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US 2012/0237335 A1Published application
Gas turbine engine with geared architecture
AssigneeUnited Technologies Corporation
InventorsMichael E. McCune, Lawrence E. Portlock, Frederick M. Schwarz
Life of this patent
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Abstract
A geared architecture with a flex mount for a fan drive gear system.
Claims15
A geared architecture for a gas turbine engine comprising:
- a fan shaft;
- a frame which supports said fan shaft;
- a gear system which drives said fan shaft;
- a torque frame which at least partially supports said gear system;
- and
- an input coupling to said gear system.
3 more elements
Dependencies are inferred from the claim text.