AU2002236432A1 - Laser machining cooling holes in gas turbine components - Google Patents
Laser machining cooling holes in gas turbine componentsInfo
- Publication number
- AU2002236432A1 AU2002236432A1 AU2002236432A AU3643202A AU2002236432A1 AU 2002236432 A1 AU2002236432 A1 AU 2002236432A1 AU 2002236432 A AU2002236432 A AU 2002236432A AU 3643202 A AU3643202 A AU 3643202A AU 2002236432 A1 AU2002236432 A1 AU 2002236432A1
- Authority
- AU
- Australia
- Prior art keywords
- gas turbine
- cooling holes
- laser machining
- turbine components
- machining cooling
- 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.)
- Abandoned
Links
Classifications
-
- 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
- B23K26/00—Working by laser beam, e.g. welding, cutting or boring
- B23K26/36—Removing material
- B23K26/40—Removing material taking account of the properties of the material involved
-
- 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
- B23K26/00—Working by laser beam, e.g. welding, cutting or boring
- B23K26/02—Positioning or observing the workpiece, e.g. with respect to the point of impact; Aligning, aiming or focusing the laser beam
- B23K26/06—Shaping the laser beam, e.g. by masks or multi-focusing
- B23K26/062—Shaping the laser beam, e.g. by masks or multi-focusing by direct control of the laser beam
- B23K26/0622—Shaping the laser beam, e.g. by masks or multi-focusing by direct control of the laser beam by shaping pulses
-
- 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
- B23K26/00—Working by laser beam, e.g. welding, cutting or boring
- B23K26/36—Removing material
- B23K26/38—Removing material by boring or cutting
- B23K26/382—Removing material by boring or cutting by boring
- B23K26/384—Removing material by boring or cutting by boring of specially shaped holes
-
- 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
- B23K26/00—Working by laser beam, e.g. welding, cutting or boring
- B23K26/36—Removing material
- B23K26/38—Removing material by boring or cutting
- B23K26/382—Removing material by boring or cutting by boring
- B23K26/389—Removing material by boring or cutting by boring of fluid openings, e.g. nozzles, jets
-
- 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
- B23K2101/00—Articles made by soldering, welding or cutting
- B23K2101/001—Turbines
-
- 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
- B23P2700/00—Indexing scheme relating to the articles being treated, e.g. manufactured, repaired, assembled, connected or other operations covered in the subgroups
- B23P2700/06—Cooling passages of turbine components, e.g. unblocking or preventing blocking of cooling passages of turbine components
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2260/00—Function
- F05B2260/20—Heat transfer, e.g. cooling
- F05B2260/202—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
Landscapes
- Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Engineering & Computer Science (AREA)
- Plasma & Fusion (AREA)
- Mechanical Engineering (AREA)
- Laser Beam Processing (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/741,727 US6420677B1 (en) | 2000-12-20 | 2000-12-20 | Laser machining cooling holes in gas turbine components |
US09741727 | 2000-12-20 | ||
PCT/US2001/028370 WO2002049795A1 (en) | 2000-12-20 | 2001-09-11 | Laser machining cooling holes in gas turbine components |
Publications (1)
Publication Number | Publication Date |
---|---|
AU2002236432A1 true AU2002236432A1 (en) | 2002-07-01 |
Family
ID=24981917
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AU2002236432A Abandoned AU2002236432A1 (en) | 2000-12-20 | 2001-09-11 | Laser machining cooling holes in gas turbine components |
Country Status (6)
Country | Link |
---|---|
US (1) | US6420677B1 (de) |
EP (1) | EP1349695B1 (de) |
JP (1) | JP2004532738A (de) |
AU (1) | AU2002236432A1 (de) |
CA (1) | CA2436912C (de) |
WO (1) | WO2002049795A1 (de) |
Families Citing this family (59)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP4508432B2 (ja) * | 2001-01-09 | 2010-07-21 | 三菱重工業株式会社 | ガスタービンの冷却構造 |
GB2381489B (en) * | 2001-10-30 | 2004-11-17 | Rolls Royce Plc | Method of forming a shaped hole |
US7411150B2 (en) * | 2002-06-12 | 2008-08-12 | Alstom Technology Ltd. | Method of producing a composite component |
GB2395157B (en) * | 2002-11-15 | 2005-09-07 | Rolls Royce Plc | Laser driliing shaped holes |
US6847004B2 (en) * | 2003-01-10 | 2005-01-25 | General Electric Company | Process of removing a ceramic coating deposit in a surface hole of a component |
