Sprayed skin turbine component
Abstract
Fabricating a turbine component (50) by casting a core structure (30), forming an array of pits (24) in an outer surface (32) of the core structure, depositing a transient liquid phase (TLP) material (40) on the outer surface of the core structure, the TLP containing a melting-point depressant, depositing a skin (42) on the outer surface of the core structure over the TLP material, and heating the assembly, thus forming both a diffusion bond and a mechanical interlock between the skin and the core structure. The heating diffuses the melting-point depressant away from the interface. Subsurface cooling channels (35) may be formed by forming grooves (34) in the outer surface of the core structure, filling the grooves with a fugitive filler (36), depositing and bonding the skin (42), then removing the fugitive material.
- Inventors:
- Issue Date:
- Research Org.:
- Siemens Energy, Inc. (Orlando, FL)
- Sponsoring Org.:
- USDOE
- OSTI Identifier:
- 1084372
- Patent Number(s):
- 8453327
- Application Number:
- 12/701,025
- Assignee:
- Siemens Energy, Inc. (Orlando, FL)
- Patent Classifications (CPCs):
-
B - PERFORMING OPERATIONS B23 - MACHINE TOOLS B23P - OTHER WORKING OF METAL
F - MECHANICAL ENGINEERING F01 - MACHINES OR ENGINES IN GENERAL F01D - NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- DOE Contract Number:
- FC26-05NT42644
- Resource Type:
- Patent
- Country of Publication:
- United States
- Language:
- English
- Subject:
- 42 ENGINEERING
Citation Formats
Allen, David B. Sprayed skin turbine component. United States: N. p., 2013.
Web.
Allen, David B. Sprayed skin turbine component. United States.
Allen, David B. Tue .
"Sprayed skin turbine component". United States. https://www.osti.gov/servlets/purl/1084372.
@article{osti_1084372,
title = {Sprayed skin turbine component},
author = {Allen, David B},
abstractNote = {Fabricating a turbine component (50) by casting a core structure (30), forming an array of pits (24) in an outer surface (32) of the core structure, depositing a transient liquid phase (TLP) material (40) on the outer surface of the core structure, the TLP containing a melting-point depressant, depositing a skin (42) on the outer surface of the core structure over the TLP material, and heating the assembly, thus forming both a diffusion bond and a mechanical interlock between the skin and the core structure. The heating diffuses the melting-point depressant away from the interface. Subsurface cooling channels (35) may be formed by forming grooves (34) in the outer surface of the core structure, filling the grooves with a fugitive filler (36), depositing and bonding the skin (42), then removing the fugitive material.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {Tue Jun 04 00:00:00 EDT 2013},
month = {Tue Jun 04 00:00:00 EDT 2013}
}
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Works referenced in this record:
Ceramic composite vane with metallic substructure
patent, February 2003
- Morrison, Jay A.; Merrill, Gary B.; Lane, Jay E.
- US Patent Document 6,514,046
Turbine airfoil with double shell outer wall
patent, July 1994
- Bunker, Ronald Scott; Wallace, Thomas Tracy
- US Patent Document 5,328,331
Turbine airfoil with convectively cooled double shell outer wall
patent, January 1996
- Isburgh, Anne M.; Lee, Ching-Pang
- US Patent Document 5,484,258
Ceramic matrix composite gas turbine vane
patent, March 2004
- Morrison, Jay A.; Campbell, Chris; Merrill, Gary B.
- US Patent Document 6,709,230
Layer system
patent, February 2007
- Bostanjoglo, Georg; Cox, Nigel-Philip; Wilkenhöner, Rolf
- US Patent Document 7,182,581
Layer system, and process for producing a layer system
patent, February 2007
- Bostanjoglo, Georg; Cox, Nigel-Philip; Wilkenhöner, Rolf
- US Patent Document 7,182,580
Method of forming internal passages within articles and articles formed by same
patent, March 1999
- McKinley, Barry L.
- US Patent Document 5,875,549
Device and method for producing a blade for a turbine and blade produced according to this method
patent, October 2004
- Tiemann, Peter
- US Patent Document 6,805,535
Lamellate CMC structure with interlock to metallic support structure
patent, July 2007
- Albrecht, Harry A.; Shteyman, Yevgeniy; Morrison, Jay A.
- US Patent Document 7,247,002
Bond coats for turbine components and method of applying the same
patent, May 2000
- Sabol, Stephen M.; Goedjen, John G.
- US Patent Document 6,060,174
Method for making a double-wall airfoil
patent, June 1997
- Jackson, Melvin Robert; Skelly, David W.; Rowe, Raymond Grant
- US Patent Document 5,640,767
Enhanced thermal barrier coating system
patent, May 1995
- Skelly, David W.; Nagaraj, Bangalore Aswatha; Wortman, David J.
- US Patent Document 5,419,971
Adhesion of a ceramic layer deposited on an article by casting features in the article surface
patent, June 2000
- Beverley, Michael; Heyward, John Peter; Conner, Jeffrey A.
- US Patent Document 6,074,706
Transient liquid phase bonding repair for advanced turbine blades and vanes
patent, January 2003
- Burke, Michael A.; Swartzbeck, Gary W.; Freyer, Paula
- US Patent Document 6,508,000