IP Library Granted Patent US 11,548,102
Granted Patent B2
US 11,548,102 · App. 16/944,914 · Granted Jan 10, 2023

Method for repairing composite components using a plug

Inventors: Herbert Chidsey Roberts (Middletown, OH); Christopher James Scott (Cincinnati, OH)
Assignee: General Electric Company
B23P6/007B23P6/002B29C73/06B29C73/166F01D25/00B29L2031/082F05D2220/32F05D2230/80F05D2300/603
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Quick Facts
Patent No.
US 11,548,102
App. No.
16/944,914
Granted
Jan 10, 2023
Kind
B2
Abstract

A method for repairing composite components includes installing a plug within a feature defined by a composite component, with the plug being formed from one or more neutral materials. Furthermore, the method includes infiltrating the composite component with an infiltrant to densify a repair region of the composite component, with the plug blocking a flow of the infiltrant into the feature. Moreover, after infiltrating the composite component, the method includes removing the plug from the feature.

Claims (29)

1. A method for repairing composite components, the method comprising:

filling a feature defined by a composite component with one or more neutral particulate materials;

compacting the one or more neutral particulate materials to form a plug within the feature;

infiltrating the composite component with an infiltrant to densify a repair region of the composite component, the plug blocking a flow of the infiltrant into the feature; and

after infiltrating the composite component, removing the plug from the feature.

2. The method of claim 1 , wherein the plug entirely fills the feature defined by the composite component.

3. The method of claim 1 , wherein removing the plug from the feature comprises chemically removing the plug from the feature defined by the composite component.

4. The method of claim 1 , wherein removing the plug from the feature comprises mechanically removing the plug from the feature defined by the composite component.

5. The method of claim 1 , wherein the one or more neutral particulate materials include a bond resistant material.

6. The method of claim 5 , wherein the one or more neutral particulate materials include boron nitride.

7. The method of claim 5 , wherein the one or more neutral particulate materials include polytetrafluoroethylene.

8. The method of claim 1 , wherein the feature comprises a hole.

9. The method of claim 1 , wherein the feature comprises a slot.

10. The method of claim 1 , wherein infiltrating the composite component comprises melt infiltrating the composite component with the infiltrant to densify the repair region of the composite component.

11. The method of claim 1 , further comprising:

positioning a repair material on the repair region of the composite component before infiltrating the composite component with the infiltrant.

12. The method of claim 11 , wherein the repair material comprises silicon carbide and the infiltrant comprises silicon.

13. A method for repairing composite turbomachine components, the method comprising:

filling a feature defined by a composite turbomachine component with one or more neutral and bond resistant particulate materials;

compacting the one or more neutral and bond resistant particulate materials to form a plug within the feature;

infiltrating the composite turbomachine component with an infiltrant to densify a repair region of the composite turbomachine component, the plug blocking a flow of the infiltrant into the feature; and

after infiltrating the composite turbomachine component, removing the plug from the feature.

14. The method of claim 13 , wherein the composite turbomachine component comprises a gas turbine engine vane, a gas turbine engine blade, or a gas turbine engine shroud block.

15. The method of claim 13 , wherein removing the plug from the feature comprises chemically removing the plug the from the feature defined by the composite turbomachine component.

16. The method of claim 13 , wherein removing the plug from the feature comprises mechanically removing the plug the from the feature defined by the composite turbomachine component.

17. The method of claim 13 , wherein the plug entirely fills the feature defined by the composite turbomachine component.

18. The method of claim 13 , wherein the one or more neutral particulate materials include a bond resistant material.

19. The method of claim 18 , wherein the one or more neutral particulate materials include boron nitride.

20. The method of claim 18 , wherein the one or more neutral particulate materials include polytetrafluoroethylene.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 31, 2020
From: ROBERTS, HERBERT CHIDSEY; SCOTT, CHRISTOPHER JAMES
To: GENERAL ELECTRIC COMPANY
Reel/Frame 053370/0986 →
Continuity (1)
Related Publication 20220032408A1 · Feb 3, 2022
Cited By (1)
US 12,709,581