US7041933B2 (en) * | 2003-04-14 | 2006-05-09 | Meyer Tool, Inc. | Complex hole shaping |
US6723951B1 (en) | 2003-06-04 | 2004-04-20 | Siemens Westinghouse Power Corporation | Method for reestablishing holes in a component |
DE50313280D1 (de) * | 2003-10-06 | 2011-01-05 | Siemens Ag | Verfahren zur Herstellung eines Lochs |
EP1681128A1 (de) * | 2005-01-14 | 2006-07-19 | Siemens Aktiengesellschaft | Verfahren zur Herstellung eines Lochs und Vorrichtung |
US7883320B2 (en) * | 2005-01-24 | 2011-02-08 | United Technologies Corporation | Article having diffuser holes and method of making same |
EP1806203A1 (de) * | 2006-01-10 | 2007-07-11 | Siemens Aktiengesellschaft | Verfahren zur Herstellung eines Lochs |
US7766606B2 (en) * | 2006-08-17 | 2010-08-03 | Siemens Energy, Inc. | Turbine airfoil cooling system with platform cooling channels with diffusion slots |
FR2909297B1 (fr) * | 2006-11-30 | 2010-03-05 | Snecma | Procede de percage laser d'une piece en materiau composite a matrice ceramique, trou obtenu par ce procede, piece en materiau composite a matrice ceramique le comportant, turboreacteur comportant une telle piece. |
US8007237B2 (en) | 2006-12-29 | 2011-08-30 | Pratt & Whitney Canada Corp. | Cooled airfoil component |
US7812282B2 (en) * | 2007-03-15 | 2010-10-12 | Honeywell International Inc. | Methods of forming fan-shaped effusion holes in combustors |
JP5249520B2 (ja) * | 2007-03-28 | 2013-07-31 | 本田技研工業株式会社 | 噴口のレーザ加工装置及びレーザ加工方法 |
US7992272B2 (en) | 2007-05-29 | 2011-08-09 | Metem Corporation | Method and apparatus for milling thermal barrier coated metals |
US20090057282A1 (en) * | 2007-08-15 | 2009-03-05 | Chunfu Huang | Laser machining method utilizing variable inclination angle |
US7820267B2 (en) * | 2007-08-20 | 2010-10-26 | Honeywell International Inc. | Percussion drilled shaped through hole and method of forming |
GB2452303B (en) * | 2007-08-31 | 2009-10-14 | Rolls Royce Plc | Method for cutting with a laser |
US20090169394A1 (en) * | 2007-12-28 | 2009-07-02 | General Electric Company | Method of forming cooling holes and turbine airfoil with hybrid-formed cooling holes |
EP2105240B1 (de) | 2008-03-28 | 2011-10-05 | Siemens Aktiengesellschaft | Verfahren zur Fertigung einer Bohrung |
US8371814B2 (en) * | 2009-06-24 | 2013-02-12 | Honeywell International Inc. | Turbine engine components |
EP2467228B1 (de) * | 2009-08-17 | 2016-07-27 | Siemens Aktiengesellschaft | Verfahren zur herstellung eines asymmetrischen diffusors unter verwendung verschiedener laserstellungen |
EP2292372B1 (de) * | 2009-08-17 | 2012-10-03 | Siemens Aktiengesellschaft | Verfahren zur Herstellung eines Lochs unter Verwendung verschiedener Laserstellungen |
US8529193B2 (en) * | 2009-11-25 | 2013-09-10 | Honeywell International Inc. | Gas turbine engine components with improved film cooling |
US9890647B2 (en) * | 2009-12-29 | 2018-02-13 | Rolls-Royce North American Technologies Inc. | Composite gas turbine engine component |
US8857055B2 (en) | 2010-01-29 | 2014-10-14 | General Electric Company | Process and system for forming shaped air holes |
US8628293B2 (en) | 2010-06-17 | 2014-01-14 | Honeywell International Inc. | Gas turbine engine components with cooling hole trenches |
US9696035B2 (en) * | 2010-10-29 | 2017-07-04 | General Electric Company | Method of forming a cooling hole by laser drilling |
US9434025B2 (en) | 2011-07-19 | 2016-09-06 | Pratt & Whitney Canada Corp. | Laser drilling methods of shallow-angled holes |
US8631557B2 (en) | 2011-07-19 | 2014-01-21 | Pratt & Whitney Canada Corp. | Laser drilling methods of shallow-angled holes |
US20130020291A1 (en) * | 2011-07-19 | 2013-01-24 | Pratt & Whitney Canada Corp. | Laser drilling methods of shallow-angled holes |
US8624151B2 (en) | 2011-07-19 | 2014-01-07 | Pratt & Whitney Canada Corp. | Laser drilling methods of shallow-angled holes |
US8858175B2 (en) * | 2011-11-09 | 2014-10-14 | General Electric Company | Film hole trench |
JP6212051B2 (ja) * | 2011-12-20 | 2017-10-11 | アイピージー フォトニクス コーポレーション | 高出力ファイバーレーザー流出孔穿孔装置、および高出力ファイバーレーザー流出孔穿孔装置を使用する方法 |
US9650900B2 (en) | 2012-05-07 | 2017-05-16 | Honeywell International Inc. | Gas turbine engine components with film cooling holes having cylindrical to multi-lobe configurations |
US10113433B2 (en) | 2012-10-04 | 2018-10-30 | Honeywell International Inc. | Gas turbine engine components with lateral and forward sweep film cooling holes |
CN103008892B (zh) * | 2012-12-12 | 2015-06-10 | 中科中涵激光设备(福建)股份有限公司 | 一种激光加工异型孔的方法 |
