A rotorcraft includes a flight control computer (FCC), a first rotor system, and a second rotor system. The first rotor system includes a first swashplate coupled to a first rotor and a first multiple actuators configured to move the first swashplate. The second rotor system includes a second swashplate coupled to a second rotor and a second multiple actuators configured to move the second swashplate. The rotorcraft also includes a first communications channel coupled between the FCC, a first actuator of the first multiple actuators, and a second actuator of the second multiple actuators. The rotorcraft also includes a second communications channel coupled between the FCC and a third actuator of the first multiple actuators.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Rotorcraft swashplate actuator control


    Beteiligte:

    Erscheinungsdatum :

    18.08.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    ROTORCRAFT SWASHPLATE ACTUATOR CONTROL

    TRANTHAM MICHAEL / ATKINS BRADY / COVINGTON CHARLES | Europäisches Patentamt | 2023

    Freier Zugriff

    Rotorcraft Swashplate Actuator Control

    TRANTHAM MICHAEL / ATKINS BRADY G / COVINGTON CHARLES ERIC | Europäisches Patentamt | 2019

    Freier Zugriff

    Composite swashplate guide for rotorcraft control systems

    ORBON JAMES / NGUYEN DEAN / LAITENBERGER KEVIN et al. | Europäisches Patentamt | 2019

    Freier Zugriff

    COMPOSITE SWASHPLATE GUIDE FOR ROTORCRAFT CONTROL SYSTEMS

    ORBON JAMES / NGUYEN DEAN / LAITENBERGER KEVIN et al. | Europäisches Patentamt | 2018

    Freier Zugriff

    Dynamically adjustable rotorcraft swashplate with undulating surface

    GALLAGHER V EDWARD F | Europäisches Patentamt | 2022

    Freier Zugriff