight control system is configured to receive signals from the sensors and for operating the actuators in response to the signals to achieve a desired pitch-flap coupling value.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    ELECTRONIC CONTROL OF BLADE PITCH ON A TILTROTOR


    Beteiligte:

    Erscheinungsdatum :

    2021-06-03


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES



    Electronic control of blade pitch on a tiltrotor

    STAMPS FRANK BRADLEY / PARHAM JR THOMAS C | Europäisches Patentamt | 2024

    Freier Zugriff


    ICE PROTECTION SYSTEM FOR TILTROTOR BLADE

    AUBERT ROBERT J / PAULSON JARED M | Europäisches Patentamt | 2020

    Freier Zugriff

    Influence of Pitch Attitude on Tiltrotor Autorotation Characteristics

    Vorwald, J. / AHS International | British Library Conference Proceedings | 2010


    Method of blade fold for tiltrotor aircraft

    KIZHAKKEPAT AMARJIT / SHIMEK GLENN ALAN | Europäisches Patentamt | 2020

    Freier Zugriff