A system for mounting a gas turbine engine to a pylon on a wing of an aircraft. At least one 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 each comprise a respective winch operable to adjust pay out of a respective tension member thereby to provide length adjustment. The temporary forward link and the temporary rearward link 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.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    MOUNTING SYSTEM AND MOUNTING METHOD FOR GAS TURBINE AERO ENGINE


    Beteiligte:

    Erscheinungsdatum :

    2019-11-28


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Mounting system and mounting method for gas turbine aero engine

    COOPER JOSEPH B | Europäisches Patentamt | 2022

    Freier Zugriff

    Mounting system and mounting method for gas turbine aero engine

    COOPER JOSEPH B | Europäisches Patentamt | 2022

    Freier Zugriff

    MOUNTING SYSTEM AND MOUNTING METHOD FOR GAS TURBINE AERO ENGINE

    COOPER JOSEPH B | Europäisches Patentamt | 2019

    Freier Zugriff

    MOUNTING SYSTEM AND MOUNTING METHOD FOR GAS TURBINE AERO ENGINE

    COOPER JOSEPH | Europäisches Patentamt | 2019

    Freier Zugriff

    MOUNTING SYSTEM AND MOUNTING METHOD FOR GAS TURBINE AERO ENGINE

    COOPER JOSEPH | Europäisches Patentamt | 2021

    Freier Zugriff