A gas turbine includes a mounting structure for mounting the engine to a pylon. A propulsor section includes a fan having a fan diameter. A geared architecture drives the fan. A generator section includes a fan drive turbine that drives the geared architecture. A turbine to fan diameter ratio is substantially less than 45%.


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    Title :

    PYLON SHAPE WITH GEARED TURBOFAN FOR STRUCTURAL STIFFNESS


    Additional title:

    PYLONFORM MIT GETRIEBETURBOFAN FÜR STRUKTURELLE STEIFIGKEIT
    FORME DE PYLÔNE AVEC TURBOSOUFFLANTE À RÉDUCTEUR POUR RIGIDITÉ STRUCTURALE


    Contributors:

    Publication date :

    2023-10-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02K JET-PROPULSION PLANTS , Strahltriebwerke



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