Apparatus and method to reduce wear and friction between CMC-to-metal attachment and interface

Patent metadata

Field	Value
Publication number	US-9500083-B2
Application number	US-201213685230-A
Country	US
Kind code	B2
Filing date	Nov 26, 2012
Priority date	Nov 26, 2012
Publication date	Nov 22, 2016
Grant date	Nov 22, 2016

Abstract

An apparatus to reduce wear and friction between CMC-to-metal attachment and interface, including a metal layer configured for insertion between a surface interface between a CMC component and a metal component. The surface interface of the metal layer is compliant relative to asperities of the surface interface of the CMC component. A coefficient of friction between the surface interface of the CMC component and the metal component is about 1.0 or less at an operating temperature between about 300° C. to about 325° C. and a limiting temperature of the metal component.

First claim

What is claimed is:

1. An apparatus to reduce wear and friction between CMC-to-metal attachment and interface, comprising:
a homogenous, one-piece single metal layer capable of being devoid of openings configured for insertion between multiple interfacing surfaces between a CMC component and a metal component, the metal layer formed separately from the CMC component and the metal component;
wherein only the metal layer is inserted between the CMC component and the metal component;
wherein the interfacing surfaces of the metal layer are compliant relative to asperities of the interfacing surfaces of the CMC component, a coefficient of friction between the interfacing surfaces of the CMC component and the metal component being above 0 and less than or equal to 0.4 at an operating temperature between about 300° C. to about 325° C. and a limiting temperature of the metal component of up to 760° C.;
wherein the multiple interfacing surfaces of the CMC component define a fir tree arrangement.

2. The apparatus of claim 1 , wherein at least one of fibers and matrix of the CMC is silicon carbide.

3. The apparatus of claim 1 , wherein the metal layer is between about 0.08 mm and about 0.25 mm.

4. The apparatus of claim 1 , wherein the metal layer is between about 0.10 mm and about 0.20 mm.

5. The apparatus of claim 1 , wherein the metal layer is between about 0.13 mm and about 0.15 mm.

6. The apparatus of claim 1 , wherein the metal layer is about 0.15 mm.

7. The apparatus of claim 1 , wherein the metal layer is selected from the group consisting of ferrous alloys, Nickel-based alloys, and Cobalt-based alloys.

8. An apparatus for use in a heated environment comprising:
a CMC component;
a metal component having multiple interfacing surfaces with the CMC component, the multiple interfacing surfaces of the CMC component defining a fir tree arrangement; and
a homogenous, one-piece single metal layer capable of being devoid of openings, the metal layer having opposed interconnected layer portions configured for insertion between corresponding portions of the multiple interfacing surfaces between the CMC component and the metal component, the metal layer formed separately from the CMC component and the metal component;
wherein only the metal layer is inserted between the CMC component and the metal component;
wherein the opposed interconnected layer portions of the multiple interfacing surfaces of the metal layer are compliant relative to asperities of corresponding layer portions of the multiple interfacing surfaces of the CMC component, a coefficient of friction between the corresponding layer portions of the multiple interfacing surfaces of the CMC component and the metal component after insertion of the corresponding layer portions of the metal layer being above 0 and less than or equal to 0.4 at an operating temperature between about 300° C. to about 325° C. and a limiting temperature of up to 760° C.

9. The apparatus of claim 8 , wherein the metal layer is between about 0.08 mm and about 0.25 mm.

10. The apparatus of claim 8 , wherein the metal layer is between about 0.10 mm and about 0.20 mm.

11. The apparatus of claim 8 , wherein the metal layer is between about 0.13 mm and about 0.15 mm.

12. The apparatus of claim 8 , wherein the metal layer is selected from the group consisting of ferrous alloys, Nickel-based alloys, and Cobalt-based alloys.

13. The apparatus of claim 8 , wherein the component is a turbine engine component.

14. The apparatus of claim 8 , wherein the component is a turbine blade.

15. A method to reduce wear and friction between CMC-to-metal attachment and interface, comprising:
configuring a homogenous, one-piece single metal layer capable of being devoid of openings, the metal layer having opposed interconnected layer portions for insertion between corresponding portions of multiple interfacing surfaces between a CMC component and a metal component, the metal layer formed separately from the CMC component and the metal component, the multiple interfacing surfaces of the CMC component defining a fir tree arrangement, wherein only the metal layer is inserted between the CMC component and the metal component, the corresponding portions of the multiple interfacing surfaces of the corresponding portions of the metal layer being compliant relative to asperities of the corresponding portions of the multiple interfacing surfaces of the CMC component, a coefficient of friction between the corresponding portions of the multiple interfacing surfaces of the CMC component and the metal component being above 0 and less than or equal to 0.4 at an operating temperature between about 300° C. to about 325° C. and a limiting temperature of the metal component; and
inserting the layer portions of the metal bar between the corresponding layer portions of the multiple interfacing surfaces between the CMC component and the metal component of up to 760° C.; and
operating the CMC component, the metal layer and the metal component at the operating temperature.

Assignees

• Gen Electric
• Us Dept Energy

Inventors

• Cairo Ronald Ralph
• Parolini Jason Robert
• Delvaux John Mcconnell

Classifications

• C04B2237/84

  Joining of a first substrate with a second substrate at least partially inside the first substrate, where the bonding area is at the inside of the first substrate, e.g. one tube inside another tube · CPC title

• C04B2237/405

  Iron metal group, e.g. Co or Ni · CPC title

• C04B35/117

  Composites · CPC title

• C04B2235/5228

  Silica and alumina, including aluminosilicates, e.g. mullite · CPC title

• C04B2237/708

  of one or more of the interlayers · CPC title