Epicyclic gear reduction carrier and torque frame connection
AssigneeRtx Corporation
InventorsAlessio Pescosolido, David A. Carroll
Life of this patent
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AssigneeRtx Corporation
InventorsAlessio Pescosolido, David A. Carroll
Estimating the term…
A gas turbine engine includes a turbine section having at least one turbine rotor. A compressor section includes at least one compressor rotor, and a propulsor. The at least one turbine rotor is connected to drive an epicyclic gear reduction to in turn drive the propulsor at a slower speed than the at least one turbine rotor. The epicyclic gear reduction includes a sun gear for receiving a drive input from the at least one turbine rotor and having gear teeth engaging gear teeth on a plurality of intermediate gears. The intermediate gears are mounted within a carrier. The teeth on the intermediate gears also engage teeth on a ring gear. One of the carrier and the ring gear is connected to drive a propulsor drive shaft to in turn drive the propulsor, and the other of the carrier and the ring gear connected to static structure, with the carrier connected to either the propulsor drive shaft or the static structure through a torque frame. The torque frame is connected to the carrier at a radially outer location through a splined connection.
A gas turbine engine comprising:
A gas turbine engine comprising:
A gas turbine engine comprising:
Dependencies are inferred from the claim text.