CA2553860C - Canal de refroidissement menage dans une paroi - Google Patents
Canal de refroidissement menage dans une paroi Download PDFInfo
- Publication number
- CA2553860C CA2553860C CA2553860A CA2553860A CA2553860C CA 2553860 C CA2553860 C CA 2553860C CA 2553860 A CA2553860 A CA 2553860A CA 2553860 A CA2553860 A CA 2553860A CA 2553860 C CA2553860 C CA 2553860C
- Authority
- CA
- Canada
- Prior art keywords
- wall
- orifice
- channel
- axis
- cone
- 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.)
- Active
Links
- 238000001816 cooling Methods 0.000 title claims abstract description 18
- 238000009792 diffusion process Methods 0.000 claims abstract description 35
- 238000000034 method Methods 0.000 claims abstract description 21
- 238000005304 joining Methods 0.000 claims abstract description 3
- 238000005553 drilling Methods 0.000 claims description 14
- 239000007789 gas Substances 0.000 description 4
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 239000013598 vector Substances 0.000 description 1
- 230000003313 weakening effect Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23H—WORKING OF METAL BY THE ACTION OF A HIGH CONCENTRATION OF ELECTRIC CURRENT ON A WORKPIECE USING AN ELECTRODE WHICH TAKES THE PLACE OF A TOOL; SUCH WORKING COMBINED WITH OTHER FORMS OF WORKING OF METAL
- B23H9/00—Machining specially adapted for treating particular metal objects or for obtaining special effects or results on metal objects
- B23H9/10—Working turbine blades or nozzles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23H—WORKING OF METAL BY THE ACTION OF A HIGH CONCENTRATION OF ELECTRIC CURRENT ON A WORKPIECE USING AN ELECTRODE WHICH TAKES THE PLACE OF A TOOL; SUCH WORKING COMBINED WITH OTHER FORMS OF WORKING OF METAL
- B23H1/00—Electrical discharge machining, i.e. removing metal with a series of rapidly recurring electrical discharges between an electrode and a workpiece in the presence of a fluid dielectric
- B23H1/04—Electrodes specially adapted therefor or their manufacture
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
- B23K35/02—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape
- B23K35/0211—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape for use in cutting
- B23K35/0216—Rods, electrodes, wires
-
- 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
- F05D2230/00—Manufacture
- F05D2230/10—Manufacture by removing material
- F05D2230/12—Manufacture by removing material by spark erosion methods
-
- 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
- F05D2230/10—Manufacture by removing material
- F05D2230/13—Manufacture by removing material using lasers
-
- 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
-
- 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
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Manufacturing & Machinery (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0507924 | 2005-07-26 | ||
| FR0507924A FR2889089B1 (fr) | 2005-07-26 | 2005-07-26 | Canal de refroidissement menage dans une paroi |
| FR0650103 | 2006-01-12 | ||
| FR0650103A FR2895691A1 (fr) | 2006-01-12 | 2006-01-12 | Element de paroi dans lequel est menage un canal de refroidissement |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CA2553860A1 CA2553860A1 (fr) | 2007-01-26 |
| CA2553860C true CA2553860C (fr) | 2016-01-26 |
Family
ID=37682465
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA2553860A Active CA2553860C (fr) | 2005-07-26 | 2006-07-25 | Canal de refroidissement menage dans une paroi |
Country Status (3)
| Country | Link |
|---|---|
| US (3) | US7950902B2 (enExample) |
| JP (1) | JP4931507B2 (enExample) |
| CA (1) | CA2553860C (enExample) |
Families Citing this family (31)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP3046283B2 (ja) | 1998-10-19 | 2000-05-29 | キヤノン株式会社 | インクジェット用ヘッドの組立装置及び組立方法及びインクジェット用ヘッド |
| FR2926481B1 (fr) * | 2008-01-23 | 2011-09-23 | Snecma | Canal de refroidissement menage dans une paroi |
| JP4898731B2 (ja) * | 2008-03-26 | 2012-03-21 | 三菱重工業株式会社 | ガスタービン冷却構造およびこれを備えたガスタービン |
