A gas turbine engine (10) includes a spool (14) along an engine centerline axis (A) which drives a gear train (25), said spool (14) includes a low stage count low pressure turbine (18).


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    Title :

    GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW STAGE PRESSURE TURBINE


    Additional title:

    GASTURBINENMOTOR MIT NIEDERSTUFIGER NIEDERSTUFENDRUCKTURBINE
    MOTEUR À TURBINE À GAZ DOTÉ D'UNE TURBINE BASSE PRESSION AVEC UN FAIBLE NOMBRE D'ÉTAGES


    Contributors:

    Publication date :

    2020-07-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02K JET-PROPULSION PLANTS , Strahltriebwerke



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