Ceramic matrix composite repair by reactive processing and mechanical interlocking

Patent metadata

Field	Value
Publication number	US-9366140-B2
Application number	US-201314141976-A
Country	US
Kind code	B2
Filing date	Dec 27, 2013
Priority date	Mar 15, 2013
Publication date	Jun 14, 2016
Grant date	Jun 14, 2016

Abstract

A method for modifying a ceramic matrix component is disclosed including identifying a non-conforming region of a composite component capable of operating in a gas turbine engine; removing at least a portion of the non-conforming region to create an exposed surface of the composite component; preparing a preform in response to the removing at least a portion of the non-conforming region; applying a reactive constituent surface region to at least one of the exposed surface of the composite component and the preform, the reactive constituent surface region being capable of producing a non-equilibrium condition; positioning the preform to provide a contact region between the exposed surface of the composite component and the preform proximate the reactive constituent surface region; and reacting the reactive constituent surface region in an equilibrium reaction at the contact region to form a bond structure between the exposed surface of the composite component and the preform.

First claim

What is claimed is:

1. A method for modifying a ceramic matrix composite component comprising:
removing at least a portion of a non-conforming region of the ceramic matrix composite component to create an exposed surface of the ceramic matrix composite component;
applying a reactive constituent surface region on at least one of the exposed surface of the ceramic matrix composite component or a surface of a perform;
positioning the preform to provide a contact region between the exposed surface of the ceramic matrix composite component and the preform, wherein the reactive constituent surface region is positioned between the ceramic matrix composite component and the perform; and
reacting the reactive constituent surface region in an equilibrium reaction at the contact region to form a bond structure between the ceramic matrix composite component and the preform.

2. The method of claim 1 , wherein removing the at least a portion of the non-conforming region comprises ultrasonically machining the at least a portion of the non-conforming region of the ceramic matrix composite component to create the exposed surface of the ceramic matrix composite component.

3. The method of claim 1 , wherein applying the reactive constituent surface region comprises applying at least a first constituent and a second constituent on the at least one of the exposed surface of the ceramic matrix composite component or the surface of the preform, wherein the first constituent and the second constituent are configured to react in the equilibrium reaction to form the bond structure between the ceramic matrix composite component and the perform.

4. The method of claim 3 , wherein applying the reactive constituent surface region on the at least one of the exposed surface of the ceramic matrix composite component or the surface of the preform comprises:
applying a first plurality of layers on the exposed surface of the ceramic matrix composite component, wherein the first plurality of layers comprises a first outer coating comprising the first constituent, and wherein at least one layer of the first plurality of layers comprises the second constituent and
applying a second plurality of layers on the preform, wherein the second plurality of layers comprises a second outer coating comprising the second constituent, and wherein at least one layer of the second plurality of layers comprises the first constituent.

5. The method of claim 3 , further comprising applying an energy source to the reactive constituent surface region to facilitate the equilibrium reaction.

6. The method of claim 5 , wherein applying the energy source accelerates the equilibrium reaction.

7. The method of claim 5 , wherein applying the energy source initiates the equilibrium reaction.

8. The method of claim 5 , wherein applying the energy source comprises infiltrating the reactive constituent surface region with a eutectic melt material.

9. The method of claim 8 , wherein a non-equilibrium condition between the eutectic melt material and at least one of the first constituent or the second constituent drives the equilibrium reaction.

10. The method of claim 1 , further comprising applying a non-destructive evaluation technique to identify the non-conforming region of the ceramic matrix composite component.

11. The method of claim 3 , wherein applying the reactive constituent surface region comprises forming alternating layers of the first constituent and the second constituent, wherein the first constituent and the second constituent are selected from the group consisting of titanium, zirconium, niobium, vanadium, hafnium, tantalum, molybdenum, chromium, tungsten, silicon, carbon, boron, aluminum, nickel, and combinations thereof.

12. A method for modifying a ceramic matrix composite component comprising:
removing at least a portion of a repairable portion of the ceramic matrix composite component to form a repair surface on the ceramic matrix composite component;
applying a first reaction layer to the repair surface, wherein the first reaction layer comprises a first constituent;
positioning a repair patch to fit against the repair surface of the ceramic matrix composite component, wherein the repair patch comprises a base ceramic matrix composite component and a second reaction layer comprising a second constituent on the base ceramic matrix composite component, wherein the repair patch is positioned with the second reaction layer contacting the first reaction layer, and wherein the first constituent and the second constituent produce a non-equilibrium condition; and
reacting the first constituent and the second constituent in an equilibrium reaction to form a bonding structure between the repair patch and the ceramic matrix composite component.

13. The method of claim 12 , wherein reacting the first constituent and the second constituent in the equilibrium reaction comprises applying an energy source to facilitate the equilibrium reaction.

14. The method of claim 13 , wherein applying the energy source comprises infiltrating the first reaction layer and the second reaction layer with an eutectic melt material.

15. The method of claim 14 , wherein the eutectic melt material comprises at least one of Si, Si—Mo, Si—Zr, Si—Hf, Si—Ti, Si—Mo, Si—Ta, Si—Yb, or Si—Y.

16. The method of claim 12 , wherein removing the at least a portion of the repairable portion of the ceramic matrix composite component forms a repair volume having geometric features, the method further comprising machining the repair patch to form complementing geometric features configured to interlock with the geometric features of the repair volume.

17. The method of claim 12 , wherein the first constituent comprises at least one of titanium, zirconium, niobium, vanadium, hafnium, tantalum, molybdenum, chromium, tungsten, silicon, carbon, boron, aluminum, or nickel.

18. The method of claim 11 , wherein the second constituent includes at least carbon.

Assignees

• Rolls Royce Corp

Inventors

• Chamberlain Adam Lee

Classifications

• C04B35/573

  obtained by reaction sintering {or recrystallisation} · CPC title

• C04B2235/6028

  Shaping around a core which is removed later · CPC title

• B28B1/42

  using mixtures containing fibres, e.g. for making sheets by slitting the wound layer · CPC title

• F01D5/284

  Selection of ceramic materials · CPC title

• B22F2005/103

  Cavity made by removal of insert · CPC title