An aeroengine control device including a mount and having pivotally mounted thereon a code wheel together with a main lever and a secondary lever, both for turning the code wheel. Each lever is movable between a rest position and a maximum actuation position. The secondary lever is mounted to pivot on the main lever. Cam paths are mounted on the code wheel and on the mount in such a manner that the main lever can move the code wheel when the main lever is moved while the secondary lever is in the rest position. The secondary lever can move the code wheel when the secondary lever is moved while the main lever is in the rest position, with movement of either lever being prevented when the other lever is clearly away from its rest position.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Aircraft throttle control device including a cam coupling


    Beteiligte:
    ELABELLAOUI HAFID (Autor:in) / BESOLD JEAN-ERIC (Autor:in) / PAUTARD SEBASTIEN (Autor:in) / CARTRY THIERRY (Autor:in) / ENGLER DAVID (Autor:in) / MERLET ETIENNE (Autor:in)

    Erscheinungsdatum :

    08.08.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Aircraft throttle control device including an engaging roller coupling

    ELABELLAOUI HAFID / BESOLD JEAN-ERIC / PAUTARD SÉBASITEN et al. | Europäisches Patentamt | 2017

    Freier Zugriff

    Aircraft throttle lever testing device

    ZHU DAWEI / CUI MINGBAO / WANG WENLIANG | Europäisches Patentamt | 2021

    Freier Zugriff

    Aircraft throttle lever synchronizing device

    WANG JUNDONG / KONG DELIANG / LI XINJUN et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Aircraft throttle lever testing device

    ZHANG LIANG / CUI MINGBAO / WANG WENLIANG | Europäisches Patentamt | 2021

    Freier Zugriff

    CONTROL PANEL INTEGRATION INTO AIRCRAFT THROTTLE CONTROL

    OTT JOSEPH / HUGHES KEITH / DE MERS ROBERT E et al. | Europäisches Patentamt | 2015

    Freier Zugriff