A gas turbine engine includes an aft frame and a forward frame disposed upstream from the aft frame. The forward frame includes an outer ring. The outer ring includes an inner surface that is radially spaced from an outer surface. A first indention is defined in the outer surface, and a first engine mount flange protrudes radially outwardly from the first indention.


    Access

    Download


    Export, share and cite



    Title :

    GAS TURBINE ENGINE MOUNT



    Publication date :

    2024-04-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    GAS TURBINE ENGINE MOUNT ARRANGEMENT

    LIM CHIA HUI / STRETTON RICHARD G / SHEAF CHRISTOPHER T J | European Patent Office | 2020

    Free access

    GAS TURBINE ENGINE MOUNT ARRANGEMENT

    LIM CHIA HUI / STRETTON RICHARD / SHEAF CHRISTOPHER | European Patent Office | 2020

    Free access

    Gas turbine engine mount assembly

    SUCIU GABRIEL L / DYE CHRISTOPHER M / MERRY BRIAN D | European Patent Office | 2017

    Free access

    TURBINE ENGINE CASE MOUNT AND DISMOUNT

    SUCIU GABRIEL L / ALVANOS IOANNIS / MERRY BRIAN | European Patent Office | 2019

    Free access

    AIRCRAFT GAS TURBINE ENGINE MOUNT BAR

    DJUNLEAVI PATRIK / MASSON RISHAR / SEHZ GILEM et al. | European Patent Office | 2015

    Free access