An auxiliary power unit (APU) includes, in serial flow communication: an engine compressor, a combustor and a turbine, the turbine rotatable about an engine axis. A first shaft operatively connects the turbine to the engine compressor and extends non-parallel to the engine axis. A second shaft operatively connects the turbine to a load and extends non-parallel to the engine axis. A method of operating an APU is also described.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    GAS TURBINE AUXILIARY POWER UNIT


    Weitere Titelangaben:

    GROUPE AUXILIAIRE DE PUISSANCE POUR TURBINE A GAZ


    Beteiligte:
    REDFORD TIMOTHY (Autor:in) / MENHEERE DAVID (Autor:in)

    Erscheinungsdatum :

    24.12.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    GAS TURBINE AUXILIARY POWER UNIT

    ELEFTHERIOU ANDREAS / ALECU DANIEL / MACCHIA ENZO | Europäisches Patentamt | 2020

    Freier Zugriff

    Gas turbine auxiliary power unit

    ELEFTHERIOU ANDREAS / ALECU DANIEL / MACCHIA ENZO | Europäisches Patentamt | 2021

    Freier Zugriff


    Gas turbine auxiliary power unit noise and its attenuation

    Dias, J.J. | Engineering Index Backfile | 1967