A gas turbine engine includes, among other things, a propulsor section including a rotor, a gear train, a low spool and a high spool. A static structure includes a first case and a second case. A mount system includes a forward mount and an aft mount arranged in a plane containing an engine axis of rotation. The forward mount is secured to the first case. The aft mount is secured to the second case.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Engine mount system for a gas turbine engine


    Beteiligte:

    Erscheinungsdatum :

    2023-08-22


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F02K JET-PROPULSION PLANTS , Strahltriebwerke



    GAS TURBINE ENGINE MOUNT

    BOWDEN WILLIAM JOSEPH / COLEMAN JONATHAN EDWARD / TIWARI SHARAD et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    ENGINE MOUNT SYSTEM FOR A GAS TURBINE ENGINE

    SUCIU GABRIEL L / MERRY BRIAN D / DYE CHRISTOPHER M et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    Gas turbine engine mount assembly

    SUCIU GABRIEL L / DYE CHRISTOPHER M / MERRY BRIAN D | Europäisches Patentamt | 2017

    Freier Zugriff

    GAS TURBINE ENGINE MOUNT ARRANGEMENT

    LIM CHIA HUI / STRETTON RICHARD / SHEAF CHRISTOPHER | Europäisches Patentamt | 2020

    Freier Zugriff

    GAS TURBINE ENGINE MOUNT ARRANGEMENT

    LIM CHIA HUI / STRETTON RICHARD G / SHEAF CHRISTOPHER T J | Europäisches Patentamt | 2020

    Freier Zugriff