A gas turbine engine includes a first annular portion that is stationary and adapted for partially surrounding an engine core. The first annular portion includes a fore pylon connecting portion. A rail is coupled to the fore pylon portion and extends in the aft direction from the stationary portion. A second annular portion is positioned aft of the first portion and coupled to the rail, the second portion being movable along an engine core centerline between a closed position and an open position, wherein the second annular portion is configured to engage with the first annular portion in the closed position to provide access to an engine core. The second annular portion includes a nozzle plug.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Integrated nozzle and plug


    Beteiligte:

    Erscheinungsdatum :

    21.02.2017


    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



    Plug-nozzle flexibility

    Berman, K. / Neuffer, B. | Engineering Index Backfile | 1960


    Charger plug nozzle

    HERMELE JAROSLAV / GARCIA-FERRE FRANCISCO / BORTOLATO MATTEO et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    CHARGER PLUG NOZZLE

    HEMRLE JAROSLAV / GARCIA-FERRE FRANCISCO / BORTOLATO MATTEO et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    Cascade Plug Nozzle

    B. W. Corson | NTIS | 1974


    CHARGER PLUG NOZZLE

    HEMRLE JAROSLAV / GARCIA-FERRE FRANCISCO / BORTOLATO MATTEO et al. | Europäisches Patentamt | 2021

    Freier Zugriff