Arrangement for cooling a component in the hot gas path of a gas turbine

Patent metadata

Field	Value
Publication number	US-9822654-B2
Application number	US-201414505588-A
Country	US
Kind code	B2
Filing date	Oct 3, 2014
Priority date	Oct 10, 2013
Publication date	Nov 21, 2017
Grant date	Nov 21, 2017

Abstract

A cooled wall segment in the hot gas path of a gas turbine. The wall segment includes a first surface, exposed to a medium of relatively high temperature, a second surface, exposed to a medium of relatively low temperature, and side surfaces connecting the first and second surface and defining a height of the wall segment. At least one cooling channel for a flow-through of a fluid cooling medium extends through the wall segment. Each cooling channel is provided with an inlet and an outlet for the cooling medium. The at least one cooling channel includes at least two heat transfer sections, a first heat transfer section extending essentially parallel to the first surface at a first distance from the first surface and a second heat transfer section extending essentially parallel to the first surface at a second distance, whereby the second distance is less than the first distance.

First claim

The invention claimed is:

1. A wall segment for a hot gas path of a gas turbine, comprising a first surface, exposed to a medium of a first temperature, a second surface, exposed to a medium of a second temperature that is lower than the first temperature, and side surfaces connecting said first and said second surface and defining a height of the wall segment, at least one cooling channel for a flow-through of a fluid cooling medium extending through the wall segment, each cooling channel being provided with an inlet for the fluid cooling medium and an outlet for the fluid cooling medium, wherein the at least one cooling channel comprises, a first heat transfer section extending essentially parallel to the first surface at a first distance from the first surface, a second heat transfer section extending essentially parallel to the first surface at a second distance from the first surface, whereby the second distance is less than the first distance, and a transition section in which a distance between a lower surface of the transition section and the first surface varies.

2. The wall segment according to claim 1 , wherein the at least one cooling channel comprises, in succession in the direction of flow of the fluid cooling medium, an inlet section for the fluid cooling medium, the first heat transfer section extending essentially parallel to the first surface of the wall segment in the first distance, the transition section with a direction vector towards the first surface, the second heat transfer section extending essentially parallel to the first surface in the second distance and an outlet for the fluid cooling medium.

3. The wall segment according to claim 1 , wherein the medium of the second temperature is the fluid cooling medium, preferably cooling air.

4. The wall segment according to claim 1 , wherein the inlet is arranged on the second surface, exposed to the medium of the second temperature.

5. The wall segment according to claim 1 , wherein the first section of the at least one cooling channel, running in a first distance essentially parallel to the surface, and the second section, running in a second distance essentially parallel to the surface, run parallel to each other.

6. The wall segment according to claim 5 , wherein said first section and the second section run parallel to each other with an opposite flow direction of the fluid cooling medium.

7. The wall segment according to claim 2 , wherein the transition section comprises two one-quarter bends.

8. The wall segment according to claim 2 , wherein the transition section has a component in the vertical direction towards the first surface and has a component in the horizontal direction.

9. The wall segment according to claim 1 , wherein the wall segment comprises two or more of cooling channels, whereby at least two cooling channels are arranged laterally reversed to each other.

10. The wall segment according to claim 1 , wherein the second surface of the wall segment, exposed to the medium of the second temperature, is configured to follow a structure of the cooling channels inside.

11. The wall segment according to claim 1 , wherein the at least one cooling channel has a rectangular cross-section.

12. The wall segment according to claim 1 , wherein the at least one cooling channel has a trapezoidal cross-section, whereby the base of the trapezoid is directed to the first surface, exposed to the medium of the first temperature.

13. The wall segment according to claim 1 , wherein the cross-sectional shape of at least one cooling channel is changing over the length.

14. The wall segment according to claim 1 , wherein the at least one cooling channel is partly or completely equipped with heat transfer enhancing means.

15. The wall segment according to claim 14 , wherein the heat transfer enhancing means are ribs.

Assignees

• Alstom Technology Ltd
• Ansaldo Energia Ip Uk Ltd

Inventors

• Brandl Herbert
• Sedlov Andrey Anatolievich
• Ivanov Artem

Classifications

• F01D9/06

  Fluid supply conduits to nozzles or the like · CPC title

• F05D2240/11

  Shroud seal segments · CPC title

• F01D25/14

  Casings modified therefor (double casings F01D25/26) · CPC title

• F01D9/065 Primary

  Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids (see also F01D25/16, F01D25/24 and F01D25/26) · CPC title

• F05D2240/15

  Heat shield · CPC title