JP3719466B2 - 非円形開口のレーザー加工 - Google Patents
非円形開口のレーザー加工 Download PDFInfo
- Publication number
- JP3719466B2 JP3719466B2 JP12273197A JP12273197A JP3719466B2 JP 3719466 B2 JP3719466 B2 JP 3719466B2 JP 12273197 A JP12273197 A JP 12273197A JP 12273197 A JP12273197 A JP 12273197A JP 3719466 B2 JP3719466 B2 JP 3719466B2
- Authority
- JP
- Japan
- Prior art keywords
- diffuser
- laser
- laser beam
- metal
- wall
- 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 - Fee Related
Links
- 238000003754 machining Methods 0.000 title claims description 11
- 238000001816 cooling Methods 0.000 claims description 29
- 239000002184 metal Substances 0.000 claims description 29
- 238000000034 method Methods 0.000 claims description 22
- 230000001154 acute effect Effects 0.000 claims description 11
- 230000007423 decrease Effects 0.000 claims description 5
- 238000012545 processing Methods 0.000 claims description 5
- 239000007789 gas Substances 0.000 description 10
- 238000005553 drilling Methods 0.000 description 8
- 230000015572 biosynthetic process Effects 0.000 description 6
- 238000004519 manufacturing process Methods 0.000 description 6
- 239000000567 combustion gas Substances 0.000 description 4
- 238000002485 combustion reaction Methods 0.000 description 3
- 238000009760 electrical discharge machining Methods 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 238000007796 conventional method Methods 0.000 description 2
- 238000001704 evaporation Methods 0.000 description 2
- 239000012530 fluid Substances 0.000 description 2
- 238000004891 communication Methods 0.000 description 1
- 239000012141 concentrate Substances 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 230000001678 irradiating effect Effects 0.000 description 1
- 238000003698 laser cutting Methods 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
Images
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
- B23K26/02—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
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 (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US08/648472 | 1996-05-15 | ||
| US08/648,472 US5609779A (en) | 1996-05-15 | 1996-05-15 | Laser drilling of non-circular apertures |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JPH1085977A JPH1085977A (ja) | 1998-04-07 |
| JPH1085977A5 JPH1085977A5 (enExample) | 2005-03-17 |
| JP3719466B2 true JP3719466B2 (ja) | 2005-11-24 |
Family
ID=24600924
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP12273197A Expired - Fee Related JP3719466B2 (ja) | 1996-05-15 | 1997-05-14 | 非円形開口のレーザー加工 |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US5609779A (enExample) |
| EP (1) | EP0807485B1 (enExample) |
| JP (1) | JP3719466B2 (enExample) |
| DE (1) | DE69708744T2 (enExample) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9278408B2 (en) | 2013-02-27 | 2016-03-08 | Honda Motor Co., Ltd. | Laser machining apparatus |
| US10060265B2 (en) | 2011-12-15 | 2018-08-28 | Ihi Corporation | Turbine blade |
Families Citing this family (101)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6624382B2 (en) * | 1997-01-30 | 2003-09-23 | Anvik Corporation | Configured-hole high-speed drilling system for micro-via pattern formation, and resulting structure |
| US5881445A (en) * | 1997-07-30 | 1999-03-16 | Mauro; George | Method of producing micro-apertures in optically flat surfaces and structures when made by the method |
| 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 |
| DE19960797C1 (de) | 1999-12-16 | 2001-09-13 | Mtu Aero Engines Gmbh | Verfahren zum Herstellen einer Öffnung in einem metallischen Bauteil |
| US6501045B1 (en) | 2000-04-06 | 2002-12-31 | Resonetics, Inc. | Method and apparatus for controlling the taper angle of the walls of laser machined features |
| US6573474B1 (en) * | 2000-10-18 | 2003-06-03 | Chromalloy Gas Turbine Corporation | Process for drilling holes through a thermal barrier coating |
| US6420677B1 (en) | 2000-12-20 | 2002-07-16 | Chromalloy Gas Turbine Corporation | Laser machining cooling holes in gas turbine components |
| GB0112234D0 (en) * | 2001-05-18 | 2001-07-11 | Welding Inst | Surface modification |
| JP2004537175A (ja) * | 2001-08-02 | 2004-12-09 | エスケーシー カンパニー,リミテッド | レーザーを使用した化学的機械的研磨パッドの製造方法 |
| GB2381489B (en) * | 2001-10-30 | 2004-11-17 | Rolls Royce Plc | Method of forming a shaped hole |
| EP1317995A1 (de) * | 2001-12-05 | 2003-06-11 | Siemens Aktiengesellschaft | Verfahren und Vorrichtung zur Glättung der Oberfläche einer Gasturbinenschaufel |
| US6612811B2 (en) * | 2001-12-12 | 2003-09-02 | General Electric Company | Airfoil for a turbine nozzle of a gas turbine engine and method of making same |
| GB2389554A (en) * | 2002-06-12 | 2003-12-17 | Alstom | Machining apparatus and a method for machining |
