COMBUSTION CHAMBER

• US 20130031904A1
• Filed: 07/16/2012
• Published: 02/07/2013
• Est. Priority Date: 08/02/2011
• Status: Active Grant

• Current Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Original Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Inventors: GARRY, Ian M.
• Granted Patent: US 8,707,706 B2
• Time in Patent Office: Days
• US Class Current: 60/722
• CPC Class Codes: B33Y 80/00 Products made by additive manufacturing
• CPC Class Codes: F23R 3/002 Wall structures F23R3/02 and F23R3/007 take precedence
• CPC Class Codes: F23R 3/06 Arrangement of apertures along the flame tube
• CPC Class Codes: F23R 3/60 Support structures; Attaching or mounting means

Abstract

A combustion chamber includes at least one annular wall. The annular wall includes a plurality of segments and each segment has a first portion, a second portion and a third portion. The first portion of each segment extends circumferentially, the third portion of each segment extends circumferentially and the second portion of each segment extends radially to connect the first portion and third portion of the segment. The segments are arranged such that the first portion of each segment overlaps the third portion of an adjacent segment and the first portion of each segment is bolted to the third portion of the adjacent segment. The segments are cast and define a double wall combustion chamber and enable easier construction of the combustion chamber and replacement of damaged segments.

Claims

1. A combustion chamber comprising at least one annular wall, the annular wall comprising a plurality of segments, each segment having a first portion, a second portion and a third portion, the first portion of each segment extending circumferentially, the third portion of each segment extending circumferentially and the second portion of each segment extending radially to connect the first portion and third portion of the segment, the segments being arranged such that the first portion of each segment overlaps the third portion of an adjacent segment and the first portion of each segment is joined to the third portion of the adjacent segment.

2. A combustion chamber as claimed in claim 1 wherein the second portion of each segment extends circumferentially and radially.

3. A combustion chamber as claimed in claim 1 wherein the first portion of each segment is spaced radially from the third portion of the adjacent segment to form at least one chamber and the chamber is arranged to be supplied with a coolant.

4. A combustion chamber as claimed in claim 1 wherein the segment is arranged such that the first portion of each segment is arranged radially outwardly of the third portion of the adjacent segment.

5. A combustion chamber as claimed in claim 4 wherein the third portion of each segment has at least one radially outwardly extending stud arranged to locate in a corresponding aperture in the first portion of the adjacent segment to join the segments together.

6. A combustion chamber as claimed in claim 5 wherein the third portion of each segment has a plurality of radially outwardly extending studs arranged to locate in a corresponding aperture of a plurality of apertures in the first portion of the adjacent segment to join the segments together.

7. A combustion chamber as claimed in claim 1 wherein the first portion of each segment has at least one dilution aperture aligned with a corresponding dilution aperture in the third portion of the adjacent segment.

8. A combustion chamber as claimed in claim 3 wherein the first portion of each segment has a plurality of cooling holes arranged to supply coolant to the at least one chamber defined between the first portion and the third portion of the adjacent segment.

9. A combustion chamber as claimed in claim 8 wherein the plurality of cooling holes are arranged to impinge the coolant upon a radially outer surface of the third portion of the adjacent segment.

10. A combustion chamber as claimed in claim 3 wherein the third portion of each segment has a plurality of effusion cooling apertures to provide a film of coolant on a radially inner surface of the third portion of each segment.

11. A combustion chamber as claimed in claim 3 wherein the third portion of each segment has a thermal barrier coating on a radially inner surface.

12. A combustion chamber as claimed in claim 1 wherein the segment is arranged such that the first portion of each segment is arranged radially inwardly of the third portion of the adjacent segment.

13. A combustion chamber as claimed in claim 12 wherein the third portion of each segment has at least one radially inwardly extending stud arranged to locate in a corresponding aperture in the first portion of the adjacent segment to join the segments together.

14. A combustion chamber as claimed in claim 13 wherein the third portion of each segment has a plurality of radially inwardly extending studs arranged to locate in a corresponding aperture of a plurality of apertures in the first portion of the adjacent segment to join the segments together.

15. A combustion chamber as claimed in claim 12 wherein the first portion of each segment has at least one dilution aperture aligned with a corresponding dilution aperture in the third portion of the adjacent segment.

16. A combustion chamber as claimed in claim 12 wherein the first portion of each segment has a plurality of cooling holes arranged to supply coolant to the at least one chamber defined between the first portion and the third portion of the adjacent segment.

17. A combustion chamber as claimed in claim 16 wherein the plurality of cooling holes are arranged to impinge the coolant upon a radially inner surface of the third portion of the adjacent segment.

18. A combustion chamber as claimed in claim 12 wherein the third portion of each segment has a plurality of effusion cooling apertures to provide a film of coolant on a radially outer surface of the third portion of each segment.

19. A combustion chamber as claimed in claim 12 wherein the third portion of each segment has a thermal barrier coating on a radially outer surface.

20. A combustion chamber as claimed in claim 1 wherein the first portion, the second portion and the third portion of each segment is formed integrally.

21. A combustion chamber as claimed in claim 20 wherein at least one of the segments comprises a casting.

22. A combustion chamber as claimed in claim 1 wherein the combustion chamber is a tubular combustion chamber and the at least one wall is a tubular wall.

23. A combustion chamber as claimed in claim 1 wherein the combustion chamber is an annular combustion chamber and the at least one wall is selected from the group consisting of a radially outer annular wall and a radially inner annular wall.

24. A combustion chamber comprising at least one annular wall, the annular wall comprising a plurality of segments, each segment having a first portion, a second portion and a third portion, the first portion of each segment extending circumferentially, the third portion of each segment extending circumferentially and the second portion of each segment extending radially to connect the first portion and third portion of the segment, the segments being arranged such that the first portion of each segment overlaps the third portion of an adjacent segment and the first portion of each segment is joined to the third portion of the adjacent segment, the first portion of each segment being arranged to extend circumferentially through substantially the same angle as the third portion of the adjacent segment.

25. A combustion chamber comprising at least one annular wall, the annular wall comprising a plurality of segments, each segment having a first portion, a second portion and a third portion, the first portion of each segment extending circumferentially, the third portion of each segment extending circumferentially and the second portion of each segment extending radially to connect the first portion and third portion of the segment, the segments being arranged such that the first portion of each segment overlaps the third portion of an adjacent segment and the first portion of each segment is joined to the third portion of the adjacent segment, the first portion of each segment being arranged to extend axially substantially the same length as the third portion of the adjacent segment.