An exhaust system for a gas turbine engine, such as an APU, comprises a pressure vessel having an annular wall circumscribing an exhaust plenum. The annular wall is composed of an arrangement of individual tubes assembled side-by-side around a central axis of the exhaust plenum. The tubes are fed with pressurized cooling air, such as P3 air. A heat exchanger in heat transfer relationship with the exhaust gases flowing through the exhaust plenum receives air from the tubes. The heat transferred from the exhaust gases to the air circulated through the heat exchanger may be used to provide pre-heated air to the engine combustor.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    GAS TURBINE ENGINE EXHAUST SYSTEM


    Weitere Titelangaben:

    SYSTEME D'ECHAPPEMENT DE TURBINE A GAZ


    Beteiligte:
    MENHEERE DAVID (Autor:in) / TRUMPOUR ADAM (Autor:in)

    Erscheinungsdatum :

    02.03.2018


    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 / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F02K JET-PROPULSION PLANTS , Strahltriebwerke / F28D Wärmetauscher, soweit in keiner anderen Unterklasse vorgesehen, in denen die Wärmetauschmittel nicht in direkte Berührung miteinander kommen , HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT



    Turbine engine exhaust nozzle performance

    WEHOFER, S. / MATZ, R. | AIAA | 1973


    Gas turbine engine exhaust component

    EASTWOOD JONATHAN JEFFERY / HART ADAM LEE / CRAIG BRIAN et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    Exhaust centerbody for a turbine engine

    POUYAU GUILLAUME / SIRVIN NICOLAS | Europäisches Patentamt | 2017

    Freier Zugriff

    EXHAUST NOZZLE FOR GAS TURBINE ENGINE

    HOLT GAVIN JOSEPH / IGLEWSKI TOMASZ / HOLLAND JOHN ROBERT | Europäisches Patentamt | 2017

    Freier Zugriff

    EXHAUST NOZZLE FOR GAS TURBINE ENGINE

    HOLT GAVIN JOSEPH / IGLEWSKI TOMASZ / HOLLAND JOHN ROBERT | Europäisches Patentamt | 2017

    Freier Zugriff