A gas turbine engine has a nose cone with a nose cone upstream end and an inlet housing including a plurality of separate flow paths at a housing upstream end which is downstream of the nose cone upstream end. The inlet housing includes a mixing portion downstream of the housing upstream end which mixes airflow from the separate flow paths, such that the airflow is generally around 360 degrees of a rotational axis of the gas turbine engine. A rotor and a turbine drive a shaft to drive the rotor with the shaft including a bearing mounted at a location downstream of the nose cone upstream end.


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    Titel :

    GAS TURBINE ENGINE HAVING A BIFURCATED AIR INLET HOUSING


    Weitere Titelangaben:

    GASTURBINENMOTOR MIT VERZWEIGTEM LUFTEINLASSGEHÄUSE
    TURBINE À GAZ AVEC BOÎTIER D'ADMISSION D'AIR DU TYPE BIFURQUÉ


    Beteiligte:

    Erscheinungsdatum :

    28.08.2019


    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



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