A gas turbine engine according to an example of the present disclosure includes a mount arrangement including a gas turbine engine, an adapter ring extending circumferentially around the gas turbine engine and mounted to both the gas turbine engine and to an aircraft beneath the gas turbine engine, and at least one thrust link including a first end mounted to the gas turbine engine fore of the adapter ring, and an opposite second end mounted to the adapter ring above the gas turbine engine.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    ADAPTER RING FOR ABOVE-WING MOUNTING OF BELOW-WING ENGINE


    Beteiligte:

    Erscheinungsdatum :

    2019-01-31


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    ADAPTER RING FOR ABOVE-WING MOUNTING OF BELOW-WING ENGINE

    SUCIU GABRIEL L / CHANDLER JESSE M | Europäisches Patentamt | 2021

    Freier Zugriff

    Aircraft Wing for Over-The-Wing Mounting of Engine Nacelle

    Hahn, Andrew S. / Kinney, David J. | NTRS | 2011


    WING MOUNTING

    LAFON PAUL | Europäisches Patentamt | 2018

    Freier Zugriff

    Aircraft engine pylon to wing mounting assembly

    CASTELLI ALBERTO DEI / FERREIRA CLOVIS AUGUSTO EÇA / MONTORO WANDERLEY et al. | Europäisches Patentamt | 2018

    Freier Zugriff

    AIRCRAFT ENGINE PYLON TO WING MOUNTING ASSEMBLY

    DA SILVA JULIO ANTONIO BELTRAMI / FERREIRA CLOVIS AUGUSTO EÇA / MONTORO WANDERLEY et al. | Europäisches Patentamt | 2019

    Freier Zugriff