Combustion chamber

Patent metadata

Field	Value
Publication number	US-9903590-B2
Application number	US-201414559320-A
Country	US
Kind code	B2
Filing date	Dec 3, 2014
Priority date	Dec 23, 2013
Publication date	Feb 27, 2018
Grant date	Feb 27, 2018

Abstract

A double wall structured combustor having an outer wall having an inner surface and an outer surface and an inner wall comprising a plurality of tiles. Each tile has at least one interlocking member at a first wall and at least one interengaging member at a second wall. The interlocking member extending through an aperture in the outer wall, and the interengaging member at the second wall engaging with a cutaway section in the first wall of an adjacent tile. On assembly of the combustion chamber, the interlocking members and interengaging members of the tiles ensure lower profile fixings and an overall reduction in number of conventional fasteners used.

First claim

The invention claimed is:

1. A combustor having a double wall structure comprising:
an annular inner wall and an annular outer wall,
the annular outer wall having an inner surface, an outer surface, and a plurality of circumferentially spaced apertures, the annular outer wall including at least one blind aperture extending into the inner surface, and
the annular inner wall comprising a plurality of circumferentially arranged tiles, the tiles having at least one interlocking member at a first circumferential end of each tile, at least one interengaging member at a second circumferential end of each tile, and at least one protrusion member extending from a wall of each tile,
each interlocking member extending through a corresponding one of the circumferentially spaced apertures in the annular outer wall and resting on the outer surface of the annular outer wall,
the interengaging member at the second circumferential end of each tile engaging with the first circumferential end of an adjacent tile, and
each protrusion member extending into a corresponding blind aperture.

2. The combustor according to claim 1 , wherein there is an interference fit between the protrusion member and the blind aperture.

3. A combustor having a double wall structure comprising:
an annular inner wall and an annular outer wall,
the annular outer wall having an inner surface, an outer surface, and a plurality of circumferentially spaced apertures,
the annular inner wall comprising a plurality of circumferentially arranged tiles, the tiles having at least one interlocking member at a first circumferential end of each tile and at least one interengaging member at a second circumferential end of each tile,
the interengaging member at the second circumferential end of each tile engaging with the first circumferential end of an adjacent tile,

wherein the annular outer wall and the annular inner wall interact together such that:
each interlocking member extends through a corresponding one of the circumferentially spaced apertures in the annular outer wall and rests on the outer surface of the annular outer wall, and
each interengaging member extends radially inward of the outer surface of the annular outer wall.

4. The combustor according to claim 3 , further including a final tile, the final tile comprising at least one interlocking member at a first circumferential end of the final tile or at least one interengaging member at a second circumferential end of the final tile.

5. The combustor according to claim 3 , wherein the at least one interlocking member extends radially from a first wall at the first circumferential end of each tile.

6. The combustor according to claim 5 , wherein the first wall at the first circumferential end has at least one cutaway section to receive an interengaging member.

7. The combustor according to claim 3 , wherein the at least one interengaging member extends circumferentially from a second wall at the second circumferential end of each tile.

8. The combustor according to claim 3 , wherein:
two interlocking members extend radially from a first wall at the first circumferential end of each tile, the first wall at the first circumferential end of each tile has two cutaway sections, and
two interengaging members extend circumferentially from a second wall at the second circumferential end of each tile.

9. The combustor according to claim 1 , wherein the at least one protrusion member is located on a third wall of each tile.

10. The combustor according to claim 4 , wherein the final tile comprises an integral stud formed at the first circumferential end or second circumferential end, the integral stud extending radially from the first circumferential end or second circumferential end.

11. The combustor according to claim 3 , wherein the at least one interlocking member is L-shaped.

12. The combustor according to claim 3 , wherein the combustor is an annular combustor, the annular outer wall being arranged around the annular inner wall, the at least one interlocking member extending radially outwardly through the corresponding one of the circumferentially spaced apertures in the annular outer wall.

13. The combustor according to claim 3 , wherein the plurality of circumferentially arranged tiles are manufactured from an additive layer manufacturing route.

14. The combustor according to claim 13 , wherein the additive layer manufacturing route is direct laser deposition.

15. The combustor according to claim 3 , wherein the plurality of circumferentially arranged tiles are manufactured from a casting process.

16. A gas turbine engine comprising a combustor, wherein the combustor comprises a double wall structure according claim 3 .

17. A combustor having a double wall structure comprising:
an annular inner wall and an annular outer wall,
the annular outer wall having an inner surface, an outer surface, and a plurality of circumferentially spaced apertures,
the annular inner wall comprising a plurality of circumferentially arranged tiles, each tile having an outer surface, a first wall at a first circumferential end of each tile, a second wall at a second circumferential end of each tile, a third wall at a first axial edge of each tile, and a fourth wall at a second axial edge of each tile,
the first wall, the second wall, the third wall, and the fourth wall extending radially outwards from the outer surface of each tile towards the inner surface of the annular outer wall,
each tile having at least one interlocking member at the first circumferential end of each tile and at least one interengaging member at the second circumferential end of each tile,
each interlocking member extending through a corresponding one of the circumferentially spaced apertures in the annular outer wall, each interlocking member extending radially and circumferentially from the first circumferential end of each tile, the interlocking member comprising a radially extending portion and a circumferentially extending portion, and the circumferentially extending portion resting on the outer surface of the annular outer wall,

the interengaging member extending circumferentially from the second wall at the second circumferential end of each tile, each interengaging member being located radially between the inner surface of the annular outer wall and the outer surface of the adjacent tile, the first wall at the first circumferential end of the tile having at least one cutaway section, and the interengaging member at the second circumferential end of each tile engaging with the at least one cutaway section in the first wall at the first circumferential end of an adjacent tile.

18. The combustor according to claim 17 , wherein the first wall, the second wall, the third wall, and the fourth wall extend radially outwards from the outer surface of the tile and abut the inner surface of the annular outer wall.

Assignees

• Rolls Royce Plc

Inventors

• Garry Ian Murray
• Carlisle Michael Lawrence

Classifications

• F23R3/60

  Support structures; Attaching or mounting means · CPC title

• F23R3/007

  constructed mainly of ceramic components · CPC title

• F23R2900/00017

  Assembling combustion chamber liners or subparts · CPC title

• F23R3/06

  Arrangement of apertures along the flame tube · CPC title

• F23R3/002

  Wall structures (F23R3/02 and F23R3/007 take precedence) · CPC title