GB201010159D0 - Turbine airfoil casting method - Google Patents
Turbine airfoil casting methodInfo
- Publication number
- GB201010159D0 GB201010159D0 GBGB1010159.0A GB201010159A GB201010159D0 GB 201010159 D0 GB201010159 D0 GB 201010159D0 GB 201010159 A GB201010159 A GB 201010159A GB 201010159 D0 GB201010159 D0 GB 201010159D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- casting method
- turbine airfoil
- airfoil casting
- turbine
- casting
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn
Links
- 238000005266 casting Methods 0.000 title 1
- 238000000034 method Methods 0.000 title 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P6/00—Restoring or reconditioning objects
- B23P6/04—Repairing fractures or cracked metal parts or products, e.g. castings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C9/00—Moulds or cores; Moulding processes
- B22C9/02—Sand moulds or like moulds for shaped castings
- B22C9/04—Use of lost patterns
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C9/00—Moulds or cores; Moulding processes
- B22C9/10—Cores; Manufacture or installation of cores
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
- F01D5/187—Convection cooling
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/20—Manufacture essentially without removing material
- F05D2230/21—Manufacture essentially without removing material by casting
- F05D2230/211—Manufacture essentially without removing material by casting by precision casting, e.g. microfusing or investment casting
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/202—Heat transfer, e.g. cooling by film cooling
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/221—Improvement of heat transfer
- F05D2260/2212—Improvement of heat transfer by creating turbulence
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Molds, Cores, And Manufacturing Methods Thereof (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US11/968,022 US20090165988A1 (en) | 2007-12-31 | 2007-12-31 | Turbine airfoil casting method |
| PCT/US2008/086569 WO2009085654A1 (en) | 2007-12-31 | 2008-12-12 | Turbine airfoil casting method |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| GB201010159D0 true GB201010159D0 (en) | 2010-07-28 |
| GB2468083A GB2468083A (en) | 2010-08-25 |
Family
ID=40342316
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1010159A Withdrawn GB2468083A (en) | 2007-12-31 | 2008-12-12 | Turbine airfoil casting method |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US20090165988A1 (en) |
| JP (1) | JP2011509185A (en) |
| CA (1) | CA2709940A1 (en) |
| DE (1) | DE112008003545T5 (en) |
| GB (1) | GB2468083A (en) |
| WO (1) | WO2009085654A1 (en) |
Families Citing this family (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8752609B2 (en) * | 2009-11-05 | 2014-06-17 | Dresser-Rand Company | One-piece manufacturing process |
| US9550230B2 (en) * | 2011-09-16 | 2017-01-24 | United Technologies Corporation | Mold for casting a workpiece that includes one or more casting pins |
| US9687910B2 (en) | 2012-12-14 | 2017-06-27 | United Technologies Corporation | Multi-shot casting |
| US10035185B2 (en) | 2012-12-14 | 2018-07-31 | United Technologies Corporation | Hybrid turbine blade for improved engine performance or architecture |
| US9057276B2 (en) * | 2013-02-06 | 2015-06-16 | Siemens Aktiengesellschaft | Twisted gas turbine engine airfoil having a twisted rib |
| US9797258B2 (en) * | 2013-10-23 | 2017-10-24 | General Electric Company | Turbine bucket including cooling passage with turn |
| WO2015112583A1 (en) * | 2014-01-21 | 2015-07-30 | United Technologies Corporation | Method for forming single crystal components using additive manufacturing and re-melt |
| US9435211B2 (en) | 2014-05-09 | 2016-09-06 | United Technologies Corporation | Method for forming components using additive manufacturing and re-melt |
| FR3037830B1 (en) * | 2015-06-29 | 2024-02-16 | Snecma | MOLDING ASSEMBLY FOR A TURBOMACHINE BLADE, INCLUDING A LARGE SECTION RELIEF PORTION |
| FR3037972B1 (en) * | 2015-06-29 | 2017-07-21 | Snecma | PROCESS SIMPLIFYING THE CORE USED FOR THE MANUFACTURE OF A TURBOMACHINE BLADE |
| US10053989B2 (en) * | 2015-12-21 | 2018-08-21 | General Electric Company | Cooling circuit for a multi-wall blade |
| US20180161866A1 (en) | 2016-12-13 | 2018-06-14 | General Electric Company | Multi-piece integrated core-shell structure for making cast component |
| US10807154B2 (en) | 2016-12-13 | 2020-10-20 | General Electric Company | Integrated casting core-shell structure for making cast component with cooling holes in inaccessible locations |
| US20180161853A1 (en) * | 2016-12-13 | 2018-06-14 | General Electric Company | Integrated casting core-shell structure with floating tip plenum |
| US11813669B2 (en) | 2016-12-13 | 2023-11-14 | General Electric Company | Method for making an integrated core-shell structure |
| WO2019046036A1 (en) * | 2017-08-28 | 2019-03-07 | Siemens Aktiengesellschaft | Method for making a turbine airfoil |
| DE102021204782A1 (en) | 2021-05-11 | 2022-11-17 | Siemens Energy Global GmbH & Co. KG | Improved blade tip in new or repaired part and process |
Family Cites Families (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3659645A (en) * | 1965-08-09 | 1972-05-02 | Trw Inc | Means for supporting core in open ended shell mold |
| US5810552A (en) * | 1992-02-18 | 1998-09-22 | Allison Engine Company, Inc. | Single-cast, high-temperature, thin wall structures having a high thermal conductivity member connecting the walls and methods of making the same |
| US5584663A (en) | 1994-08-15 | 1996-12-17 | General Electric Company | Environmentally-resistant turbine blade tip |
| DE19905887C1 (en) * | 1999-02-11 | 2000-08-24 | Abb Alstom Power Ch Ag | Hollow cast component |
| US6454156B1 (en) * | 2000-06-23 | 2002-09-24 | Siemens Westinghouse Power Corporation | Method for closing core printout holes in superalloy gas turbine blades |
| US6495793B2 (en) * | 2001-04-12 | 2002-12-17 | General Electric Company | Laser repair method for nickel base superalloys with high gamma prime content |
| EP1396299A1 (en) * | 2002-09-06 | 2004-03-10 | Siemens Aktiengesellschaft | Process for filling up a hole in a component |
| EP1561536A1 (en) * | 2004-02-03 | 2005-08-10 | Siemens Aktiengesellschaft | Process of brazing repairing of a part having a base material with oriented microstructure |
| US7322396B2 (en) * | 2005-10-14 | 2008-01-29 | General Electric Company | Weld closure of through-holes in a nickel-base superalloy hollow airfoil |
-
2007
- 2007-12-31 US US11/968,022 patent/US20090165988A1/en not_active Abandoned
-
2008
- 2008-12-12 GB GB1010159A patent/GB2468083A/en not_active Withdrawn
- 2008-12-12 DE DE112008003545T patent/DE112008003545T5/en not_active Withdrawn
- 2008-12-12 JP JP2010540763A patent/JP2011509185A/en active Pending
- 2008-12-12 WO PCT/US2008/086569 patent/WO2009085654A1/en not_active Ceased
- 2008-12-12 CA CA2709940A patent/CA2709940A1/en not_active Abandoned
Also Published As
| Publication number | Publication date |
|---|---|
| WO2009085654A1 (en) | 2009-07-09 |
| JP2011509185A (en) | 2011-03-24 |
| GB2468083A (en) | 2010-08-25 |
| US20090165988A1 (en) | 2009-07-02 |
| CA2709940A1 (en) | 2009-07-09 |
| DE112008003545T5 (en) | 2010-12-09 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |