A thrust mount assembly includes a thrust link-lever that has a first end region, a second end region, and a fulcrum region disposed between the first end region and the second end region. A thrust link-lever may be coupled or couplable to a fulcrum body of an aft engine-mount at a fulcrum position of the thrust link-lever. When coupled to a turbomachine, the fulcrum position of the thrust link-lever may be laterally offset and/or laterally adjustable relative to an axis of rotation of the turbomachine. A load translated from an engine frame of a turbomachine to an engine-mounting linkage system may be determined and a fulcrum position for the thrust mount assembly may be adjusted laterally relative to an axis of rotation of the turbomachine.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Thrust mounts with load-balancing thrust link-lever


    Beteiligte:

    Erscheinungsdatum :

    30.04.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



    THRUST MOUNTS WITH LOAD-BALANCING THRUST LINK-LEVER

    SHINDE KUDUM / SHENVI KHANDEPARKER MAHESH BHALCHANDRA | Europäisches Patentamt | 2022

    Freier Zugriff

    Thrust lever

    Europäisches Patentamt | 2015

    Freier Zugriff

    Vertical thrust lever

    WONG SHELDON / SHOEMAKER WILLIAM C | Europäisches Patentamt | 2018

    Freier Zugriff

    Variable thrust lever

    Europäisches Patentamt | 2018

    Freier Zugriff

    Variable thrust lever

    KIM TAE YEONG | Europäisches Patentamt | 2018

    Freier Zugriff