DE50108928D1 - Verfahren zur Herstellung eines thermisch belasteten Gussteils - Google Patents
Verfahren zur Herstellung eines thermisch belasteten GussteilsInfo
- Publication number
- DE50108928D1 DE50108928D1 DE50108928T DE50108928T DE50108928D1 DE 50108928 D1 DE50108928 D1 DE 50108928D1 DE 50108928 T DE50108928 T DE 50108928T DE 50108928 T DE50108928 T DE 50108928T DE 50108928 D1 DE50108928 D1 DE 50108928D1
- Authority
- DE
- Germany
- Prior art keywords
- producing
- thermally loaded
- loaded casting
- casting
- thermally
- 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.)
- Expired - Lifetime
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C7/00—Patterns; Manufacture thereof so far as not provided for in other classes
- B22C7/02—Lost patterns
- B22C7/023—Patterns made from expanded plastic materials
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C7/00—Patterns; Manufacture thereof so far as not provided for in other classes
- B22C7/02—Lost patterns
-
- 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
- B22C9/02—Sand moulds or like moulds for shaped castings
- B22C9/04—Use of lost patterns
- B22C9/043—Removing the consumable pattern
-
- 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
-
- 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
- F01D5/182—Transpiration cooling
- F01D5/183—Blade walls being porous
-
- 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
- F01D5/186—Film cooling
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/606—Directionally-solidified crystalline structures
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/611—Coating
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/612—Foam
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE50108928T DE50108928D1 (de) | 2000-05-17 | 2001-04-12 | Verfahren zur Herstellung eines thermisch belasteten Gussteils |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE10024302A DE10024302A1 (de) | 2000-05-17 | 2000-05-17 | Verfahren zur Herstellung eines thermisch belasteten Gussteils |
DE50108928T DE50108928D1 (de) | 2000-05-17 | 2001-04-12 | Verfahren zur Herstellung eines thermisch belasteten Gussteils |
Publications (1)
Publication Number | Publication Date |
---|---|
DE50108928D1 true DE50108928D1 (de) | 2006-04-20 |
Family
ID=7642477
Family Applications (3)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE10024302A Withdrawn DE10024302A1 (de) | 2000-05-17 | 2000-05-17 | Verfahren zur Herstellung eines thermisch belasteten Gussteils |
DE50108928T Expired - Lifetime DE50108928D1 (de) | 2000-05-17 | 2001-04-12 | Verfahren zur Herstellung eines thermisch belasteten Gussteils |
DE50114026T Expired - Lifetime DE50114026D1 (de) | 2000-05-17 | 2001-04-12 | Verfahren zur Herstellung eines thermisch belasteten Gussteils |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE10024302A Withdrawn DE10024302A1 (de) | 2000-05-17 | 2000-05-17 | Verfahren zur Herstellung eines thermisch belasteten Gussteils |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE50114026T Expired - Lifetime DE50114026D1 (de) | 2000-05-17 | 2001-04-12 | Verfahren zur Herstellung eines thermisch belasteten Gussteils |
Country Status (3)
Country | Link |
---|---|
US (1) | US6412541B2 (de) |
EP (2) | EP1645347B1 (de) |
DE (3) | DE10024302A1 (de) |
Families Citing this family (73)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1186748A1 (de) * | 2000-09-05 | 2002-03-13 | Siemens Aktiengesellschaft | Laufschaufel für eine Strömungsmaschine sowie Strömungsmaschine |
US6695582B2 (en) * | 2002-06-06 | 2004-02-24 | General Electric Company | Turbine blade wall cooling apparatus and method of fabrication |
AU2005233004C1 (en) * | 2003-03-13 | 2011-08-04 | Kureha Corporation | Porous water filtration membrane of vinylidene fluoride resin hollow fiber and process for production thereof |
EP1475567A1 (de) * | 2003-05-08 | 2004-11-10 | Siemens Aktiengesellschaft | Schichtstruktur und Verfahren zur Herstellung einer Schichtstruktur |
EP1481747A3 (de) * | 2003-05-27 | 2007-05-02 | Alstom Technology Ltd | Verfahren zur Herstellung eines wärmebelasteten Bauteils sowie wärmebelastetes Bauteil |
EP1496140A1 (de) * | 2003-07-09 | 2005-01-12 | Siemens Aktiengesellschaft | Schichtstruktur und Verfahren zur Herstellung einer Schichtstruktur |
EP1533113A1 (de) | 2003-11-14 | 2005-05-25 | Siemens Aktiengesellschaft | Hochtemperatur-Schichtsystem zur Wärmeableitung und Verfahren zu dessen Herstellung |
US20050111966A1 (en) * | 2003-11-26 | 2005-05-26 | Metheny Alfred P. | Construction of static structures for gas turbine engines |
DE10360164A1 (de) * | 2003-12-20 | 2005-07-21 | Mtu Aero Engines Gmbh | Gasturbinenbauteil |
US7144220B2 (en) * | 2004-07-30 | 2006-12-05 | United Technologies Corporation | Investment casting |
DE102005002671B3 (de) * | 2005-01-14 | 2006-06-22 | Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. | Turbinenschaufel für Strömungsmaschinen und Verfahren zu ihrer Herstellung |
US7500828B2 (en) * | 2005-05-05 | 2009-03-10 | Florida Turbine Technologies, Inc. | Airfoil having porous metal filled cavities |
US20080257517A1 (en) * | 2005-12-16 | 2008-10-23 | General Electric Company | Mold assembly for use in a liquid metal cooled directional solidification furnace |
DE102006031305A1 (de) * | 2006-07-06 | 2008-01-10 | Mtu Aero Engines Gmbh | Gasturbinenbauteil für Flugtriebwerke sowie Verfahren zur Herstellung von Gasturbinenbauteilen für Flugtriebwerke |
GB0613715D0 (en) | 2006-07-11 | 2006-08-23 | Rolls Royce Plc | A seal between relatively moveable members |
US7968144B2 (en) * | 2007-04-10 | 2011-06-28 | Siemens Energy, Inc. | System for applying a continuous surface layer on porous substructures of turbine airfoils |
EP2184449A1 (de) * | 2008-11-05 | 2010-05-12 | Siemens Aktiengesellschaft | Leitschaufelträger, und Gasturbine und Gas- bzw. Dampfturbinenanlage mit solchem Leitschaufelträger |
GB0822416D0 (en) * | 2008-12-10 | 2009-01-14 | Rolls Royce Plc | A seal and a method of manufacturing a seal |
WO2011019672A2 (en) * | 2009-08-09 | 2011-02-17 | Rolls-Royce Corporation | Support for a fired article |
EP2418354A1 (de) | 2010-08-10 | 2012-02-15 | Siemens Aktiengesellschaft | Verfahren zur Herstellung einer innengekühlten Turbinenschaufel und Gasturbine mit einer so hergestellten Turbinenschaufel |
US8387245B2 (en) | 2010-11-10 | 2013-03-05 | General Electric Company | Components with re-entrant shaped cooling channels and methods of manufacture |
US8673397B2 (en) | 2010-11-10 | 2014-03-18 | General Electric Company | Methods of fabricating and coating a component |
US9249491B2 (en) | 2010-11-10 | 2016-02-02 | General Electric Company | Components with re-entrant shaped cooling channels and methods of manufacture |
US8727727B2 (en) | 2010-12-10 | 2014-05-20 | General Electric Company | Components with cooling channels and methods of manufacture |
US8753071B2 (en) | 2010-12-22 | 2014-06-17 | General Electric Company | Cooling channel systems for high-temperature components covered by coatings, and related processes |
US8807944B2 (en) * | 2011-01-03 | 2014-08-19 | General Electric Company | Turbomachine airfoil component and cooling method therefor |
US8533949B2 (en) | 2011-02-14 | 2013-09-17 | General Electric Company | Methods of manufacture for components with cooling channels |
US8793871B2 (en) | 2011-03-17 | 2014-08-05 | Siemens Energy, Inc. | Process for making a wall with a porous element for component cooling |
US8528208B2 (en) | 2011-04-11 | 2013-09-10 | General Electric Company | Methods of fabricating a coated component using multiple types of fillers |
