Gas turbine transition piece aft frame assembly supports

Patent metadata

Field	Value
Publication number	US-2016169113-A1
Application number	US-201414568394-A
Country	US
Kind code	A1
Filing date	Dec 12, 2014
Priority date	Dec 12, 2014
Publication date	Jun 16, 2016
Grant date	—

Abstract

Aft frame assemblies for aft ends of gas turbine transition pieces comprise a body comprising a downstream facing seal surface on an aft end, wherein at least a portion of the downstream facing seal surface configured to be exposed to a combustion discharge stream, a heat shield disposed proximate the aft end of the body, wherein the heat shield is configured to deflect at least a portion of the combustion discharge stream away from the aft end of the body, and, one or more heat shield supports connected to the body and configured to at least partially restrict deflection of the heat shield back towards the body.

First claim

What is claimed is:

1 . An aft frame assembly for an aft end of a gas turbine transition piece, the aft frame assembly comprising:
a body comprising a downstream facing seal surface on an aft end, at least a portion of the downstream facing seal surface configured to be exposed to a combustion discharge stream; a heat shield disposed proximate the aft end of the body, wherein the heat shield is configured to deflect at least a portion of the combustion discharge stream away from the aft end of the body; and, one or more heat shield supports connected to the body and configured to at least partially restrict deflection of the heat shield back towards the body.

2 . The aft frame assembly of claim 1 , wherein the teat shield and the body comprise one continuous piece.

3 . The aft frame assembly of claim 1 , further comprising an exterior trench separation at a least a portion of the heat shield from the body.

4 . The aft frame assembly of claim 1 , wherein the one or more heat shield supports are connected to an exterior surface of body.

5 . The aft frame assembly of claim 1 , wherein the one or more heat shield supports are at least partially disposed in a recess in an exterior surface of the body.

6 . The aft frame assembly of claim 1 , wherein the one or more heat shield supports comprise a support arm extending from a base portion.

7 . The aft frame assembly of claim 6 , wherein the base portion is connected to an exterior surface of the body.

8 . The aft frame assembly of claim 7 , wherein the base portion and the support arm are at least partially disposed in a recess in the exterior surface of the body.

9 . The aft frame assembly of claim 6 , wherein the base portion comprises one or more connection gaps, and wherein the base portion is connected to the body by welding at the one or more connection gaps.

10 . The aft frame assembly of claim 1 , wherein at least one heat shield support is configured to at least initially be separated from the heat shield by a tolerance gap.

11 . The aft frame assembly of claim 1 , wherein the body comprises a plurality of walls.

12 . The aft frame assembly of claim 11 , wherein each of the plurality of walls comprise at least one heat shield support.

13 . The aft frame assembly of claim 1 , wherein the heat shield comprises the downstream facing seal surface.

14 . The aft frame assembly of claim 1 , further comprising one or more exterior cooling holes fluidly connected to one or more interior cooling outlets.

15 . A method for assembling a gas turbine transition piece, the method comprising:
connecting an aft frame assembly on an aft end of the gas turbine transition piece, the aft frame assembly comprising:
a body comprising a downstream facing seal surface on an aft end, at least a portion of the downstream facing seal surface configured to be exposed to a combustion discharge stream; and,
a heat shield disposed proximate the aft end of the body, wherein the heat shield is configured to deflect at least a portion of the combustion discharge stream away from the aft end of the body; and,
connecting one or more heat shield supports to the body, wherein the one or more heat shield supports are configured to at least partially restrict deflection of the heat shield back towards the body.

16 . The method of claim 15 , wherein the one or more heat shield supports comprise a support arm extending from a base portion.

17 . The method of claim 16 , wherein the base portion comprises one or more connection gaps, and wherein connecting the one or more heat shield supports comprises welding at the one or more connection gaps.

18 . The method of claim 15 , wherein connecting the one or more heat shield supports to the body comprises connecting the one or more heat shield supports to an exterior surface of the body.

19 . The method of claim 15 , wherein the body comprises a plurality of walls, and wherein connecting the one or more heat shield supports to the body comprises connecting at least one heat shield support to each of the walls.

20 . The method of claim 15 , wherein connecting the one or more heat shield supports comprises separating at least one heat shield support from the heat shield by a tolerance gap.

Assignees

• Gen Electric

Inventors

• Bellino Mark Carmine
• Stoia Lucas John
• Willis Christopher Paul

Classifications

• F02C7/32

  Arrangement, mounting, or driving, of auxiliaries · CPC title

• F05D2220/32

  in gas turbines · CPC title

• F05D2240/90

  Mounting on supporting structures or systems · CPC title

• F02C7/24 Primary

  Heat or noise insulation (air intakes having provisions for noise suppression F02C7/045; turbine exhaust heads, chambers, or the like F01D25/30; silencing nozzles of jet-propulsion plants F02K1/00) · CPC title

• F01D25/145

  Thermally insulated casings · CPC title