A system for mounting a gas turbine engine to a pylon on a wing of an aircraft. A temporary forward link, being length-adjustable, and at least one temporary rearward link, being length-adjustable, are provided. These are for temporarily attaching the gas turbine engine to the pylon. The temporary forward link and the temporary rearward link are each adapted to resist tension and compression, to maintain a positional relationship between the gas turbine engine and the pylon in the absence of adjustment of the lengths of the temporary forward link and the temporary rearward link. Adjustment of the length of the temporary links brings engine mounts into alignment with pylon mounts for service attachment of the gas turbine engine to the pylon.


    Access

    Download


    Export, share and cite



    Title :

    MOUNTING SYSTEM AND MOUNTING METHOD FOR GAS TURBINE AERO ENGINE


    Contributors:

    Publication date :

    2019-11-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    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



    Mounting system and mounting method for gas turbine aero engine

    COOPER JOSEPH B | European Patent Office | 2022

    Free access

    MOUNTING SYSTEM AND MOUNTING METHOD FOR GAS TURBINE AERO ENGINE

    COOPER JOSEPH B | European Patent Office | 2019

    Free access

    MOUNTING SYSTEM AND MOUNTING METHOD FOR GAS TURBINE AERO ENGINE

    COOPER JOSEPH | European Patent Office | 2019

    Free access

    Mounting system and mounting method for gas turbine aero engine

    COOPER JOSEPH B | European Patent Office | 2022

    Free access

    MOUNTING SYSTEM AND MOUNTING METHOD FOR GAS TURBINE AERO ENGINE

    COOPER JOSEPH | European Patent Office | 2021

    Free access