Bearing locking assemblies and methods of assembling the same

Patent metadata

Field	Value
Publication number	US-2016341073-A1
Application number	US-201415111077-A
Country	US
Kind code	A1
Filing date	Dec 5, 2014
Priority date	Jan 15, 2014
Publication date	Nov 24, 2016
Grant date	—

Abstract

A bearing assembly for use in a gas turbine engine is provided. The bearing assembly includes a bearing retainer having an inner portion, an outer portion spaced radially apart from the inner portion, and an intermediate portion connecting the inner portion and the outer portion, wherein the inner portion and the outer portion define a space there-between. The bearing assembly also includes a bearing housing having an extended portion positioned within the space. The bearing assembly also includes a locking assembly comprising a locking plate and an axial keyway that extends axially away from the locking plate. The locking plate is coupled to the bearing retainer and the axial keyway is coupled to the extended portion of the bearing housing.

First claim

What is claimed is:

1 . A bearing assembly comprising:
a bearing retainer including an inner portion, an outer portion spaced radially apart from the inner portion, and an intermediate portion connecting the inner portion and the outer portion, wherein the inner portion and the outer portion define a space there-between; a bearing housing having an extended portion positioned within the space; and a locking assembly comprising a locking plate and an axial keyway that extends axially away from the locking plate and toward the bearing housing, wherein the locking plate is coupled to the bearing retainer and the axial keyway is coupled to the extended portion of the bearing housing.

2 . A bearing assembly according to claim 1 , wherein the intermediate portion has a first axial end and a second axial end, and a window is defined through a part of the intermediate portion from the first axial end to the second axial end.

3 . A bearing assembly according to claim 2 , wherein the window is substantially rectangular in shape, and is sized to receive the axial keyway.

4 . A bearing assembly according to claim 2 , wherein the axial keyway extends through the window, and couples with the extended portion of the bearing housing.

5 . A bearing assembly according to claim 1 , wherein the locking assembly is removably secured to the bearing retainer and to the bearing housing.

6 . A bearing assembly according to claim 1 , wherein the axial keyway defines a cavity in the aft axial end of the axial keyway, and the cavity is configured to receive a part of the extended portion of the bearing housing.

7 . A bearing assembly according to claim 6 , wherein the cavity includes a plurality of retention features, the extended portion includes a plurality of corresponding machined slots, and the retention features and corresponding machined slots securely engage the axial keyway and the extended portion.

8 . A bearing assembly according to claim 1 , further comprising a plurality of locking assemblies spaced circumferentially about the periphery of the bearing retainer.

9 . A bearing assembly according to claim 1 , wherein the locking assembly is an annular ring having a plurality of axial keyways spaced about the periphery of the ring, wherein each of the plurality of axial keyways is configured to extend through a corresponding window in the bearing retainer.

10 . A bearing assembly according to claim 1 , wherein the bearing retainer defines a plurality of self-locking inserts configured to receive respective retaining elements that secure the locking plate to the bearing retainer.

11 . A bearing assembly according to claim 10 , wherein the retaining elements are at least one of a bolt, a screw, a cotter pin, a lockwire, and a polymeric compound.

12 . A locking assembly for use in a gas turbine engine, the locking assembly comprising:
a substantially flat locking plate that defines at least one slot; an axial keyway coupled to the flat locking plate and extending axially outward from the locking plate, wherein the axial keyway is configured to be inserted through a window of a bearing retainer and coupled to a bearing housing; and at least one retaining element configured to be inserted through a respective slot of the locking plate such that the locking plate is secured to the bearing retainer.

13 . The locking assembly of claim 12 , wherein an aft axial end of the axial keyway defines a cavity configured to receive a portion of the bearing housing.

14 . The locking assembly of claim 13 , wherein a plurality of retaining features extend from the axial keyway to the cavity, and the plurality of retaining features are configured to engage with corresponding slots on the bearing housing.

15 . A method of assembling a bearing assembly for use in a gas turbine engine, the method comprising:
positioning an extended portion of a bearing housing between an inner portion and an outer portion of a bearing retainer, wherein the inner portion is radially spaced from the outer portion and an intermediate portion connects the inner portion and the outer portion; defining a window in the intermediate portion of the bearing retainer, wherein the window extends from a first axial end to a second axial end of the intermediate portion; coupling an axial keyway to a locking plate, wherein the axial keyway extends axially away from the locking plate; coupling the locking plate to the bearing retainer; inserting the axial keyway through the window; and coupling the axial keyway with the extended portion of the bearing housing.

Assignees

• Gen Electric

Inventors

• Carter Bruce Alan
• Ganiger Ravindra Shankar
• Wainwright Richard Charles
• Moongilpalayam Chenniappan Venkatachalapathy
• Chelstowski Krzysztof

Classifications

• F16C19/06

  with a single row or balls · CPC title

• F16C35/067

  Fixing them in a housing (with interposition of an element F16C35/07) · CPC title

• F16C2360/23

  Gas turbine engines · CPC title

• F05D2230/60

  Assembly methods · CPC title

• F05D2220/32

  in gas turbines · CPC title