CN104096974A (zh) * | 2013-04-08 | 2014-10-15 | 昆山允升吉光电科技有限公司 | 一种激光切割设备 |
JP5908009B2 (ja) * | 2013-08-20 | 2016-04-26 | 三菱重工業株式会社 | レーザ加工方法及びレーザ加工装置 |
WO2015108858A1 (en) * | 2014-01-16 | 2015-07-23 | United Technologies Corporation | Systems and methods for thermal location of cooling holes |
US9662743B2 (en) * | 2014-01-27 | 2017-05-30 | General Electric Company | Method for drilling a hole in an airfoil |
US9931814B2 (en) | 2014-09-25 | 2018-04-03 | General Electric Company | Article and method for making an article |
US9931695B2 (en) | 2014-09-25 | 2018-04-03 | General Electric Company | Article and method for making an article |
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 |
WO2016105327A1 (en) | 2014-12-22 | 2016-06-30 | Siemens Aktiengesellschaft | Method for controlling coating delamination caused when forming cooling holes through thermal barrier coatings |
US9757936B2 (en) | 2014-12-29 | 2017-09-12 | General Electric Company | Hot gas path component |
US20160298462A1 (en) * | 2015-04-09 | 2016-10-13 | United Technologies Corporation | Cooling passages for a gas turbine engine component |
US11021965B2 (en) | 2016-05-19 | 2021-06-01 | Honeywell International Inc. | Engine components with cooling holes having tailored metering and diffuser portions |
US10232469B2 (en) * | 2016-09-30 | 2019-03-19 | Caterpillar Inc. | System and method for manufacturing component |
CN109175732A (zh) * | 2018-09-18 | 2019-01-11 | 中国航空制造技术研究院 | 异型孔加工方法及异型孔 |
US11898465B2 (en) | 2021-08-13 | 2024-02-13 | Rtx Corporation | Forming lined cooling aperture(s) in a turbine engine component |
US11673200B2 (en) | 2021-08-13 | 2023-06-13 | Raytheon Technologies Corporation | Forming cooling aperture(s) using electrical discharge machining |
US11732590B2 (en) | 2021-08-13 | 2023-08-22 | Raytheon Technologies Corporation | Transition section for accommodating mismatch between other sections of a cooling aperture in a turbine engine component |
US11913119B2 (en) | 2021-08-13 | 2024-02-27 | Rtx Corporation | Forming cooling aperture(s) in a turbine engine component |
US11813706B2 (en) | 2021-08-13 | 2023-11-14 | Rtx Corporation | Methods for forming cooling apertures in a turbine engine component |
US11542831B1 (en) | 2021-08-13 | 2023-01-03 | Raytheon Technologies Corporation | Energy beam positioning during formation of a cooling aperture |
US11603769B2 (en) | 2021-08-13 | 2023-03-14 | Raytheon Technologies Corporation | Forming lined cooling aperture(s) in a turbine engine component |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5739502A (en) | 1983-12-27 | 1998-04-14 | General Electric Company | Laser intensity redistribution |
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 |
US4737613A (en) | 1987-08-24 | 1988-04-12 | United Technologies Corporation | Laser machining method |
GB2227965B (en) | 1988-10-12 | 1993-02-10 | Rolls Royce Plc | Apparatus for drilling a shaped hole in a workpiece |
US5223692A (en) * | 1991-09-23 | 1993-06-29 | General Electric Company | Method and apparatus for laser trepanning |
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 |
US5418345A (en) | 1994-02-28 | 1995-05-23 | United Technologies Corporation | Method for forming shaped passages |
US5609779A (en) * | 1996-05-15 | 1997-03-11 | General Electric Company | Laser drilling of non-circular apertures |
US5837964A (en) * | 1998-01-16 | 1998-11-17 | Chromalloy Gas Turbine Corporation | Laser drilling holes in components by combined percussion and trepan drilling |
EP0950463B1 (de) * | 1998-03-23 | 2002-01-23 | Alstom | Nichtkreisförmige Kühlbohrung und Verfahren zur Herstellung derselben |
-
2000
- 2000-12-20 US US09/741,727 patent/US6420677B1/en not_active Expired - Lifetime
-
2001
- 2001-09-11 WO PCT/US2001/028370 patent/WO2002049795A1/en active Application Filing
- 2001-09-11 EP EP01985954.5A patent/EP1349695B1/de not_active Expired - Lifetime
- 2001-09-11 JP JP2002551122A patent/JP2004532738A/ja active Pending
- 2001-09-11 AU AU2002236432A patent/AU2002236432A1/en not_active Abandoned
- 2001-09-11 CA CA002436912A patent/CA2436912C/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
EP1349695B1 (de) | 2014-04-09 |
CA2436912A1 (en) | 2002-06-27 |
EP1349695A4 (de) | 2009-08-12 |
WO2002049795A1 (en) | 2002-06-27 |
US6420677B1 (en) | 2002-07-16 |
JP2004532738A (ja) | 2004-10-28 |
CA2436912C (en) | 2007-05-15 |
EP1349695A1 (de) | 2003-10-08 |
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