An engine assembly including an engine core with at least one internal combustion engine, a first casing, a turbine module including a second casing located outside of the first casing, and a compressor module including a third casing located outside of the first and second casings. The turbine shaft extends into the first casing, is rotationally supported by a bearings all contained within the first casing, and is free of rotational support within the second casing. The first casing may be a gearbox module casing through which the turbine shaft is in driving engagement with the engine shaft. A method of driving a rotatable load of an aircraft, and an engine assembly with a rotary engine core, a gearbox module with a first casing, and a second module including a second casing located outside of the first casing and detachably connected to the first casing are also discussed.


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    Titel :

    ENGINE ASSEMBLY WITH MODULAR COMPRESSOR AND TURBINE


    Weitere Titelangaben:

    MOTORANORDNUNG MIT MODULAREM VERDICHTER UND TURBINE
    ENSEMBLE MOTEUR À COMPRESSEUR ET TURBINE MODULAIRES


    Beteiligte:
    LAMARRE SYLVAIN (Autor:in) / FONTAINE MIKE (Autor:in) / JULIEN ANDRE (Autor:in) / GAUL MICHAEL (Autor:in) / THOMASSIN JEAN (Autor:in) / MITROVIC LAZAR (Autor:in) / MEDVEDEV ILYA (Autor:in) / USIKOV SERGEY (Autor:in) / ZOLOTOV ANDREY (Autor:in)

    Erscheinungsdatum :

    2020-01-08


    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 / F01C Rotationskolben- oder Schwenkkolbenmaschinen, Rotationskolben- oder Schwenkkolbenkraftmaschinen , ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES



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