US8601691B2 (en) | 2011-04-27 | 2013-12-10 | General Electric Company | Component and methods of fabricating a coated component using multiple types of fillers |
US9216491B2 (en) | 2011-06-24 | 2015-12-22 | General Electric Company | Components with cooling channels and methods of manufacture |
US9327384B2 (en) | 2011-06-24 | 2016-05-03 | General Electric Company | Components with cooling channels and methods of manufacture |
US9057523B2 (en) * | 2011-07-29 | 2015-06-16 | United Technologies Corporation | Microcircuit cooling for gas turbine engine combustor |
US9206696B2 (en) | 2011-08-16 | 2015-12-08 | General Electric Company | Components with cooling channels and methods of manufacture |
US9249672B2 (en) | 2011-09-23 | 2016-02-02 | General Electric Company | Components with cooling channels and methods of manufacture |
US20130086784A1 (en) | 2011-10-06 | 2013-04-11 | General Electric Company | Repair methods for cooled components |
US9249670B2 (en) | 2011-12-15 | 2016-02-02 | General Electric Company | Components with microchannel cooling |
WO2013144022A1 (en) | 2012-03-28 | 2013-10-03 | Alstom Technology Ltd | Method for removing a ceramic |
US9435208B2 (en) | 2012-04-17 | 2016-09-06 | General Electric Company | Components with microchannel cooling |
US9243503B2 (en) | 2012-05-23 | 2016-01-26 | General Electric Company | Components with microchannel cooled platforms and fillets and methods of manufacture |
DE102013109116A1 (de) | 2012-08-27 | 2014-03-27 | General Electric Company (N.D.Ges.D. Staates New York) | Bauteil mit Kühlkanälen und Verfahren zur Herstellung |
US8974859B2 (en) | 2012-09-26 | 2015-03-10 | General Electric Company | Micro-channel coating deposition system and method for using the same |
US9242294B2 (en) | 2012-09-27 | 2016-01-26 | General Electric Company | Methods of forming cooling channels using backstrike protection |
US9238265B2 (en) | 2012-09-27 | 2016-01-19 | General Electric Company | Backstrike protection during machining of cooling features |
US9562436B2 (en) | 2012-10-30 | 2017-02-07 | General Electric Company | Components with micro cooled patterned coating layer and methods of manufacture |
US9200521B2 (en) | 2012-10-30 | 2015-12-01 | General Electric Company | Components with micro cooled coating layer and methods of manufacture |
US9003657B2 (en) | 2012-12-18 | 2015-04-14 | General Electric Company | Components with porous metal cooling and methods of manufacture |
US10156359B2 (en) | 2012-12-28 | 2018-12-18 | United Technologies Corporation | Gas turbine engine component having vascular engineered lattice structure |
US10018052B2 (en) | 2012-12-28 | 2018-07-10 | United Technologies Corporation | Gas turbine engine component having engineered vascular structure |
US9759090B2 (en) * | 2013-03-03 | 2017-09-12 | Rolls-Royce North American Technologies, Inc. | Gas turbine engine component having foam core and composite skin with cooling slot |
DE102013212465B4 (de) * | 2013-06-27 | 2015-03-12 | MTU Aero Engines AG | Dichtanordnung für eine Strömungsmaschine, eine Leitschaufelanordnung und eine Strömungsmaschine mit einer derartigen Dichtanordnung |
US20150064019A1 (en) * | 2013-08-30 | 2015-03-05 | General Electric Company | Gas Turbine Components with Porous Cooling Features |
US9278462B2 (en) | 2013-11-20 | 2016-03-08 | General Electric Company | Backstrike protection during machining of cooling features |
US9476306B2 (en) | 2013-11-26 | 2016-10-25 | General Electric Company | Components with multi-layered cooling features and methods of manufacture |
WO2015112885A1 (en) * | 2014-01-23 | 2015-07-30 | United Technologies Corporation | An additive manufactured mold, a method of manufacturing the mold, and a workpiece casted from the mold |
