A restraint system for a transmission in an aircraft can include a first strut having a first fluid chamber, a first piston resiliently coupled to a first housing with a first elastomeric member. The restraint system can include a second strut having second fluid chamber, a second piston resiliently coupled to a second housing with a second elastomeric member. The restraint system can include a fluid line between the first fluid chamber and the second fluid chamber. The first strut and the second strut collectively provide not only torque restraint, but also torque measurement and fore/aft vibration isolation.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Helicopter transmission mount system


    Beteiligte:
    HENDRICKS MATTHEW W (Autor:in) / GRIFFIN MAURICE D (Autor:in) / SMITH MICHAEL R (Autor:in) / LEE TAEOH (Autor:in)

    Erscheinungsdatum :

    09.02.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F16F SPRINGS , Federn



    Helicopter transmission mount system

    GRIFFIN MAURICE D / HENDRICKS MATTHEW W | Europäisches Patentamt | 2016

    Freier Zugriff

    Helicopter servo cylinder mount fixture for assembly work

    LEE HAN KYU | Europäisches Patentamt | 2024

    Freier Zugriff

    Helicopter transmission device and helicopter

    HONG LIANG / SUN RAN / JIANG YUXUAN et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    Transmission system and helicopter

    WU YANPENG / WANG QI / TIAN GANGYIN | Europäisches Patentamt | 2022

    Freier Zugriff

    HELICOPTER TRANSMISSION

    NEKRASOV VLADIMIR IVANOVICH / SYZRANTSEV VLADIMIR NIKOLAEVICH / ZIGANSHIN RUSLAN ALBERTOVICH et al. | Europäisches Patentamt | 2016

    Freier Zugriff