A gas generator (22) has at least one compressor rotor (24), at least one gas generator turbine rotor (30) and a combustion section (32). A fan drive turbine (36) is positioned downstream of a path of the products of combustion having passed over the at least one gas generator turbine rotor (30). The fan drive turbine (36) drives a shaft (40) and the shaft engages gears to drive at least three fan rotors (42,44,46,48).
GAS TURBINE ENGINE WITH DISTRIBUTED FANS
GASTURBINENMOTOR MIT VERTEILTEN GEBLÄSEN
MOTEUR À TURBINE À GAZ AVEC SOUFFLANTES RÉPARTIES
2022-01-05
Patent
Electronic Resource
English
IPC: | F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F02K JET-PROPULSION PLANTS , Strahltriebwerke |