CH703747B1 - Gasturbinenkomponente mit wenigstens einem gekrümmten Filmkühlungsloch und Verfahren für deren Herstellung. - Google Patents
Gasturbinenkomponente mit wenigstens einem gekrümmten Filmkühlungsloch und Verfahren für deren Herstellung. Download PDFInfo
- Publication number
- CH703747B1 CH703747B1 CH01365/11A CH13652011A CH703747B1 CH 703747 B1 CH703747 B1 CH 703747B1 CH 01365/11 A CH01365/11 A CH 01365/11A CH 13652011 A CH13652011 A CH 13652011A CH 703747 B1 CH703747 B1 CH 703747B1
- Authority
- CH
- Switzerland
- Prior art keywords
- film cooling
- cooling hole
- component
- film
- hole
- Prior art date
Links
Classifications
-
- 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
- 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
- F05D2250/00—Geometry
- F05D2250/10—Two-dimensional
- F05D2250/13—Two-dimensional trapezoidal
-
- 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
- F05D2250/00—Geometry
- F05D2250/20—Three-dimensional
- F05D2250/21—Three-dimensional pyramidal
-
- 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
- F05D2250/00—Geometry
- F05D2250/20—Three-dimensional
- F05D2250/23—Three-dimensional prismatic
- F05D2250/232—Three-dimensional prismatic conical
-
- 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
- F05D2250/00—Geometry
- F05D2250/30—Arrangement of components
- F05D2250/32—Arrangement of components according to their shape
- F05D2250/324—Arrangement of components according to their shape divergent
-
- 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
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49229—Prime mover or fluid pump making
- Y10T29/49236—Fluid pump or compressor making
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/49336—Blade making
- Y10T29/49339—Hollow blade
- Y10T29/49341—Hollow blade with cooling passage
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49995—Shaping one-piece blank by removing material
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US12/872,559 US8672613B2 (en) | 2010-08-31 | 2010-08-31 | Components with conformal curved film holes and methods of manufacture |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CH703747A2 CH703747A2 (de) | 2012-03-15 |
| CH703747B1 true CH703747B1 (de) | 2015-12-15 |
Family
ID=45697532
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CH01365/11A CH703747B1 (de) | 2010-08-31 | 2011-08-22 | Gasturbinenkomponente mit wenigstens einem gekrümmten Filmkühlungsloch und Verfahren für deren Herstellung. |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US8672613B2 (enExample) |
| JP (1) | JP5948027B2 (enExample) |
| CN (1) | CN102434287B (enExample) |
| CH (1) | CH703747B1 (enExample) |
| DE (1) | DE102011052675B4 (enExample) |
Families Citing this family (81)
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| US8672613B2 (en) * | 2010-08-31 | 2014-03-18 | General Electric Company | Components with conformal curved film holes and methods of manufacture |
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| US20130086784A1 (en) * | 2011-10-06 | 2013-04-11 | General Electric Company | Repair methods for cooled components |
| US9416665B2 (en) | 2012-02-15 | 2016-08-16 | United Technologies Corporation | Cooling hole with enhanced flow attachment |
| US9410435B2 (en) | 2012-02-15 | 2016-08-09 | United Technologies Corporation | Gas turbine engine component with diffusive cooling hole |
| US8689568B2 (en) | 2012-02-15 | 2014-04-08 | United Technologies Corporation | Cooling hole with thermo-mechanical fatigue resistance |
| US8850828B2 (en) | 2012-02-15 | 2014-10-07 | United Technologies Corporation | Cooling hole with curved metering section |
| US9273560B2 (en) | 2012-02-15 | 2016-03-01 | United Technologies Corporation | Gas turbine engine component with multi-lobed cooling hole |
| US8733111B2 (en) | 2012-02-15 | 2014-05-27 | United Technologies Corporation | Cooling hole with asymmetric diffuser |
| US8572983B2 (en) | 2012-02-15 | 2013-11-05 | United Technologies Corporation | Gas turbine engine component with impingement and diffusive cooling |
| US8683814B2 (en) | 2012-02-15 | 2014-04-01 | United Technologies Corporation | Gas turbine engine component with impingement and lobed cooling hole |
| US9284844B2 (en) | 2012-02-15 | 2016-03-15 | United Technologies Corporation | Gas turbine engine component with cusped cooling hole |
| US8683813B2 (en) | 2012-02-15 | 2014-04-01 | United Technologies Corporation | Multi-lobed cooling hole and method of manufacture |
| US9279330B2 (en) | 2012-02-15 | 2016-03-08 | United Technologies Corporation | Gas turbine engine component with converging/diverging cooling passage |
