IP Library › Granted Patent US 10,094,220
Granted Patent B2
US 10,094,220 · App. 14/773,441 · Granted Oct 9, 2018

Turbine engine repair methods

Inventors: John H. Vontell, Sr. (Manchester, CT); Charles R. Watson (Windsor, CT)
Assignee: United Technologies Corporation
F01D5/005B29C73/10B32B7/06B32B27/283C09J183/06F01D5/288B29K2083/00B29K2105/0097B29L2031/08B29L2031/7504B32B2307/748B32B2556/00F05D2220/32F05D2220/36F05D2230/10F05D2230/23F05D2230/80F05D2300/222F05D2300/40F05D2300/437F05D2300/601F05D2300/603
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Quick Facts
Patent No.
US 10,094,220
App. No.
14/773,441
Granted
Oct 9, 2018
Kind
B2
Abstract

A method for patching a damaged polymeric erosion coating ( 250 ) on a gas turbine engine component. The method comprises removing a portion of the coating around a damage site ( 200; 202; 204 ) and applying a pre-formed coating patch ( 220 ).

Claims (33)

1. A method for patching a damaged polymeric erosion coating ( 250 ) on a gas turbine engine component, the method comprising:

removing a portion of the coating around a damage site ( 200 ; 202 ; 204 ); and

applying a pre-formed coating patch ( 220 ); wherein the patch comprises: a molded cured silicone body; a silane primer on an underside of the body; a silicone adhesive on the primer; and a release strip on the adhesive, the method comprising removing the release strip before applying the patch.

2. The method of claim 1 further comprising:

priming the component.

3. The method of claim 2 wherein:

the priming is with a silane primer.

4. The method of claim 1 further comprising:

applying a vacuum to the patch.

5. The method of claim 4 wherein:

the vacuum is applied via a vacuum blanket ( 260 ).

6. The method of claim 4 further comprising:

heating the patch while the vacuum is applied.

7. The method of claim 6 wherein:

the heating is an internal heating via an anti-icing system ( 280 ).

8. The method of claim 1 wherein:

the method is performed in situ with the engine on an aircraft.

9. The method of claim 1 wherein:

the damage site is along a fan inlet strut ( 206 ) or fan exit strut ( 29 ).

10. The method of claim 1 wherein:

the damage site has a polymer matrix composite substrate ( 240 ).

11. A patch ( 220 ) comprising:

a molded cured silicone body ( 227 );

a silane primer ( 224 ) on an underside of the body;

a silicone adhesive on the primer ( 226 ); and

a release strip on the adhesive ( 228 ).

12. The patch of claim 11 wherein:

the adhesive is a peroxide-cured silicone.

13. A method for manufacturing a patch comprising a silicone body; a silane primer on an underside of the body; a silicone adhesive on the primer; and a release strip on the adhesive, the method comprising:

molding and curing the body;

preparing the underside by mechanical abrasion or plasma treating;

applying the primer to the underside after the preparing; and

applying the adhesive to the primer.

Assignments (3)
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 →
Continuity (2)
Provisional Application 61794571 · Mar 15, 2013
Related Publication 20160017712A1 · Jan 21, 2016
Cited By (4)
US 12,392,244 US 12,637,947 US 12,643,298 US 12,650,077