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).
GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW STAGE PRESSURE TURBINE
GASTURBINENMOTOR MIT NIEDERSTUFIGER NIEDERSTUFENDRUCKTURBINE
MOTEUR À TURBINE À GAZ DOTÉ D'UNE TURBINE BASSE PRESSION AVEC UN FAIBLE NOMBRE D'ÉTAGES
01.07.2020
Patent
Elektronische Ressource
Englisch
Gas turbine engine with low stage count low pressure turbine
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