High temperature seals and high temperature sealing systems

• US 7,771,159 B2
• Filed: 10/16/2006
• Issued: 08/10/2010
• Est. Priority Date: 10/16/2006
• Status: Active Grant

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Johnson, Curtis, Bruce, Kevin L., Cairo, Ronald Ralph
• Primary Examiner(s): Look; Edward
• Assistant Examiner(s): White; Dwayne J
• Application Number:
  US11/581,250
• Publication Number:
  US 20080089781A1
• Time in Patent Office: 1,394 Days
• Field of Search: 415/135, 415/136, 277/641, 277/650, 277/652, 277/654, 277/931, 277/943
• US Class Current: 415/135
• CPC Class Codes: F01D 11/008 by spacer elements between the blades, e.g. independent interblade platforms
• CPC Class Codes: F05D 2300/2283 of silicon
• CPC Class Codes: F05D 2300/603 Composites; e.g. fibre-reinforced
• CPC Class Codes: F16J 15/102 characterised by material
• CPC Class Codes: F16J 15/104 characterised by structure

Abstract

A high temperature seal that may include an interior region comprising a material that swells when exposed to a high temperature environment and at least one projection that is able to be inserted into a slot, and a coating that substantially prevents swelling to coated areas of the interior region. The coating may be disposed upon an exterior surface of the interior region such that a distal end of at least one projection remains at least partially uncoated and the remainder of the interior region is substantially covered by the coating. The interior region may include a ceramic matrix composite.

Claims

1. A high temperature seal comprising:

an interior region comprising a ceramic matrix composite material that swells due to oxidation when exposed to a high temperature environment of at least 500°

Celsius and at least one projection that is able to be inserted into a slot; and

an environmental barrier coating that substantially prevents the oxidation swelling to coated areas of the interior region;

wherein the coating is disposed upon an exterior surface of the interior region such that a distal end of at least one projection is partially uncoated and the remainder of the interior region is substantially covered by the coating.

2. The high temperature seal of claim 1, wherein the interior region comprises a silicon carbide ceramic matrix composite.

3. The high temperature seal of claim 1, wherein the ceramic matrix composite comprises a continuous fiber ceramic matrix composite.

4. The high temperature seal of claim 1, wherein the exposure of the uncoated region of the distal end of the projection to the high temperature environment causes the oxidation swelling of the projection.

5. The high temperature seal of claim 1, wherein the high temperature environment comprises a flowpath of a gas turbine engine.

6. The high temperature seal of claim 1, wherein the coating comprises a multi-layered environmental barrier coating.

7. The high temperature seal of claim 1, wherein the interior region comprises an approximate rectangular cross-section having opposing long sides and opposing short sides, each of the short sides comprising the distal end of the projection.

8. The high temperature seal of claim 7, wherein the opposing long sides are at least twice as long as the short sides.

9. The high temperature seal of claim 7, wherein each of the short sides is uncoated.

10. The high temperature seal of claim 7, wherein at least one of the long sides angles inward as the long side nears the short side.

11. The high temperature seal of claim 10, wherein the angle between the long side before it angles inward and the long side after it angles inward is between about 150 to about 170 degrees.

12. The high temperature seal of claim 7, wherein at least one of the short sides is partially coated such that the uncoated region comprises a window disposed in the approximate center of the short side.

13. The high temperature seal of claim 12, wherein exposure of the uncoated region of the window to the high temperature environment causes the oxidation swelling of the projection;

and

wherein the window comprises a predetermined size based upon the amount of oxidation swelling desired in the projection.

14. The high temperature seal of claim 12, wherein the partially coated short side further comprises rounded edges.

15. The high temperature seal of claim 7, further comprising a build-up of coating along the middle section of one of the long sides.

16. A high temperature sealing system comprising:

a first structure with a first seal slot and a second structure with a second seal slot, the first seal slot and the second seal slot opposing each other across a sealing area;

a high temperature seal, the high temperature seal comprising an interior region with a first projection that fits within the first seal slot and a second projection that fits within the second seal slot such that, upon assembly, the high temperature seal bridges the sealing area, the interior region being comprised of a ceramic matrix composite that swells due to oxidation when exposed to a high temperature environment; and

an environmental barrier coating that substantially prevents the oxidation swelling to coated areas of the interior region;

wherein the environmental barrier coating is disposed upon the exterior surface of the interior region such that a distal end of the first projection and a distal end of the second projection are each partially uncoated and the remainder of the interior region is substantially covered by the environmental barrier coating.

17. A high temperature sealing system for a shroud damper system in a turbine, comprising:

a first damper block with a first seal slot and a second damper block with a second seal slot, the first seal slot and the second seal slot opposing each other across a sealing area;

a high temperature seal, the high temperature seal comprising an interior region with a first projection that fits within the first seal slot and a second projection that fits within the second seal slot such that, upon assembly, the high temperature seal bridges the sealing area, the interior region being comprised of a ceramic matrix composite that swells due to oxidation when exposed to a flow path of the gas turbine; and

an environmental barrier coating that substantially prevents the oxidation swelling to coated areas of the interior region;

wherein the environmental barrier coating is disposed upon the exterior surface of the interior region such that a distal end of the first projection and a distal end of the second projection are each partially uncoated and the remainder of the interior region is substantially covered by the environmental barrier coating.

18. The high temperature sealing system for a shroud damper system in a turbine of claim 17, wherein the first seal slot is enclosed on one side by a first shroud and the second seal slot is enclosed on one side by a second shroud.

19. The high temperature sealing system for a shroud damper system in a turbine of claim 17, wherein each of the distal ends is partially coated such that the uncoated region comprises a window in the approximate center of the short side.

20. The high temperature sealing system for a shroud damper system in a turbine of claim 19, wherein the exposure of the uncoated region of the window to the flow path of the gas turbine causes the oxidation swelling of the projection;

and

wherein the window comprises a predetermined size based upon the amount of oxidation swelling desired in each of the projections.