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%.
PYLON SHAPE WITH GEARED TURBOFAN FOR STRUCTURAL STIFFNESS
2021-07-01
Patent
Electronic Resource
English
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