Flexible support structure for a geared architecture gas turbine engine
First Claim
Patent Images
1. A geared architecture for a gas turbine engine comprising:
- a fan shaft;
a frame which supports said fan shaft, said frame defines a frame transverse stiffness;
a gear system which drives said fan shaft;
a flexible support which at least partially supports said gear system, said flexible support defines a flexible support transverse stiffness with respect to said frame transverse stiffness; and
an input coupling to said gear system, said input coupling defines an input coupling transverse stiffness with respect to said frame transverse stiffness.
4 Assignments
0 Petitions
Accused Products
Abstract
A geared architecture with a flex mount for a Fan Drive Gear System defined by a transverse stiffness relationship.
52 Citations
28 Claims
-
1. A geared architecture for a gas turbine engine comprising:
-
a fan shaft; a frame which supports said fan shaft, said frame defines a frame transverse stiffness; a gear system which drives said fan shaft; a flexible support which at least partially supports said gear system, said flexible support defines a flexible support transverse stiffness with respect to said frame transverse stiffness; and an input coupling to said gear system, said input coupling defines an input coupling transverse stiffness with respect to said frame transverse stiffness. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18)
-
-
19. 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, said gear system includes a gear mesh that defines a gear mesh transverse stiffness; a flexible support which at least partially supports said gear system, said flexible support defines a flexible support transverse stiffness with respect to said gear mesh transverse stiffness; and an input coupling to said gear system, said input coupling defines an input coupling transverse stiffness with respect to said gear mesh transverse stiffness. - View Dependent Claims (20, 21, 22, 23, 24, 25, 26, 27, 28)
-
Specification