Composite component modifications

Patent metadata

Field	Value
Publication number	US-12152500-B2
Application number	US-201816003627-A
Country	US
Kind code	B2
Filing date	Jun 8, 2018
Priority date	Jun 8, 2018
Publication date	Nov 26, 2024
Grant date	Nov 26, 2024

Abstract

Composite components and methods for adding a composite material to a composite component are provided. For example, a method comprises positioning a composite material segment against the composite component to form a component layup; applying an insulating material around at least a portion of the component layup to form an insulated layup; and densifying the insulated layup, where the composite component was previously densified before positioning the composite material segment against the composite component. In some embodiments, the composite material is ceramic matrix composite (CMC) and the composite material segment is a plurality of CMC plies. The composite component may be a CMC gas turbine engine component that comprises an original CMC component and a new CMC material segment joined to the original CMC component through the transfer of silicon between the original CMC component and the new CMC material segment during melt infiltration.

First claim

What is claimed is:

1. A method for adding a composite material to a previously densified composite component, the method comprising:
positioning a composite material segment against the previously densified composite component to form a component layup;
temporarily applying, without bonding, a silicon-based insulating material against at least a portion of previously densified outer surfaces of the component layup to form an insulated layup,
wherein the silicon-based insulating material comprises, by dry weight, ≥25% and ≤95% silicon and >0% and <50% boron nitride;
densifying the insulated layup; and
removing the silicon-based insulating material after densifying the insulated layup.

2. The method of claim 1 , wherein positioning the composite material segment against the previously densified composite component comprises positioning a plurality of composite material plies against the previously densified composite component, the plurality of composite material plies and the previously densified composite component forming the component layup.

3. The method of claim 2 , wherein each composite material ply of the plurality of composite material plies comprises fibers extending generally along a longitudinal direction L 1 defined by the composite material ply,
wherein a first composite material ply of the plurality of composite material plies is positioned against the previously densified composite component and a remainder of the plurality of composite material plies are stacked against the first composite material ply, and
wherein an orientation of the plurality of composite material plies is varied such that the fibers of at least one ply of the plurality of composite material plies are oriented in a different direction with respect to a longitudinal direction L 2 defined by the previously densified composite component.

4. The method of claim 1 , wherein densifying the insulated layup includes melt infiltrating the insulated layup.

5. The method of claim 1 , wherein, when the insulated layup is densified, a locally high silicon vapor pressure is created at the previously densified composite component.

6. The method of claim 1 , further comprising:
preparing a damaged area for repair prior to positioning the composite material segment against the previously densified composite component,
wherein positioning the composite material segment against the previously densified composite component comprises positioning the composite material segment at the damaged area.

7. The method of claim 1 , further comprising:
selectively applying a coating to a region of the previously densified outer surfaces of the component layup prior to applying the silicon-based insulating material, and leaving one or more portions of the previously densified outer surfaces uncoated.

8. The method of claim 7 , wherein the coating is a non-organic parting agent capable of withstanding a temperature of at least 1000° C.

9. The method of claim 8 , wherein the coating is boron nitride.

10. The method of claim 1 , wherein the silicon-based insulating material further comprises, by dry weight, >0% and ≤10% boron carbide, and/or >0% and ≤20% organic binder.

11. A method for adding ceramic matrix composite (CMC) plies to a previously densified CMC component, the method comprising:
positioning a plurality of CMC plies against the previously densified CMC component to form a component layup;
applying a coating to a region of outer surfaces of the previously densified CMC component of the component layup to form a coated layup;
temporarily applying, without bonding, a silicon-based insulating material against at least a portion of the previously densified outer surfaces of the coated layup outside of the coating to form an insulated layup,
wherein the silicon-based insulating material comprises, by dry weight, ≥25% and ≤95% silicon and >0% and ≤50% boron nitride;
densifying the insulated layup; and
removing the silicon-based insulating material after densifying the insulated layup.

12. The method of claim 11 , wherein each CMC ply of the plurality of CMC plies comprises fibers extending generally along a longitudinal direction L 1 defined by the CMC ply,
wherein a first CMC ply of the plurality of CMC plies is positioned against the CMC component and a remainder of the plurality of CMC plies are stacked against the first CMC ply, and
wherein an orientation of the plurality of CMC plies is varied such that the fibers of at least one ply of the plurality of CMC plies are oriented in a different direction with respect to a longitudinal direction L 2 defined by the CMC component.

13. The method of claim 12 , further comprising:
preparing a damaged area for repair prior to positioning the plurality of CMC plies against the CMC component,
wherein positioning the plurality of CMC plies against the CMC component comprises positioning the plurality of CMC plies at the damaged area.

14. The method of claim 11 , wherein densifying the insulated layup includes melt infiltrating the insulated layup.

15. The method of claim 11 , wherein, when the insulated layup is densified, a locally high silicon vapor pressure is created at the CMC component.

16. A method for adding a composite material to a previously densified composite component, the method comprising:
positioning a composite material segment against the previously densified composite component to form a component layup;
temporarily applying, without bonding, a silicon-based insulating material around at least a portion of the component layup to form an insulated layup,
wherein the silicon-based insulating material comprises, by dry weight, 25-95% silicon and >0% and ≤50% boron nitride;
densifying the insulated layup; and
removing the silicon-based insulating material after densifying the insulated layup.

17. The method of claim 11 , wherein the silicon-based insulating material comprises, by dry weight, >0% and ≤10% boron carbide, and/or >0% and ≤20% organic binder.

18. The method of claim 16 , wherein the silicon-based insulating material comprises, by dry weight, >0% and ≤10% boron carbide and/or >0% and ≤20% organic binder.

Assignees

• Gen Electric

Inventors

• Roberts Herbert Chidsey
• Taxacher Glenn Curtis
• Coons Timothy P
• Weaver Jared Hogg
• Dunn Daniel Gene
• Magnant Jerome Geoffrey

Classifications

• F05D2220/32

  in gas turbines · CPC title

• F05D2240/14

  Casings or housings protecting or supporting assemblies within · CPC title

• F05D2240/35

  Combustors or associated equipment · CPC title

• F05D2240/11

  Shroud seal segments · CPC title

• F05D2240/128

  Nozzles · CPC title