A gas turbine includes a mounting structure for mounting the engine to a pylon. A propulsor section includes a fan having a fan diameter. A geared architecture drives the fan. A generator section includes a fan drive turbine that drives the geared architecture. A turbine to fan diameter ratio is substantially less than 45%.
ASSEMBLY COMPRISING A GEARED TURBOFAN, A PYLON AND A WING
ANORDNUNG UMFASSEND EINEN GETRIEBEFAN, EINE AUFHÄNGUNG UND EINE TRAGFLÄCHE
ASSEMBLAGE COMPRENANT UN MOTEUR À DOUBLE FLUX À ENGRENAGE, UN MÂT DE LIAISON ET UNE AILE
2020-05-06
Patent
Electronic Resource
English
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