| DE102009007164A1 (de) * | 2009-02-03 | 2010-08-12 | Rolls-Royce Deutschland Ltd & Co Kg | Verfahren zum Ausbilden einer Kühlluftöffnung in einer Wand einer Gasturbinenbrennkammer sowie nach dem Verfahren hergestellte Brennkammerwand |
| US8168912B1 (en) * | 2009-02-19 | 2012-05-01 | Florida Turbine Technologies, Inc. | Electrode for shaped film cooling hole |
| US20120164376A1 (en) * | 2010-12-23 | 2012-06-28 | General Electric Company | Method of modifying a substrate for passage hole formation therein, and related articles |
| US20120295061A1 (en) * | 2011-05-18 | 2012-11-22 | General Electric Company | Components with precision surface channels and hybrid machining method |
| US8915713B2 (en) * | 2011-09-27 | 2014-12-23 | General Electric Company | Offset counterbore for airfoil cooling hole |
| US9090343B2 (en) * | 2011-10-13 | 2015-07-28 | Sikorsky Aircraft Corporation | Rotor blade component cooling |
| US20130209232A1 (en) | 2012-02-15 | 2013-08-15 | Jinquan Xu | Multi-lobed cooling holes in gas turbine engine components having thermal barrier coatings |
| JP2013167205A (ja) * | 2012-02-15 | 2013-08-29 | Hitachi Ltd | ガスタービン翼、その放電加工用工具及び加工方法 |
| JP2015520322A (ja) | 2012-06-13 | 2015-07-16 | ゼネラル・エレクトリック・カンパニイ | ガスタービンエンジンの壁 |
| US9617859B2 (en) * | 2012-10-05 | 2017-04-11 | General Electric Company | Turbine components with passive cooling pathways |
| US9415468B2 (en) * | 2013-08-20 | 2016-08-16 | General Electric Company | Method for manufacturing an airfoil |
| ITCO20130051A1 (it) | 2013-10-23 | 2015-04-24 | Nuovo Pignone Srl | Metodo per la produzione di uno stadio di una turbina a vapore |
| US9662743B2 (en) | 2014-01-27 | 2017-05-30 | General Electric Company | Method for drilling a hole in an airfoil |
| US9468991B2 (en) | 2014-01-27 | 2016-10-18 | General Electric Company | Method determining hole completion |
| GB201419327D0 (en) | 2014-10-30 | 2014-12-17 | Rolls Royce Plc | A cooled component |
| WO2016074135A1 (zh) | 2014-11-10 | 2016-05-19 | 西门子公司 | 利用激光在工件上加工冷却孔的方法和装置 |
| EP3043023B1 (en) * | 2015-01-06 | 2019-09-18 | Ansaldo Energia IP UK Limited | Method for producing contoured cooling holes |
| CN104668675B (zh) * | 2015-03-05 | 2017-01-04 | 华南理工大学 | 一种具有微锥塔阵列端面的电极及其加工方法与应用 |
| CN105171158B (zh) * | 2015-10-10 | 2017-11-14 | 贵阳中航动力精密铸造有限公司 | 一种涡轮导向叶片锥形气膜孔加工工艺 |
| EP3179040B1 (en) | 2015-11-20 | 2021-07-14 | Raytheon Technologies Corporation | Component for a gas turbine engine and corresponding a method of manufacturing a film-cooled article |
| CN106529069B (zh) * | 2016-11-24 | 2019-06-11 | 中国航发沈阳黎明航空发动机有限责任公司 | 一种过弯叶片锻件叶身余量设计方法 |
| US11041389B2 (en) | 2017-05-31 | 2021-06-22 | General Electric Company | Adaptive cover for cooling pathway by additive manufacture |
| US10704399B2 (en) | 2017-05-31 | 2020-07-07 | General Electric Company | Adaptively opening cooling pathway |
| US10927680B2 (en) | 2017-05-31 | 2021-02-23 | General Electric Company | Adaptive cover for cooling pathway by additive manufacture |
| US10760430B2 (en) | 2017-05-31 | 2020-09-01 | General Electric Company | Adaptively opening backup cooling pathway |
| EP3981954B1 (en) * | 2019-06-07 | 2024-05-01 | IHI Corporation | Film cooling structure and turbine blade for gas turbine engine |
| US11220917B1 (en) | 2020-09-03 | 2022-01-11 | Raytheon Technologies Corporation | Diffused cooling arrangement for gas turbine engine components |
| CN113182625B (zh) * | 2021-05-07 | 2022-05-20 | 江苏江航智飞机发动机部件研究院有限公司 | 一种多齿涡轮叶片精密电解加工工艺 |
Family Cites Families (30)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4197443A (en) | 1977-09-19 | 1980-04-08 | General Electric Company | Method and apparatus for forming diffused cooling holes in an airfoil |
| US4684323A (en) * | 1985-12-23 | 1987-08-04 | United Technologies Corporation | Film cooling passages with curved corners |
| US4650949A (en) * | 1985-12-23 | 1987-03-17 | United Technologies Corporation | Electrode for electrical discharge machining film cooling passages in an airfoil |
| US4653983A (en) | 1985-12-23 | 1987-03-31 | United Technologies Corporation | Cross-flow film cooling passages |
