Segmented combustion chamber head

Patent metadata

Field	Value
Publication number	US-9328926-B2
Application number	US-201213426070-A
Country	US
Kind code	B2
Filing date	Mar 21, 2012
Priority date	Mar 22, 2011
Publication date	May 3, 2016
Grant date	May 3, 2016

Abstract

A combustion chamber head for a gas turbine, with the gas turbine having a substantially annular outer combustion chamber wall, at least one substantially annular inner combustion chamber wall, and several burners 106 distributed around a circumference of the gas turbine. Several segment-like head segments are arranged over the circumference in equal number to the number of burners and extend in the radial direction between the inner combustion chamber wall and the outer combustion chamber wall and in the circumferential direction between radial planes formed by the burner axes.

First claim

What is claimed is:

1. A combustion chamber head for a gas turbine:
wherein the gas turbine includes an axis; a substantially annular outer combustion chamber wall; at least one substantially annular inner combustion chamber wall: and a plurality of burners distributed around a circumference of the gas turbine;
the combustion chamber head comprising a plurality of head segments arranged around the circumference in equal number to a number of the burners and extending in a radial direction between the inner combustion chamber wall and the outer combustion chamber wall and also extending in a circumferential direction between two adjacent ones of the burners;
each head segment having a radially outer edge, a radially inner edge and opposite first and second outer side edges each extending between the radially inner edge and the radially outer edge, with the first outer side edge positioned adjacent a first one of the two adjacent ones of the burners and the second outer side edges positioned adjacent a second one of the two adjacent ones of the burners;
the first outer side edge including a first portion extending between the inner combustion chamber wall and the first one of the two adjacent ones of the burners, a second portion notched toward a center of the head segment to fit around a portion of an outer periphery of the first one of the two adjacent ones of the burners and a third portion extending between the first one of the two adjacent ones of the burners and the outer combustion chamber wall;
the second outer side edge including a fourth portion extending between the inner combustion chamber wall and the second one of the two adjacent ones of the burners, a fifth portion notched toward a center of the head segment to fit around a portion of an outer periphery of the second one of the two adjacent ones of the burners and a sixth the outer combustion chamber wall.

2. The combustion chamber head of claim 1 , and further comprising at least one sealing element positioned between the burners and the head segments.

3. The combustion chamber head of claim 2 , wherein the sealing element is substantially annular.

4. The combustion chamber head of claim 3 , wherein the sealing element is at least partly positioned in at least one of grooves of the burner or of the head element.

5. The combustion chamber head of claim 4 , wherein the sealing element includes at least one fin and a deformable element that can be interactively engaged with the fin.

6. The combustion chamber head of claim 4 , wherein the sealing element includes at least one labyrinth seal.

7. The combustion chamber head of claim 4 , wherein a plurality of the head segments each include at least one bushing for interaction with at least one holding element.

8. The combustion chamber head of claim 4 , wherein the head segments in an assembled state form at least one dampening volume.

9. The combustion chamber head of claim 8 , wherein the head segments in the assembled state form a combustion chamber head with a baseplate and a heat-shield.

10. The combustion chamber head of claim 9 , wherein the head segments in the assembled state are, tightly or with defined openings, connected to the outer combustion chamber wall and to the inner combustion chamber wall.

11. The combustion chamber head of claim 2 , wherein the sealing element is at least partly positioned in at least one of grooves of the burner or of the head element.

12. The combustion chamber head of claim 2 , wherein the sealing element includes at least one fin and a deformable element that can be interactively engaged with the fin.

13. The combustion chamber head of claim 2 , wherein the sealing element includes at least one labyrinth seal.

14. The combustion chamber head of claim 1 , wherein a plurality of the head segments each include at least one bushing for interaction with at least one holding element.

15. The combustion chamber head of claim 1 , wherein the head segments in an assembled state form at least one dampening volume.

16. The combustion chamber head of claim 1 , wherein the head segments in the assembled state form a combustion chamber head with a baseplate and a heat-shield.

17. The combustion chamber head of claim 1 , wherein the head segments in the assembled state are, tightly or with defined openings, connected to the outer combustion chamber wall and to the inner combustion chamber wall.

Assignees

• Penz Stefan
• Gerendas Miklos
• Sadig Sermed
• Rolls Royce Deutschland

Inventors

• Penz Stefan
• Gerendas Miklos
• Sadig Sermed

Classifications

• F23R3/283

  Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances · CPC title

• F23R3/002

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

• F23R3/10

  for primary air (F23R3/06, F23R3/045 take precedence) · CPC title

• F23R2900/00012

  Details of sealing devices · CPC title

• F23R2900/00014

  Reducing thermo-acoustic vibrations by passive means, e.g. by Helmholtz resonators · CPC title