| US10422230B2 (en) | 2012-02-15 | 2019-09-24 | United Technologies Corporation | Cooling hole with curved metering section |
| US8522558B1 (en) | 2012-02-15 | 2013-09-03 | United Technologies Corporation | Multi-lobed cooling hole array |
| US9482100B2 (en) | 2012-02-15 | 2016-11-01 | United Technologies Corporation | Multi-lobed cooling hole |
| US8707713B2 (en) | 2012-02-15 | 2014-04-29 | United Technologies Corporation | Cooling hole with crenellation features |
| US9024226B2 (en) | 2012-02-15 | 2015-05-05 | United Technologies Corporation | EDM method for multi-lobed cooling hole |
| US8763402B2 (en) | 2012-02-15 | 2014-07-01 | United Technologies Corporation | Multi-lobed cooling hole and method of manufacture |
| US9598979B2 (en) | 2012-02-15 | 2017-03-21 | United Technologies Corporation | Manufacturing methods for multi-lobed cooling holes |
| US9422815B2 (en) | 2012-02-15 | 2016-08-23 | United Technologies Corporation | Gas turbine engine component with compound cusp cooling configuration |
| US8584470B2 (en) | 2012-02-15 | 2013-11-19 | United Technologies Corporation | Tri-lobed cooling hole and method of manufacture |
| US9416971B2 (en) | 2012-02-15 | 2016-08-16 | United Technologies Corporation | Multiple diffusing cooling hole |
| US10100650B2 (en) | 2012-06-30 | 2018-10-16 | General Electric Company | Process for selectively producing thermal barrier coatings on turbine hardware |
| US10113433B2 (en) | 2012-10-04 | 2018-10-30 | Honeywell International Inc. | Gas turbine engine components with lateral and forward sweep film cooling holes |
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| JP6057778B2 (ja) | 2013-02-27 | 2017-01-11 | 本田技研工業株式会社 | レーザ加工装置 |
| EP2971667B1 (en) * | 2013-03-15 | 2024-06-12 | RTX Corporation | Component for a gas turbine engine and method of manufacturing a component for a gas turbine engine |
| WO2014150490A1 (en) * | 2013-03-15 | 2014-09-25 | United Technologies Corporation | Additive manufacturing method for the addition of features within cooling holes |
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| US10370987B2 (en) | 2014-04-03 | 2019-08-06 | Mitsubishi Hitachi Power Systems, Ltd. | Blade or vane row and gas turbine |
| US10563514B2 (en) | 2014-05-29 | 2020-02-18 | General Electric Company | Fastback turbulator |
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| US20160153282A1 (en) * | 2014-07-11 | 2016-06-02 | United Technologies Corporation | Stress Reduction For Film Cooled Gas Turbine Engine Component |
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| US10982552B2 (en) * | 2014-09-08 | 2021-04-20 | Raytheon Technologies Corporation | Gas turbine engine component with film cooling hole |
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| US10443395B2 (en) | 2016-03-18 | 2019-10-15 | General Electric Company | Component for a turbine engine with a film hole |
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| US11065715B2 (en) * | 2016-05-03 | 2021-07-20 | General Electric Company | Combined liquid guided laser and electrical discharge machining |
| US11021965B2 (en) | 2016-05-19 | 2021-06-01 | Honeywell International Inc. | Engine components with cooling holes having tailored metering and diffuser portions |
| US10605092B2 (en) | 2016-07-11 | 2020-03-31 | United Technologies Corporation | Cooling hole with shaped meter |
| CN106761947B (zh) * | 2016-11-28 | 2018-11-20 | 西北工业大学 | 一种用于涡轮叶片的漏斗型气膜孔结构 |
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| US8672613B2 (en) * | 2010-08-31 | 2014-03-18 | General Electric Company | Components with conformal curved film holes and methods of manufacture |
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-
2010
- 2010-08-31 US US12/872,559 patent/US8672613B2/en active Active
-
2011
- 2011-08-12 DE DE102011052675.7A patent/DE102011052675B4/de active Active
- 2011-08-22 CH CH01365/11A patent/CH703747B1/de not_active IP Right Cessation
- 2011-08-24 JP JP2011182165A patent/JP5948027B2/ja active Active
- 2011-08-31 CN CN201110268454.3A patent/CN102434287B/zh active Active
Also Published As
| Publication number | Publication date |
|---|---|
| CN102434287A (zh) | 2012-05-02 |
| DE102011052675B4 (de) | 2021-07-29 |
| US8672613B2 (en) | 2014-03-18 |
| CH703747A2 (de) | 2012-03-15 |
| JP5948027B2 (ja) | 2016-07-06 |
| DE102011052675A1 (de) | 2012-03-29 |
| JP2012052535A (ja) | 2012-03-15 |
| CN102434287B (zh) | 2016-08-10 |
| US20120051941A1 (en) | 2012-03-01 |
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Representative=s name: GENERAL ELECTRIC TECHNOLOGY GMBH GLOBAL PATENT, CH |
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| PL | Patent ceased |