| US4664597A (en) | 1985-12-23 | 1987-05-12 | United Technologies Corporation | Coolant passages with full coverage film cooling slot |
| US4672727A (en) | 1985-12-23 | 1987-06-16 | United Technologies Corporation | Method of fabricating film cooling slot in a hollow airfoil |
| US4738588A (en) | 1985-12-23 | 1988-04-19 | Field Robert E | Film cooling passages with step diffuser |
| US4762464A (en) | 1986-11-13 | 1988-08-09 | Chromalloy Gas Turbine Corporation | Airfoil with diffused cooling holes and method and apparatus for making the same |
| US4819325A (en) | 1987-06-01 | 1989-04-11 | Technical Manufacturing Systems, Inc. | Method of forming electro-discharge machining electrode |
| US4803339A (en) * | 1987-09-16 | 1989-02-07 | Rockwell International Corporation | Hollow electrode and arc initiation method |
| GB2227965B (en) * | 1988-10-12 | 1993-02-10 | Rolls Royce Plc | Apparatus for drilling a shaped hole in a workpiece |
| US5368441A (en) | 1992-11-24 | 1994-11-29 | United Technologies Corporation | Turbine airfoil including diffusing trailing edge pedestals |
| US5683600A (en) * | 1993-03-17 | 1997-11-04 | General Electric Company | Gas turbine engine component with compound cooling holes and method for making the same |
| SE509984C2 (sv) * | 1994-03-18 | 1999-03-29 | Sandvik Ab | Chargeringssystem för CVD |
| US5609779A (en) * | 1996-05-15 | 1997-03-11 | General Electric Company | Laser drilling of non-circular apertures |
| US6287075B1 (en) * | 1997-10-22 | 2001-09-11 | General Electric Company | Spanwise fan diffusion hole airfoil |
| EP0945593B1 (de) * | 1998-03-23 | 2003-05-07 | ALSTOM (Switzerland) Ltd | Filmkühlungsbohrung |
| DE59802893D1 (de) * | 1998-03-23 | 2002-03-14 | Alstom | Nichtkreisförmige Kühlbohrung und Verfahren zur Herstellung derselben |
| JP2000141069A (ja) * | 1998-11-10 | 2000-05-23 | Toshiba Corp | タービン翼およびその冷却孔加工方法 |
| US6206638B1 (en) | 1999-02-12 | 2001-03-27 | General Electric Company | Low cost airfoil cooling circuit with sidewall impingement cooling chambers |
| DE19960797C1 (de) * | 1999-12-16 | 2001-09-13 | Mtu Aero Engines Gmbh | Verfahren zum Herstellen einer Öffnung in einem metallischen Bauteil |
| US6368060B1 (en) * | 2000-05-23 | 2002-04-09 | General Electric Company | Shaped cooling hole for an airfoil |
| US6573474B1 (en) * | 2000-10-18 | 2003-06-03 | Chromalloy Gas Turbine Corporation | Process for drilling holes through a thermal barrier coating |
| FR2820066B1 (fr) | 2001-02-01 | 2003-03-07 | Snecma Moteurs | Dispositif de centrage et de percage de formes et de trous cylindriques |
| US6554572B2 (en) | 2001-05-17 | 2003-04-29 | General Electric Company | Gas turbine engine blade |
| GB2395157B (en) * | 2002-11-15 | 2005-09-07 | Rolls Royce Plc | Laser driliing shaped holes |
| US6994514B2 (en) * | 2002-11-20 | 2006-02-07 | Mitsubishi Heavy Industries, Ltd. | Turbine blade and gas turbine |
| US7041933B2 (en) * | 2003-04-14 | 2006-05-09 | Meyer Tool, Inc. | Complex hole shaping |
| US6897401B2 (en) * | 2003-07-31 | 2005-05-24 | United Technologies Corporation | Non-separating diffuser for holes produced by a two step process |
| US7008186B2 (en) * | 2003-09-17 | 2006-03-07 | General Electric Company | Teardrop film cooled blade |
-
2006
- 2006-07-24 JP JP2006200296A patent/JP4931507B2/ja active Active
- 2006-07-25 CA CA2553860A patent/CA2553860C/fr active Active
- 2006-07-25 US US11/492,110 patent/US7950902B2/en active Active
-
2010
- 2010-05-26 US US12/787,477 patent/US8875393B2/en active Active
-
2014
- 2014-08-18 US US14/462,059 patent/US9114469B2/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| US20100229388A1 (en) | 2010-09-16 |
| CA2553860A1 (fr) | 2007-01-26 |
| US20070025852A1 (en) | 2007-02-01 |
| US7950902B2 (en) | 2011-05-31 |
| JP4931507B2 (ja) | 2012-05-16 |
| US9114469B2 (en) | 2015-08-25 |
| US20140353284A1 (en) | 2014-12-04 |
| JP2007032567A (ja) | 2007-02-08 |
| US8875393B2 (en) | 2014-11-04 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| EEER | Examination request |