IP Library Granted Patent US 10,697,323
Granted Patent B2
US 10,697,323 · App. 15/216,180 · Granted Jun 30, 2020

Engine bearing damper with interrupted oil film

Inventor: Matthew J. Forcier (Rocky Hill, CT)
Assignee: Raytheon Technologies Corporation
F01D25/164F01D25/183F02C3/04F02C7/06F04D29/059F16C19/16F16C33/6674F16C33/6677F16C35/04F16C35/077F05D2220/32F05D2240/60
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Quick Facts
Patent No.
US 10,697,323
App. No.
15/216,180
Granted
Jun 30, 2020
Kind
B2
Abstract

Aspects of the disclosure are directed to an engine oil damper comprising: a bearing support, and a housing radially outward from the bearing support and co-axial with the bearing support, where at least one oil flow restrictor is formed with respect to at least one of the bearing support and the housing, where the at least one oil flow restrictor is configured to at least partially interrupt a flow of oil in an annulus radially defined between the bearing support and the housing.

Claims (31)

1. An engine oil damper having an axial centerline, the engine oil damper comprising:

a bearing support;

a housing radially outward from the bearing support and co-axial with the bearing support; and

a plurality of oil flow restrictors extending radially a first radial distance from a floor, defined by at least one of a radially outermost surface of the bearing support and a radially innermost surface of the housing, to a ceiling, which is less than a second radial distance extending from the bearing support to the housing so as to define a clearance radially adjacent the ceiling, the plurality of oil flow restrictors circumferentially spaced from one another;

wherein the plurality of oil flow restrictors is configured to at least partially restrict a flow of oil in an annulus radially defined between the bearing support and the housing;

wherein each of the plurality of oil flow restrictors includes the ceiling defining a distal surface of the respective oil flow restrictor with respect to the floor and first and second walls that project in a substantially radial reference direction between and connect the floor and the ceiling; and

wherein the bearing support includes at least one stop clearance extending radially from the floor of the bearing support and wherein the respective ceiling of each of the plurality of oil flow restrictors is radially inward of a radially outer surface of the at least one stop clearance.

2. The engine oil damper of claim 1 , wherein a first dimension of a first of the plurality of oil flow restrictors is different from a second counterpart dimension of a second of the plurality of oil flow restrictors.

3. The engine oil damper of claim 1 , wherein the plurality of oil flow restrictors includes at least three oil flow restrictors, and wherein a first spacing between circumferentially adjacent first and second oil flow restrictors of the at least three oil flow restrictors is different from a second spacing between circumferentially adjacent second and third oil flow restrictors of the at least three oil flow restrictors.

4. The engine oil damper of claim 1 , wherein each of the plurality of oil flow restrictors extends radially inward from the floor of the housing.

5. The engine oil damper of claim 1 , wherein each of the plurality of oil flow restrictors extends radially outward from the floor of the bearing support.

6. The engine oil damper of claim 5 , wherein a clearance between the bearing support and the housing varies around a circumference of the damper.

7. The engine oil damper of claim 6 , wherein the clearance between the bearing support and the housing varies between a maximum value defined by the floor of the bearing support and a minimum value defined by the respective ceiling of each of the plurality of oil flow restrictors.

8. The engine oil damper of claim 1 , further comprising:

a first seal; and

a second seal axially spaced from the first seal,

wherein the annulus is axially defined between the first seal and the second seal.

9. The engine oil damper of claim 1 , wherein the annulus is continuous around a circumference of the damper.

10. The engine oil damper of claim 1 , further comprising:

an axial seal extending from at least one of the plurality of oil flow restrictors.

11. An engine comprising:

a compressor;

a combustor located axially aft of the compressor;

a turbine located axially aft of the combustor;

a shaft coupled to the compressor and the turbine; and

an engine oil damper having an axial centerline, the engine oil damper including:

a bearing support coupled to the shaft, the bearing support having a circumferentially extending outer radial surface with a plurality of first portions disposed at a first radial distance from the axial centerline, and a plurality of second portions disposed at a second radial distance from the axial centerline, wherein the second radial distance is greater than the first radial distance, and each of the plurality of second portions is spaced apart from another of the plurality of second portions by one of the plurality of first portions; and

a housing disposed radially outward from the bearing support and co-axial with the bearing support, and having an inner radial surface disposed at a third radial distance from the axial centerline, wherein the third radial distance is greater than the second radial distance;

wherein the plurality of second portions of the circumferentially extending outer radial surface is radially spaced from the housing so as to define a radial clearance therebetween;

wherein the plurality of second portions are configured to at least partially restrict a flow of oil in an annulus radially defined between the bearing support and the housing; and

wherein the bearing support includes a stop clearance extending radially outward from an axial end of the circumferentially extending outer radial surface of the bearing support and each of the plurality of second portions is radially inward of a radially outer surface of the stop clearance.

Assignments (4)
CHANGE OF NAME Recorded Jul 27, 2023
From: RAYTHEON TECHNOLOGIES CORPORATION
To: RTX CORPORATION
Reel/Frame 064714/0001 →
CORRECTIVE ASSIGNMENT TO CORRECT THE AND REMOVE PATENT APPLICATION NUMBER 11886281 AND ADD PATENT APPLICATION NUMBER 14846874. TO CORRECT THE RECEIVING PARTY ADDRESS PREVIOUSLY RECORDED AT REEL: 054062 FRAME: 0001. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF ADDRESS. Recorded Mar 4, 2021
From: UNITED TECHNOLOGIES CORPORATION
To: RAYTHEON TECHNOLOGIES CORPORATION
Reel/Frame 055659/0001 →
CHANGE OF NAME Recorded Sep 4, 2020
From: UNITED TECHNOLOGIES CORPORATION
To: RAYTHEON TECHNOLOGIES CORPORATION
Reel/Frame 054062/0001 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 21, 2016
From: FORCIER, MATTHEW J.
To: UNITED TECHNOLOGIES CORPORATION
Reel/Frame 039214/0077 →
Continuity (1)
Related Publication 20180023418A1 · Jan 25, 2018