A multi-spool gas turbine engine comprises a low pressure (LP) spool and a high pressure (HP) spool. The LP spool and the HP spool are independently rotatable about an axis. The LP pressure spool has an LP compressor and an LP turbine. The HP spool has an HP turbine and an HP compressor. An accessory gear box (AGB) is axially mounted at one end of the engine. The LP compressor is axially positioned between the HP compressor and the AGB. The AGB is drivingly connected to the HP spool through the center of the LP compressor.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Multi-spool gas turbine engine architecture


    Beteiligte:
    LEFEBVRE GUY (Autor:in)

    Erscheinungsdatum :

    2020-09-08


    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 / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / F02K JET-PROPULSION PLANTS , Strahltriebwerke / F16H Getriebe , GEARING



    Multi-spool gas turbine engine architecture

    LEFEBVRE GUY | Europäisches Patentamt | 2021

    Freier Zugriff

    Gear train architecture for a multi-spool gas turbine engine

    LEFEBVRE GUY | Europäisches Patentamt | 2020

    Freier Zugriff

    SPLIT COMPRESSOR SYSTEM ON MULTI-SPOOL ENGINE

    PLANTE GHISLAIN / MORGAN KEITH / COUTURE-GAGNON VINCENT | Europäisches Patentamt | 2020

    Freier Zugriff

    Twin centrifugal single spool engine

    KUPRATIS DANIEL BERNARD / UTAY ARTHUR W / KASHYAP TANIA BHATIA et al. | Europäisches Patentamt | 2019

    Freier Zugriff

    TWO SPOOL MORE ELECTRICAL ENGINE

    Colin, A. / International Council of the Aeronautical Sciences | British Library Conference Proceedings | 2006