An aircraft hybrid flight control system comprising a manual control element, a mechanical transmission interposed between the manual control element and a control surface, an electromechanical actuator and a coupling unit configured to connect selectively the control surface to the mechanical transmission in a manual control mode and to the electromechanical actuator in a fly-by-wire control mode; the coupling unit is configured to maintain the mechanical transmission in a condition of substantial continuity with said control surface even in fly-by-wire mode, but for a freedom of relative motion of pre-set amplitude.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    AIRCRAFT HYBRID FLIGHT CONTROL SYSTEM


    Weitere Titelangaben:

    SYSTEME DE COMMANDE DE VOL HYBRIDE POUR UN AERONEF


    Beteiligte:

    Erscheinungsdatum :

    20.11.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    AIRCRAFT HYBRID FLIGHT CONTROL SYSTEM

    TENDOLA ANDREA / LIGNAROLO VITTORIO | Europäisches Patentamt | 2018

    Freier Zugriff

    Aircraft hybrid flight control system

    TENDOLA ANDREA / LIGNAROLO VITTORIO | Europäisches Patentamt | 2018

    Freier Zugriff

    AIRCRAFT HYBRID FLIGHT CONTROL SYSTEM

    TENDOLA ANDREA / LIGNAROLO VITTORIO | Europäisches Patentamt | 2016

    Freier Zugriff

    Hybrid flight aircraft

    MARTIN WARNER / CHARLES WILLIAM DENNIS / BRIAN DAVID TUTTY et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Hybrid flight aircraft

    Europäisches Patentamt | 2022

    Freier Zugriff