Transition duct for a gas turbine

Patent metadata

Field	Value
Publication number	US-9249678-B2
Application number	US-201213534744-A
Country	US
Kind code	B2
Filing date	Jun 27, 2012
Priority date	Jun 27, 2012
Publication date	Feb 2, 2016
Grant date	Feb 2, 2016

Abstract

A transition duct for a combustor of a gas turbine generally includes a transition duct having a frame at an aft end of the transition duct. The frame generally includes a downstream end, a radially outer portion, a radially inner portion opposed to the radially outer portion, a first side portion between the radially outer and inner portions, and a second side portion opposed to the first side portion. A slot in the first side portion of the frame may have a downstream surface adjacent to the downstream end of the frame. A heat shield having an inner surface, an outer surface and a plurality of spacers may extend generally outward from the heat shield inner surface such that the inner surface is adjacent to the slot downstream surface and the frame downstream end.

First claim

What is claimed is:

1. A transition duct comprising;
a. a frame at an aft end of the transition duct, the frame having a downstream end, a radially outer portion, a radially inner portion opposed to the radially outer portion, a first side portion between the radially outer and inner portions, and a second side portion opposed to the first side portion between the radially outer and inner portions;
b. a slot in the first side portion of the frame, the slot having a downstream surface adjacent to the downstream end of the frame;
c. a heat shield having an inner surface, an outer surface and a plurality of spacers that extend outward from the inner surface, wherein the inner surface is adjacent to the slot downstream surface and the frame downstream end and wherein the heat shield is configured to exert a compressive force against the slot downstream surface and the frame downstream end; and
d. a first cooling passage defined between the heat shield inner surface, the slot downstream surface, the frame side portion and the frame downstream end.

2. The transition duct as in claim 1 , wherein at least a portion of the plurality of spacers extend from the heat shield inner surface towards the frame downstream end.

3. The transition duct as in claim 1 , wherein at least a portion of the plurality of spacers extend from the heat shield inner surface towards the slot downstream surface.

4. The transition duct as in claim 1 , wherein at least a portion of the heat shield inner surface is adjacent to a portion of a frame side surface.

5. The transition duct as in claim 4 , wherein at least a portion of the plurality of spacers extend from the heat shield inner surface towards the frame side surface.

6. The transition duct as in claim 1 , wherein the heat shield further comprises one or more spacers that extend outward from the heat shield outer surface.

7. The transition duct as in claim 1 , wherein at least a portion of the heat shield is coated in at least one of a heat resistant or a wear resistant material.

8. A combustor comprising:
a. a transition duct that extends at least partially through the combustor, the transition duct having an aft end and a frame that surrounds the aft end, the frame having a downstream end, a radially outer portion, a radially inner portion opposed to the radially outer portion, a first side portion between the radially outer and inner portions, and a second side portion opposed to the first side portion between the radially outer and inner portions;
b. a slot in the first side portion of the frame, the slot having a downstream surface adjacent to the downstream end of the frame;
c. a radial seal at least partially disposed within the slot, the radial seal having an upstream surface and a downstream surface, the radial seal at least partially disposed within the slot upstream from a heat shield, wherein the radial seal downstream surface is generally adjacent to a heat shield outer surface;
d. the heat shield disposed downstream from the radial seal, the heat shield having an inner surface, the heat shield outer surface and a plurality of spacers that extend outward from the inner surface, wherein the inner surface is adjacent to the slot downstream surface and the frame downstream end, wherein the heat shield further comprises at least one spacer that extends from the heat shield outer surface towards the radial seal downstream surface;
e. a first cooling passage defined between the heat shield inner surface, the slot downstream surface, the frame side portion and the frame downstream end; and
f. a second cooling flow passage at least partially defined between the radial seal downstream surface and the outer surface of the heat shield.

9. The combustor as in claim 8 , wherein a portion of the outer surface of the heat shield is adjacent to the radial seal.

10. The combustor as in claim 8 , wherein at least a portion of the plurality of spacers extend from the heat shield inner surface towards the downstream end of the frame.

11. The combustor as in claim 8 , wherein at least a portion of the plurality of spacers extend from the heat shield inner surface towards the slot downstream surface.

12. The combustor as in claim 8 , wherein at least a portion of the heat shield is coated in at least one of a heat resistant or a wear resistant material.

13. A combustor comprising:
a. a transition duct that extends at least partially through the combustor, the transition duct having an aft end and a frame that surrounds the aft end, the frame having a downstream end, a radially outer portion, a radially inner portion opposed to the radially outer portion, a first side portion between the radially outer and inner portions, and a second side portion opposed to the first side portion between the radially outer and inner portions;
b. a slot in the first side portion of the frame, the slot having a downstream surface adjacent to the downstream end of the frame;
c. a heat shield having an inner surface, an outer surface and a plurality of spacers that extend outward from the inner surface, wherein the inner surface is adjacent to the slot downstream surface and the frame downstream end;
d. a first cooling passage defined between the heat shield inner surface, the slot downstream surface, the frame side portion and the frame downstream end; and
e. wherein the heat shield is configured to exert a compressive force against the slot downstream surface and the frame downstream end.

14. The combustor as in claim 13 , wherein at least a portion of the plurality of spacers extend between the heat shield inner surface and at least one of the downstream end of the frame, the slot downstream surface or the side portion of the frame.

15. The combustor as in claim 13 , further comprising a radial seal having an upstream surface and a downstream surface, the radial seal at least partially disposed within the slot upstream from the heat shield, wherein the radial seal downstream surface is generally adjacent to the heat shield outer surface.

16. The combustor as in claim 15 , wherein the heat shield further comprises at least one spacer that extends from the heat shield outer surface towards the radial seal downstream surface.

17. The combustor as in claim 16 , further comprising a second cooling flow passage at least partially defined between the radial seal downstream surface and the outer surface of the heat shield.

Assignees

• Simo John Alfred
• Melton Patrick Benedict
• Dicintio Richard Martin
• Willis Christopher Paul
• Gen Electric

Inventors

• Simo John Alfred
• Melton Patrick Benedict
• Dicintio Richard Martin
• Willis Christopher Paul

Classifications

• F23R3/60

  Support structures; Attaching or mounting means · CPC title

• F01D25/28

  Supporting or mounting arrangements, e.g. for turbine casing · CPC title

• F01D9/023 Primary

  Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings · CPC title