Shroud assembly with discourager

• US 8,303,245 B2
• Filed: 10/09/2009
• Issued: 11/06/2012
• Est. Priority Date: 10/09/2009
• Status: Active Grant

• Current Assignee: GE Infrastructure Technology, LLC (GE Vernova, Inc.)
• Original Assignee: General Electric Company
• Inventors: Foster, Gregory Thomas, Crespo, Andres Jose Garcia, Roberts, Herbert Chidsey
• Primary Examiner(s): EDGAR, RICHARD A
• Application Number:
  US12/576,386
• Publication Number:
  US 20110085899A1
• Time in Patent Office: 1,124 Days
• Field of Search: 415/134, 415/139, 415/173.1, 416/193.A
• US Class Current: 415/134
• CPC Class Codes: F01D 11/00 Preventing or minimising internal leakage of working-fluid, e.g. between stages sealings in general F16J ; sealing arrangements for transition ducts of combustor cans F01D9/023
• CPC Class Codes: F01D 25/265 Vertically split casings; Clamping arrangements therefor
• CPC Class Codes: F01D 9/04 forming ring or sector
• CPC Class Codes: F05D 2240/11 Shroud seal segments
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

A turbine shroud assembly is disclosed, the shroud assembly including an outer shroud, at least one inner shroud attached to the outer shroud, and at least one discourager enclosed within the inner shroud. The discourager prevents the hot gas or steam in the turbine from having a direct line of access to the outer shroud. In one embodiment, one inner shroud is provided for the shroud assembly, with one discourager enclosed within the inner shroud, the discourager positioned offset from the inner shroud so as to extend past the inner shroud and into an inner shroud of a neighboring shroud assembly. In another embodiment, a plurality of inner shrouds are provided, each inner shroud enclosing a discourager, the discouragers being adjacent to each other within the inner shrouds and positioned offset from the inner shrouds so as to cover a gap between the inner shrouds.

Claims

1. A shroud assembly for use in a turbine, the shroud assembly comprising:

an outer shroud having a first side configured to interface with an outer casing of the turbine, and a second side proximate to a flow of an operative fluid of the turbine;

a hollow inner shroud positioned between the second side of the outer shroud and the operative fluid flow of the turbine, wherein the hollow inner shroud has a channel therethrough; and

a solid discourager shaped to substantially correspond to a circumferential and axial shape and size of the channel in the hollow inner shroud, wherein the discourager is within the hollow inner shroud and is positioned to extend at least partially into a hollow inner shroud of a neighboring shroud assembly.

2. The shroud assembly of claim 1, wherein the hollow inner shroud is comprised of a ceramic material, a ceramic matrix composite material, a monolithic type ceramic, or a Ni superalloy.

3. The shroud assembly of claim 1, wherein the solid discourager has at least one beveled edge.

4. The shroud assembly of claim 1, wherein the hollow inner shroud has at least one beveled edge.

5. The shroud assembly of claim 1, wherein the solid discourager is comprised of a ceramic material, a ceramic matrix composite material, a monolithic type ceramic, or a Ni superalloy.

6. A shroud assembly for use in a turbine, the shroud assembly comprising:

an outer shroud having a first side configured to interface with an outer casing of the turbine, and a second side proximate to a flow of an operative fluid of the turbine;

at least two hollow inner shrouds adjacent to each other, positioned to create an expansion space therebetween, the at least two hollow inner shrouds positioned between the second side of the outer shroud and the operative fluid flow of the turbine, wherein each hollow inner shroud has a channel therethrough; and

at least two solid discouragers adjacent to each other, each solid discourager shaped to substantially correspond to a circumferential and axial shape and size of the channel in a corresponding hollow inner shroud, wherein the at least two discouragers are within the hollow inner shrouds and are positioned offset from the at least two hollow inner shrouds so as to cover the expansion space.

7. The shroud assembly of claim 6, wherein at least one of:

the at least two hollow inner shrouds and the at least two solid discouragers are comprised of a ceramic material, a ceramic matrix composite material, a monolithic type ceramic, or a Ni superalloy.

8. The shroud assembly of claim 6, wherein the at least two solid discouragers are positioned such that an end of at least one solid discourager extends past an end of the hollow inner shroud that the at least one solid discourager is within.

9. The shroud assembly of claim 8, wherein the end of the at least one solid discourager that extends past the hollow inner shroud extends into a hollow inner shroud of a neighboring shroud assembly.

10. The shroud assembly of claim 6, wherein the at least two solid discouragers each have at least one beveled edge, and wherein the at least two hollow inner shrouds each have at least one beveled edge.

11. The shroud assembly of claim 6, further comprising a gap between the at least two solid discouragers.

12. A turbine comprising:

an outer casing;

at least one rotating blade; and

a shroud assembly positioned between the outer casing of the turbine and the at least one rotating blade, the shroud assembly comprising;

an outer shroud having a first side configured to interface with the outer casing, and a second side configured to interface with the at least one rotating blade proximate to a flow of an operative fluid of the turbine;

at least one hollow inner shroud positioned between the second side of the outer shroud and the operative fluid flow of the turbine, wherein the at least one hollow inner shroud has a channel therethrough; and

at least one solid discourager shaped to substantially correspond to a circumferential and axial shape and size of the channel in the hollow inner shroud, wherein the discourager is within the at least one hollow inner shroud and is positioned offset from the at least one hollow inner shroud.

13. The turbine of claim 12, wherein the at least one hollow inner shroud is comprised of a ceramic material, a ceramic matrix composite material, a monolithic type ceramic, or a Ni superalloy.

14. The turbine of claim 12, wherein the at least one solid discourager is comprised of a ceramic material, a ceramic matrix composite material, a monolithic type ceramic, or a Ni superalloy.

15. The turbine of claim 12, wherein the at least one hollow inner shroud comprises two hollow inner shrouds adjacent to each other, positioned to create an expansion space therebetween and wherein the at least one solid discourager comprises two solid discouragers adjacent to each other positioned within the hollow inner shrouds, the solid discouragers positioned offset from the hollow inner shrouds so as to cover the expansion space.

16. The turbine of claim 15, further comprising a gap between the two solid discouragers.

17. The turbine of claim 12, wherein at least one solid discourager is positioned such that an end of the at least one solid discourager extends past an end of the at least one hollow inner shroud that the at least one solid discourager is within.

18. The turbine of claim 17, wherein the end of the at least one solid discourager that extends past the at least one hollow inner shroud extends into a hollow inner shroud of a neighboring shroud assembly.