Tile and exo-skeleton tile structure

• US 7,942,004 B2
• Filed: 11/30/2005
• Issued: 05/17/2011
• Est. Priority Date: 11/30/2004
• Status: Active Grant

• Current Assignee: Ansaldo Energia Switzerland AG (Ansaldo Energia SPA)
• Original Assignee: Alstom Technology Ltd. (Alstom SA)
• Inventors: Hodder, David
• Primary Examiner(s): Lillis; Eileen
• Assistant Examiner(s): FERENCE, JAMES M
• Application Number:
  US11/290,998
• Publication Number:
  US 20060179770A1
• Time in Patent Office: 1,994 Days
• Field of Search: 525/821, 525/822, 525/09, 60/393.2, 607/52, 607/53, 607/54
• US Class Current: 60/752
• CPC Class Codes: F23M 2900/05004 Special materials for walls or lining
• CPC Class Codes: F23M 5/02 characterised by the shape of the bricks or blocks used
• CPC Class Codes: F23R 2900/00005 Preventing fatigue failures or reducing mechanical stress in gas turbine components
• CPC Class Codes: F23R 2900/03044 Impingement cooled combustion chamber walls or subassemblies
• CPC Class Codes: F23R 2900/03045 Convection cooled combustion chamber walls provided with turbolators or means for creating turbulences to increase cooling
• CPC Class Codes: F23R 3/002 Wall structures F23R3/02 and F23R3/007 take precedence
• CPC Class Codes: F23R 3/50 Combustion chambers comprising an annular flame tube within an annular casing toroidal combustion chambers F23R3/52

Abstract

It is known to assist cooling of a combustion chamber in a gas turbine by fixing an exo-skeleton tile structure to an inner annular combustion liner shell. To improve structural integrity of the exo-skeleton tile structure, each tile is formed with at least one rib extending circumferentially across the outer surface of the tile. An end of each rib projects beyond one edge of the tile, like tiles being linked at overlapping edges by the inter-engagement of a projecting rib of one tile with the rib of an adjacent tile. The inter-engaging ends of the ribs are relatively slideable circumferentially to allow thermal expansion and contraction of the exo-skeleton structure, but sockets are provided where the ribs engage so as to resist relative bending of the adjacent tiles about their linked edges and impart rigidity to the structure.

Claims

1. A combustion liner tile for securement to an underlying generally annular combustion liner shell, the tile comprising:

a generally part-annular tile body having an outer surface facing away from the liner shell and first and second circumferentially opposed edges, the first edge having a first radius;

an edge strip at the second edge of the tile body, the edge strip having a second radius different from the first radius, the edge strip of the tile being operative for overlapping a first edge of an adjacent tile to form a generally continuous annular surface between adjacent tiles during circumferential thermal expansion and contraction in use;

at least one external main rib fastened to, and extending circumferentially across and substantially normally away from, the outer surface of the tile body, the at least one external main rib having a projecting end region that projects beyond one of the edges of the tile body, and a socket end region that is circumferentially spaced away from the other of the edges of the tile body, the socket end region of the at least one external main rib of the tile being operative for receiving a projecting end region of an external main rib of the adjacent tile in circumferential sliding engagement to resist relative circumferential bending of the adjacent tiles about their overlapping edges; and

wherein the socket end region includes an external short rib fastened to the outer surface of the tile body, the short rib having a length shorter than the at least one main external rib and extending parallel thereto, and a top cover bridging the short rib and the at least one main external rib.

2. The tile according to claim 1, and a multiplicity of apertures for impingement flow of gas through the tile body and into a gap between the tile and the liner shell in use.

3. The tile according to claim 1, in which the socket end region extends circumferentially over between ⅕

and ½

of a width of the tile body.

4. The tile according to claim 1, in which the socket end region extends circumferentially over between ¼

and ⅓

of a width of the tile body.

5. The tile according to claim 1, in which the at least one main external rib is of rectangular section and has a longer side that extends normally from the outer surface of the tile body.

6. The tile according to claim 1, comprising at least two external main ribs axially spaced apart and extending in mutual parallelism.

7. The tile according to claim 1, and at least one axially-extending stiffening rib fastened to the outer surface of the tile body and axially crossing the at least one external main rib.

8. The tile according to claim 6, and at least one axially-extending stiffening rib fastened to the outer surface of the tile body and axially crossing the at least two external main ribs.

9. The tile according to claim 1, and apertures through the tile body for receiving studs projecting radially from the liner shell.

10. The tile according to claim 1, in which the tile body is formed of high strength weldable metal alloy capable of withstanding 500°

C.

11. The tile according to claim 10, in which the alloy is an indium cobalt alloy.

12. The tile according to claim 1, in which the at least one external main rib is brazed or tungsten inert gas (TIG) type welded to the tile body to transmit shear loading in use.

13. The tile according to claim 1, in which the tile body has a curvature which varies smoothly along a major axis of the liner shell.

14. The tile according to claim 1, and means for temporarily fixing together the socket end region of the at least one external main rib of the tile and the projecting end region of the adjacent tile to resist circumferential movement during assembly.

15. The tile according to claim 14, in which the fixing means comprise pins received in holes axially formed through the socket end region and the projecting end region.

16. The tile according to claim 1, in which the tile body subtends circumferentially an angle of from 5 degrees to 15 degrees.

17. The tile according to claim 16, in which the tile body subtends circumferentially an angle of from 10 degrees to 15 degrees.

18. A generally annular exo-skeleton tile structure for securement to an underlying annular combustion liner shell to facilitate cooling of the liner shell by axial gas flow along a gap therebetween, comprising:

a plurality of circumferentially adjacent part-annular tiles linked together edgewise, each tile including a generally part-annular tile body having an outer surface facing away from the liner shell and first and second circumferentially opposed edges, the first edge of a respective tile having a first radius, an edge strip at the second edge of the tile body of the respective tile and having a second radius different from the first radius, the edge strip of each tile overlapping the first edge of an adjacent tile to form a generally continuous annular surface between the adjacent tiles during circumferential thermal expansion and contraction in use; and

at least one external main rib fastened to, and extending circumferentially across and substantially normally away from, the outer surface of each tile body, the at least one external main rib having a projecting end region that projects beyond one of the edges of the tile body, and a socket end region that is circumferentially spaced away from the other of the edges of the tile body, the socket end region of the at least one external main rib of each tile receiving the projecting end region of the external main rib of the adjacent tile in circumferential sliding engagement to resist relative circumferential bending of the adjacent tiles about their overlapping edges.

19. The exo-skeleton tile structure according to claim 18, in which each tile body has a radius which varies smoothly along a major axis of the tile structure, and in which the exo-skeleton tile structure has a radius which varies smoothly along the major axis.