An example gas turbine engine (20) includes a propulsor assembly (62) including at least a fan module (66) and a fan drive turbine module (68); a gas generator assembly (64) including at least a compressor section (52), a combustor (56) in fluid communication with the compressor section (52), and a turbine in fluid communication with the combustor (56); and a geared architecture (48) driven by the fan drive turbine module (68) for rotating a fan (42) of the fan module (66). A weight of the fan module (66) and the fan drive turbine module (68) is less than about 40% of a total weight (EngTOT) of a gas turbine engine (20).
GEARED TURBINE ENGINE WITH RELATIVELY LIGHTWEIGHT PROPULSOR MODULE
GETRIEBETURBINENMOTOR MIT RELATIV LEICHTEM PROPULSOR-MODUL
MOTEUR À TURBINE À ENGRENAGES COMPRENANT UN MODULE PROPULSEUR RELATIVEMENT LÉGER
2020-04-22
Patent
Electronic Resource
English
GEARED TURBINE ENGINE WITH RELATIVELY LIGHTWEIGHT PROPULSOR MODULE
European Patent Office | 2020
|Twin - geared gas turbines power a 10350 kW KaMeWa Water jet propulsor
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Twin-geared gas turbines power a 10,350 kW KaMeWa water jet propulsor
Tema Archive | 1984
Matching propulsion engine with propulsor
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