IP Library Granted Patent US 10,760,529
Granted Patent B2
US 10,760,529 · App. 15/910,827 · Granted Sep 1, 2020

Composite wear pad for exhaust nozzle

Inventors: Donald W. Peters (Colchester, CT); Emma J. Place (New Hartford, CT)
Assignee: RAYTHEON TECHNOLOGY CORPORATION
F02K1/80F01D25/168F02K1/1223F05D2220/32F05D2240/128F05D2260/231F05D2300/434F05D2300/44F05D2300/603F05D2300/614F16C29/001F16C29/02F16C33/201Y02T50/672
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Quick Facts
Patent No.
US 10,760,529
App. No.
15/910,827
Granted
Sep 1, 2020
Kind
B2
Abstract

A composite wear pad for being coupled to a slider block of a convergent nozzle of a gas turbine engine includes a high heat capacity composite having a resin and a plurality of carbon fibers bonded together by the resin. The composite wear pad also includes a first rod coupled to the high heat capacity composite at a first axial end of the composite wear pad such that a first end thickness. The composite wear pad also includes a second rod coupled to the high heat capacity composite at a second axial end of the composite wear pad such that the first axial end and the second axial end of the composite wear pad each have an end thickness that is greater than a middle thickness of the composite wear pad.

Claims (31)

1. A slider block of a convergent nozzle of a gas turbine engine, the slider block comprising:

a body comprising a first end and a second end opposite the first end, wherein a first axial arm extends from the first end and a second axial arm extends from the second end, wherein the first end defines a first slot above the first axial arm and the second end defines a second slot above the second axial arm; and

a wear pad comprising:

a high heat capacity composite having a resin and a plurality of carbon fibers bonded together by the resin;

a first rod coupled to the high heat capacity composite at a first axial end of the wear pad; and

a second rod coupled to the high heat capacity composite at a second axial end of the wear pad;

wherein the first axial end of the wear pad wraps around the first axial arm of the body and the first rod is retained within the first slot;

wherein the second axial end of the wear pad wraps around the second axial arm of the body and the second rod is retained within the second slot; and

wherein the wear pad is configured such that the first axial end and the second axial end of the wear pad each have an end thickness that is greater than a middle thickness of the wear pad.

2. The slider block of claim 1 , wherein the first rod and the second rod are made of a metal material.

3. The slider block of claim 2 , wherein the metal material comprises at least one of steel and titanium.

4. The slider block of claim 1 , wherein the first rod and the second rod are co-cured with the wear pad.

5. The slider block of claim 1 , wherein the first rod, the second rod, and the high heat capacity composite are co-cured with the slider block.

6. A slider block of a convergent nozzle of a gas turbine engine, the slider block comprising:

a body comprising a first end and a second end opposite the first end, wherein a first axial arm extends from the first end and a second axial arm extends from the second end, wherein the first end defines a first slot above the first axial arm and the second end defines a second slot above the second axial arm; and

a wear pad comprising:

a high heat capacity composite having a resin and a plurality of carbon fibers bonded together by the resin;

a first rod coupled to the high heat capacity composite at a first axial end of the wear pad; and

a second rod coupled to the high heat capacity composite at a second axial end of the wear pad;

wherein the first axial end of the wear pad wraps around the first axial arm of the body and the first rod is retained within the first slot;

wherein the second axial end of the wear pad wraps around the second axial arm of the body and the second rod is retained within the second slot; and

wherein the first rod and the second rod are co-cured with the wear pad.

7. A slider block of a convergent nozzle of a gas turbine engine, the slider block comprising:

a body comprising a first end and a second end opposite the first end, wherein a first axial arm extends from the first end and a second axial arm extends from the second end, wherein the first end defines a first slot above the first axial arm and the second end defines a second slot above the second axial arm; and

a wear pad comprising:

a high heat capacity composite having a resin and a plurality of carbon fibers bonded together by the resin;

a first rod coupled to the high heat capacity composite at a first axial end of the wear pad; and

a second rod coupled to the high heat capacity composite at a second axial end of the wear pad;

wherein the first axial end of the wear pad wraps around the first axial arm of the body and the first rod is retained within the first slot;

wherein the second axial end of the wear pad wraps around the second axial arm of the body and the second rod is retained within the second slot; and

wherein the first rod, the second rod, and the high heat capacity composite are co-cured with the slider block.

Assignments (5)
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 →
CHANGE OF NAME Recorded Jul 22, 2020
From: UNITED TECHNOLOGIES CORPORATION
To: RAYTHEON TECHNOLOGIES CORPORATION
Reel/Frame 053287/0528 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 2, 2018
From: PETERS, DONALD W.; PLACE, EMMA J.
To: UNITED TECHNOLOGY CORPORATION
Reel/Frame 045094/0203 →
Continuity (2)
Division 14709072 · May 11, 2015
Related Publication 20180238268A1 · Aug 23, 2018