Process for producing combustor structural member, and combustor structural member, combustor for gas turbine and gas turbine

Patent metadata

Field	Value
Publication number	US-9370846-B2
Application number	US-78908410-A
Country	US
Kind code	B2
Filing date	May 27, 2010
Priority date	Jun 2, 2009
Publication date	Jun 21, 2016
Grant date	Jun 21, 2016

Abstract

A process including brazing a first plate-like member formed from a heat-resistant alloy, and a second plate-like member formed from a heat-resistant alloy and having fins on the surface, with the fins facing the first plate-like member, by interposing a brazing filler metal comprising a melting point lowering element between the two plate-like members, molding the plate-like assembly to form a combustor structural member, identifying, in accordance with the shape of the combustor structural member, strain locations where the strain generated during the press molding step exceeds a predetermined value, performing localized heating of the locations within the plate-like assembly corresponding with the strain locations identified, and as the above press molding step subjecting the plate-like assembly to cold press molding with the temperature of the heated locations corresponding with the strain locations maintained at a desired temperature.

First claim

What is claimed is:

1. A process for producing a combustor structural member, the process comprising:
brazing a first plate-like member formed from a heat-resistant alloy, and a second plate-like member formed from a heat-resistant alloy and having a plurality of fins on a surface thereof, with the second plate-like member positioned with the fins facing the first plate-like member, by interposing a brazing filler metal comprising a melting point lowering element between the first and second plate-like members, thereby forming a first plate-like assembly,
identifying strain locations in a second plate-like assembly where a strain exceeds a predetermined value after being press-molded into a desired shape, said second plate-like assembly having been formed by brazing a third plate-like member formed from the first heat-resistant alloy and having a plurality of fins on surface thereof with the fourth plate-like member positioned with the fins facing the third plate-like member, by interposing the brazing filler metal comprising the melting point lowering element between the third and fourth plate-like members, prior to press-molding,
determining the locations within the first plate-like assembly corresponding to the identified strain locations within the second plate-like assembly,
performing localized heating of the determined locations within the first plate-like assembly, and then
subjecting the first plate-like assembly to cold press molding while maintaining a temperature of the determined locations subjected to the localized heating at a desired temperature.

2. The process for producing a combustor structural member according to claim 1 , wherein a heating temperature within the localized heating step is not less than 650° C. and not more than 1,000° C.

3. The process for producing a combustor structural member according to claim 1 , wherein a heating temperature within the localized heating step is not less than 800° C. and not more than 1,000° C.

4. A combustor structural member, produced using the process for producing a combustor structural member according to claim 1 .

5. A combustor for a gas turbine, molded using the combustor structural member according to claim 4 .

6. A gas turbine, comprising the combustor for a gas turbine according to claim 5 .

7. The process for producing a combustor structural member according to claim 1 ,
wherein a temperature of the localized heating is lower than melting points of the brazing filler metal, the first plate-like member, and the second plate-like member, and
wherein the first and second plate-like members are heated to a temperature in which a level of ductility equal or superior to that exhibited by the first plate-like member and the second plate-like member prior to embrittlement.

8. The process for producing a combustor structural member according to claim 1 , wherein the heat-resistant alloy is formed from a heat-resistant Ni-based alloy or a heat-resistant Co-based alloy.

9. The process for producing a combustor structural member according to claim 1 , wherein the strain locations where the strain in the second plate-like assembly exceeds the predetermined value are identified by performing a simulation analysis using physical property values for a material of the second plate-like assembly as input data, and using a die temperature, a die shape, and a coefficient of friction of a lubricant as parameters.

10. The process for producing a combustor structural member according to claim 1 , wherein the strain locations where the strain in the second plate-like assembly exceeds the predetermined value are identified using a degree of deformation after the press-molding of circular patters with a predetermined diameter marked on the second plate-like assembly.

11. The process for producing a combustor structural member according to claim 1 , wherein the cold press molding is subjected to the first plate-like assembly while the localized heating is performed.

Assignees

• Morimoto Hitoshi
• Taneike Masaki
• Nagai Tomoto
• Mitsubishi Hitachi Power Sys

Inventors

• Morimoto Hitoshi
• Taneike Masaki
• Nagai Tomoto

Classifications

• F23R2900/00018

  Manufacturing combustion chamber liners or subparts · CPC title

• B23P2700/13

  Parts of turbine combustion chambers · CPC title

• Y10T29/49616

  Structural member making · CPC title

• B23P15/00 Primary

  Making specific metal objects by operations not covered by a single other subclass or a group in this subclass · CPC title

• F23R3/002

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