US9789536B2 (en) | 2015-01-20 | 2017-10-17 | United Technologies Corporation | Dual investment technique for solid mold casting of reticulated metal foams |
US9737930B2 (en) | 2015-01-20 | 2017-08-22 | United Technologies Corporation | Dual investment shelled solid mold casting of reticulated metal foams |
US9789534B2 (en) | 2015-01-20 | 2017-10-17 | United Technologies Corporation | Investment technique for solid mold casting of reticulated metal foams |
US10094287B2 (en) | 2015-02-10 | 2018-10-09 | United Technologies Corporation | Gas turbine engine component with vascular cooling scheme |
US9884363B2 (en) | 2015-06-30 | 2018-02-06 | United Technologies Corporation | Variable diameter investment casting mold for casting of reticulated metal foams |
US9731342B2 (en) | 2015-07-07 | 2017-08-15 | United Technologies Corporation | Chill plate for equiax casting solidification control for solid mold casting of reticulated metal foams |
US10221694B2 (en) | 2016-02-17 | 2019-03-05 | United Technologies Corporation | Gas turbine engine component having vascular engineered lattice structure |
US10458259B2 (en) * | 2016-05-12 | 2019-10-29 | General Electric Company | Engine component wall with a cooling circuit |
US10598026B2 (en) * | 2016-05-12 | 2020-03-24 | General Electric Company | Engine component wall with a cooling circuit |
US20180051566A1 (en) * | 2016-08-16 | 2018-02-22 | General Electric Company | Airfoil for a turbine engine with a porous tip |
US10583489B2 (en) * | 2017-04-26 | 2020-03-10 | General Electric Company | Method of providing cooling structure for a component |
US20180347442A1 (en) * | 2017-05-31 | 2018-12-06 | General Electric Company | Lattice structure in cooling pathway by additive manufacture |
US10974312B2 (en) | 2017-06-28 | 2021-04-13 | General Electric Company | Additively manufactured casting core-shell mold with integrated filter and ceramic shell |
US11208902B2 (en) * | 2018-12-03 | 2021-12-28 | General Electric Company | Tip rail cooling insert for turbine blade tip cooling system and related method |
US10774653B2 (en) | 2018-12-11 | 2020-09-15 | Raytheon Technologies Corporation | Composite gas turbine engine component with lattice structure |
CN110566290A (zh) * | 2019-07-23 | 2019-12-13 | 华南理工大学 | 金属丝冶金结合多孔材料在制造耐高温机械零件的应用 |
US11746660B2 (en) | 2021-12-20 | 2023-09-05 | Rolls-Royce Plc | Gas turbine engine components with foam filler for impact resistance |
US11834956B2 (en) * | 2021-12-20 | 2023-12-05 | Rolls-Royce Plc | Gas turbine engine components with metallic and ceramic foam for improved cooling |
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GB2310896A (en) * | 1996-03-05 | 1997-09-10 | Rolls Royce Plc | Air cooled wall |
DE19612500A1 (de) * | 1996-03-29 | 1997-10-02 | Bleistahl Prod Gmbh & Co Kg | Verfahren zur Herstellung von Zylinderköpfen für Verbrennungsmotoren |
DE19718886A1 (de) * | 1997-05-03 | 1998-11-05 | Bosch Gmbh Robert | Verfahren zur Herstellung von porösen Formkörpern |
-
2000
- 2000-05-17 DE DE10024302A patent/DE10024302A1/de not_active Withdrawn
-
2001
- 2001-04-12 EP EP05111586A patent/EP1645347B1/de not_active Expired - Lifetime
- 2001-04-12 DE DE50108928T patent/DE50108928D1/de not_active Expired - Lifetime
- 2001-04-12 EP EP01109115A patent/EP1155760B1/de not_active Expired - Lifetime
- 2001-04-12 DE DE50114026T patent/DE50114026D1/de not_active Expired - Lifetime
- 2001-04-18 US US09/836,297 patent/US6412541B2/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
US20010042607A1 (en) | 2001-11-22 |
EP1645347A1 (de) | 2006-04-12 |
DE50114026D1 (de) | 2008-07-24 |
EP1645347B1 (de) | 2008-06-11 |
DE10024302A1 (de) | 2001-11-22 |
EP1155760B1 (de) | 2006-02-15 |
EP1155760A1 (de) | 2001-11-21 |
US6412541B2 (en) | 2002-07-02 |
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