IP Library › Granted Patent US 12680472
Granted Patent B2
US 12680472 · App. 18/926,479 · Granted Jul 14, 2026

Strut for bearing assembly and method for removing strut

Inventor: Richard Meyer (Derby, GB)
Assignee: Rolls-Royce PLC
F01D25/162F05D2220/32F05D2230/70F05D2240/50
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Quick Facts
Patent No.
US 12680472
App. No.
18/926,479
Granted
Jul 14, 2026
Kind
B2
Abstract

A strut for a bearing assembly of a gas turbine engine. The bearing assembly has a first bearing structure and a second bearing structure. The strut includes a first mounting end portion, a second mounting end portion spaced apart from the first mounting end portion, and a shaft portion extending between the first mounting end portion and the second mounting end portion along a longitudinal axis. The first mounting end portion is configured to be attached to the first bearing structure thereby forming an interference fit between the first mounting end portion and the first bearing structure. The second mounting end portion is configured to be attached to the second bearing structure. The first mounting end portion includes at least one relief feature.

Claims (28)

1 . A strut for a bearing assembly of a gas turbine engine, the bearing assembly having a first bearing structure and a second bearing structure, the strut comprising:

a first mounting end portion, a second mounting end portion spaced apart from the first mounting end portion, and a shaft portion extending between the first mounting end portion and the second mounting end portion along a longitudinal axis;

wherein the first mounting end portion is configured to be attached to the first bearing structure of the bearing assembly thereby forming an interference fit between the first mounting end portion and the first bearing structure;

the second mounting end portion is configured to be attached to the second bearing structure of the bearing assembly;

the first mounting end portion includes at least one relief feature formed therein to facilitate the removal of the first mounting end portion from the first bearing structure and thereafter the removal of the second mounting end portion from the second bearing structure; and

a length of the at least one relief feature along the longitudinal axis is substantially equal to a length of the first mounting end portion along the longitudinal axis.

2 . The strut of claim 1 , wherein the first mounting end portion includes an outer surface forming the interference fit with the first bearing structure, and wherein the at least one relief feature is disposed on the outer surface.

3 . The strut of claim 1 , wherein the first mounting end portion includes a wall having a wall thickness, wherein the at least one relief feature has a maximum depth perpendicular to the longitudinal axis, and wherein the maximum depth is at most two-thirds of the wall thickness of the first mounting end portion.

4 . The strut of claim 1 , wherein the at least one relief feature has a curved profile.

5 . The strut of claim 4 , wherein the curved profile is a circular arc.

6 . The strut of claim 1 , wherein the at least one relief feature is a single relief feature.

7 . The strut of claim 1 , wherein the at least one relief feature includes a pair of diametrically opposite relief features.

8 . A bearing assembly for a gas turbine engine, the bearing assembly comprising:

a first bearing structure;

a second bearing structure spaced apart from the first bearing structure; and

a strut of claim 1 , wherein the first mounting end portion is attached to the first bearing structure thereby forming an interference fit between the first mounting end portion and the first bearing structure, and wherein the second mounting end portion is attached to the second bearing structure.

9 . A gas turbine engine including the bearing assembly of claim 8 .

10 . A method for removing a strut from a bearing assembly, the bearing assembly having a first bearing structure and a second bearing structure, the strut comprising:

a first mounting end portion, a second mounting end portion spaced apart from the first mounting end portion, and a shaft portion extending between the first mounting end portion and the second mounting end portion along a longitudinal axis;

wherein the first mounting end portion is configured to be attached to the first bearing structure of the bearing assembly thereby forming an interference fit between the first mounting end portion and the first bearing structure;

the second mounting end portion is configured to be attached to the second bearing structure of the bearing assembly; and

the first mounting end portion includes at least one relief feature formed therein to facilitate the removal of the first mounting end portion from the first bearing structure and thereafter the removal of the second mounting end portion from the second bearing structure;

the method comprising the steps of:

cutting the shaft portion of the strut proximally to the first mounting end portion to form a cut surface of the first mounting end portion;

drilling a pilot hole located at the radial center of the cut surface of the first mounting end portion;

progressively increasing a drill diameter of the pilot hole until the drill diameter of the pilot hole breaks through the at least one relief feature; and

removing the first mounting end portion from the first bearing structure of the bearing assembly.

11 . The method of claim 10 , further comprising removing the second mounting end portion from the second bearing structure after removal of the first mounting end portion from the first bearing structure.