Hold and cool process for superalloy joining

Patent metadata

Field	Value
Publication number	US-9347124-B2
Application number	US-201213489863-A
Country	US
Kind code	B2
Filing date	Jun 6, 2012
Priority date	Nov 7, 2011
Publication date	May 24, 2016
Grant date	May 24, 2016

Abstract

Ni base superalloys containing relatively large amounts of Al and/or Ti are known to be difficult to weld satisfactorily. As the Al and Ti content of the superalloy is increased to improve the strength, the weldability of the component is drastically reduced. It is concluded herein that reducing the γ′ phase improves weldability. A stepwise, controlled heating and cooling process is described to be used in cooperation with a welding process to reduce the γ′ present and thereby improve weldability.

First claim

What is claimed is:

1. A nickel base superalloy, alloy 247, including a welded seam therein wherein said welded seam was produced by the process of:
a) prior to welding, heating the weld location to an initial predetermined temperature above about 2100 deg. F. with a first heat source,
b) welding said nickel base superalloy with a second heat source; and,
c) removing said second heat source immediately upon completion of said welding; and,
d) performing a controlled step cooling of said weld location such that no more than about 30 weight percent of the γ′ phase is formed at any hold temperature during the step cool and hold process; and,
e) cooling said weld location to room temperature to produce a final γ′ weight percent of less than 30 percent.

2. A superalloy component assembly having therein the welded seam formed by the process of claim 1 .

3. The superalloy component assembly of claim 2 , wherein the said component assembly comprises a turbine blade.

4. A superalloy component assembly formed by joining nickel base superalloy components of alloy 247 at one or more joining locations by the process comprising:
a) heating said one or more joining locations to a temperature above about 2100 deg. F. with a first heat source;
b) welding said one or more joining locations of said nickel base superalloy components with a second heat source at a temperature above about 2100 deg. F.;
c) removing said second heat source immediately upon completion of said welding; and,
d) performing a controlled step and hold cooling of said welds such that no more than about 30 weight percent of the γ′ phase is formed at any hold portion of said cooling process; and,
e) cooling said one or more joining locations to room temperature to produce a final γ′ weight percent of less than 30 percent.

5. The superalloy component assembly of claim 4 , wherein the said component assembly comprises a turbine blade.

6. A nickel base superalloy, alloy 247, including a welded seam therein wherein said welded seam was produced by the process of:
a) prior to welding, heating the weld location to an initial predetermined temperature above about 2100 deg. F. with a first heat source,
b) welding said nickel base superalloy with a second heat source; and,
c) removing said second heat source immediately upon completion of said welding; and,
d) performing a controlled step cooling of said weld location such that no more than about 20 weight percent of the γ′ phase is formed at any hold temperature during the step cool and hold process; and,
e) cooling said weld location to room temperature to produce a final γ′ weight percent of less than 30 percent.

7. A superalloy component assembly having therein the welded seam formed by the process of claim 6 .

8. The superalloy component assembly of claim 7 , wherein the said component assembly comprises a turbine blade.

9. A superalloy component assembly formed by joining nickel base superalloy alloy 247 components at one or more joining locations by the process comprising:
a) heating said one or more joining locations to a temperature above about 2100 deg. F. with a first heat source;
b) welding said one or more joining locations of said nickel base superalloy components with a second heat source at a temperature above about 2100 deg. F.;
c) removing said second heat source immediately upon completion of said welding; and,
d) performing a controlled step and hold cooling of said welds such that no more than about 20 weight percent of the γ′ phase is formed at any hold portion of said cooling process; and,
e) cooling said one or more joining locations to room temperature to produce a final γ′ weight percent of less than 30 percent.

10. The superalloy component assembly of claim 9 , wherein the said component assembly comprises a turbine blade.

Assignees

• Ozbaysal Kazim
• Abdo Zafir A M
• Timotin Ovidiu
• Kamel Ahmed
• Siemens Energy Inc

Inventors

• Ozbaysal Kazim
• Abdo Zafir A M
• Timotin Ovidiu
• Kamel Ahmed

Classifications

• B23K2103/08

  Non-ferrous metals or alloys · CPC title

• F05D2230/80

  Repairing, retrofitting or upgrading methods · CPC title

• B23K2103/14

  Titanium or alloys thereof · CPC title

• F05D2300/177

  Ni - Si alloys · CPC title

• B23K26/342

  Build-up welding · CPC title