Combustion section with a casing shielding

Patent metadata

Field	Value
Publication number	US-12215864-B2
Application number	US-202118270855-A
Country	US
Kind code	B2
Filing date	Oct 12, 2021
Priority date	Jan 25, 2021
Publication date	Feb 4, 2025
Grant date	Feb 4, 2025

Abstract

A combustion section of a gas turbine includes an annular combustion chamber, a burner arrangement upstream of the combustion chamber, an annular compressor diffusor, and an annular combustion casing. The combustion casing has an outer section wall, an upstream section wall, and an inner section wall. The inner section wall extends along the rotor axis and is arranged between the burner arrangement and the compressor diffusor. A shielding is attached to the inner section wall at the side facing the rotor axis with a free space in-between at least. An outer diffusor wall of the compressor diffusor extends in axial direction up to the upstream half of the shielding.

First claim

The invention claimed is:

1. An assembly for a gas turbine, the assembly comprising a rotor axis, a compressor section, and a combustion section, the combustion section comprising:
an upstream side and a downstream side;
an annular combustion, chamber;
a burner arrangement upstream of the annular combustion, chamber;
an annular compressor diffusor downstream of the compressor section and having an annular inner diffusor wall and an annular outer diffusor wall, the annular outer diffuser wall having a wall end at a downstream side of the annular outer diffusor wall;
an annular combustion casing having an outer section wall extending along the rotor axis and arranged radially outward relative to the annular combustion chamber, an upstream section wall extending along a radial direction and arranged upstream relative to the annular combustion chamber, and an inner section wall extending along the rotor axis and arranged between the burner arrangement and the compressor diffusor, wherein the outer diffusor wall the inner section wall in an axial direction; and
a shielding attached to the inner section wall on a radially inner side of the inner section wall facing the rotor axis, wherein a free space is defined between the shielding and the radially inner side of the inner section wall along at least half of an axial length of the inner section wall, wherein the wall end of the annular outer diffuser wall is arranged axially between an upstream end of the shielding and an axial midpoint of the shielding.

2. The assembly according to claim 1 , wherein the upstream end of the shielding is axially spaced apart from the upstream section wall.

3. The assembly according to claim 1 , wherein the inner section wall comprises a recess spaced apart from each of the upstream section wall and a downstream end of the inner section wall, wherein the recess is covered by the shielding.

4. The assembly according to claim 3 , wherein the radially inner side of the inner section wall upstream and downstream of the shielding forms a continuous surface with a radially inner side of the shielding.

5. The assembly according to claim 1 , wherein a free distance from the shielding to the radially inner side of the inner section wall is at least 0.1 times, and at most 0.3 times, a thickness from a radially outer side of the inner section wall to a radially inner side of the shielding.

6. The assembly according to claim 5 , wherein the free distance is at least 0.15 and/or at most 0.2 times the thickness from the radially outer side of the inner section wall to the radially inner side of the shielding.

7. The assembly according to claim 1 , wherein a free distance from the shielding to the radially inner side of the inner section wall is at least 0.5 times, and at most 1.5 times, a distance from the shielding to the outer diffuser wall.

8. The assembly according to claim 7 , wherein the free distance is at least 0.7 times and/or at most 0.9 times the distance from the shielding to the outer diffuser wall.

9. The assembly according to claim 1 , wherein an inner cover is attached on a radially outer side of the inner section wall, an inner gap defined between the inner cover and the radially outer side of the inner section wall.

10. The assembly according to claim 9 , wherein the inner cover comprises a downstream end having a bend.

11. The assembly according to claim 10 , wherein the bend is in contact with the inner section wall.

12. The assembly according to claim 9 , wherein a width of the inner gap is at least 0.6 times, and at most 1.5 times, a free distance from the shielding to the radially inner side of the inner section wall.

13. The assembly according to claim 12 , wherein the width of the inner gap is at least 0.8 times and/or at most 1.2 times the free distance.

14. The assembly according to claim 1 , wherein an upstream cover is attached on a downstream side of the upstream section wall, an upstream gap defined between the upstream cover and the downstream side of the upstream section wall.

15. The assembly according to claim 14 , wherein the upstream cover comprises a radially outer end having a bend.

16. The assembly according to claim 15 , wherein the bend is in contact with the upstream section wall.

17. The assembly according to claim 14 , wherein a width of the upstream gap is at least 0.6 times, and at most 1.5 times, a free distance from the shielding to the radially inner side of the inner section wall.

18. The assembly according to claim 17 , wherein the width of the upstream gap is at least 0.8 times and/or at most 1.2 times the free distance.

19. The assembly according to claim 14 , wherein an inner cover is attached on a radially outer side of the inner section wall, an inner gap defined between the inner cover and the radially outer side of the inner section wall, and wherein the inner cover is connected to the upstream cover, the inner gap and the upstream gap being connected to define a continuous gap.

Assignees

• Siemens Energy Global Gmbh & Co Kg

Inventors

• Frejd Mikael
• Nilsson Johan
• Silfver Daniel

Classifications

• F05D2260/231

  Preventing heat transfer · CPC title

• F01D25/145 Primary

  Thermally insulated casings · CPC title

• F23R3/50

  Combustion chambers comprising an annular flame tube within an annular casing (toroidal combustion chambers F23R3/52) · CPC title

• F23R3/60

  Support structures; Attaching or mounting means · CPC title

• F23R3/46

  Combustion chambers comprising an annular arrangement of {several essentially tubular} flame tubes within a common annular casing or within individual casings · CPC title