| 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 |
| US6988872B2 (en) | 2003-01-27 | 2006-01-24 | Mitsubishi Heavy Industries, Ltd. | Turbine moving blade and gas turbine |
| GB2389330B (en) * | 2003-03-31 | 2004-05-05 | M J Technologies Ltd | Machining of cooling air holes in gas turbine components |
| DE10335657B4 (de) * | 2003-08-04 | 2015-04-30 | Alstom Technology Ltd. | Parametrische Herstellung von Kühlbohrungen |
| US8491353B2 (en) * | 2003-09-30 | 2013-07-23 | Panasonic Corporation | Mold for optical components |
| EP1529580B1 (de) * | 2003-10-29 | 2009-01-07 | Siemens Aktiengesellschaft | Gussform |
| US7374401B2 (en) * | 2005-03-01 | 2008-05-20 | General Electric Company | Bell-shaped fan cooling holes for turbine airfoil |
| US7784183B2 (en) * | 2005-06-09 | 2010-08-31 | General Electric Company | System and method for adjusting performance of manufacturing operations or steps |
| JP4931507B2 (ja) * | 2005-07-26 | 2012-05-16 | スネクマ | 壁内に形成された冷却流路 |
| FR2895691A1 (fr) * | 2006-01-12 | 2007-07-06 | Snecma Sa | Element de paroi dans lequel est menage un canal de refroidissement |
| WO2007052337A1 (ja) * | 2005-11-01 | 2007-05-10 | Ihi Corporation | タービン部品 |
| CA2580102A1 (en) * | 2006-03-06 | 2007-09-06 | General Electric Company | System and method for monitoring drilling process parameters and controlling drilling operation |
| US20070296967A1 (en) * | 2006-06-27 | 2007-12-27 | Bhupendra Kumra Gupta | Analysis of component for presence, composition and/or thickness of coating |
| US20080003096A1 (en) * | 2006-06-29 | 2008-01-03 | United Technologies Corporation | High coverage cooling hole shape |
| US8084706B2 (en) * | 2006-07-20 | 2011-12-27 | Gsi Group Corporation | System and method for laser processing at non-constant velocities |
| EP1892375A1 (en) * | 2006-08-23 | 2008-02-27 | Siemens Aktiengesellschaft | Turbine engine rotor disc with cooling passage |
| EP1898051B8 (en) * | 2006-08-25 | 2017-08-02 | Ansaldo Energia IP UK Limited | Gas turbine airfoil with leading edge cooling |
| US7812282B2 (en) * | 2007-03-15 | 2010-10-12 | Honeywell International Inc. | Methods of forming fan-shaped effusion holes in combustors |
| US7820267B2 (en) * | 2007-08-20 | 2010-10-26 | Honeywell International Inc. | Percussion drilled shaped through hole and method of forming |
| US20090169394A1 (en) * | 2007-12-28 | 2009-07-02 | General Electric Company | Method of forming cooling holes and turbine airfoil with hybrid-formed cooling holes |
| FR2926481B1 (fr) * | 2008-01-23 | 2011-09-23 | Snecma | Canal de refroidissement menage dans une paroi |
| US8246306B2 (en) * | 2008-04-03 | 2012-08-21 | General Electric Company | Airfoil for nozzle and a method of forming the machined contoured passage therein |
| US8057181B1 (en) | 2008-11-07 | 2011-11-15 | Florida Turbine Technologies, Inc. | Multiple expansion film cooling hole for turbine airfoil |
| US8371814B2 (en) * | 2009-06-24 | 2013-02-12 | Honeywell International Inc. | Turbine engine components |
| GB0912796D0 (en) * | 2009-07-23 | 2009-08-26 | Cummins Turbo Tech Ltd | Compressor,turbine and turbocharger |
| US8292583B2 (en) * | 2009-08-13 | 2012-10-23 | Siemens Energy, Inc. | Turbine blade having a constant thickness airfoil skin |
| US8529193B2 (en) * | 2009-11-25 | 2013-09-10 | Honeywell International Inc. | Gas turbine engine components with improved film cooling |
| US8857055B2 (en) * | 2010-01-29 | 2014-10-14 | General Electric Company | Process and system for forming shaped air holes |
| US8905713B2 (en) | 2010-05-28 | 2014-12-09 | General Electric Company | Articles which include chevron film cooling holes, and related processes |
| US8628293B2 (en) * | 2010-06-17 | 2014-01-14 | Honeywell International Inc. | Gas turbine engine components with cooling hole trenches |
| US20120102959A1 (en) * | 2010-10-29 | 2012-05-03 | John Howard Starkweather | Substrate with shaped cooling holes and methods of manufacture |
| US9696035B2 (en) | 2010-10-29 | 2017-07-04 | General Electric Company | Method of forming a cooling hole by laser drilling |
| US9157328B2 (en) | 2010-12-24 | 2015-10-13 | Rolls-Royce North American Technologies, Inc. | Cooled gas turbine engine component |
| JP5632812B2 (ja) * | 2011-10-03 | 2014-11-26 | 三菱日立パワーシステムズ株式会社 | ガスタービン翼 |
| 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 |
| US9279330B2 (en) | 2012-02-15 | 2016-03-08 | United Technologies Corporation | Gas turbine engine component with converging/diverging cooling passage |
| US9482100B2 (en) | 2012-02-15 | 2016-11-01 | United Technologies Corporation | Multi-lobed cooling hole |
| US10422230B2 (en) | 2012-02-15 | 2019-09-24 | United Technologies Corporation | Cooling hole with curved metering section |
| US8683813B2 (en) | 2012-02-15 | 2014-04-01 | United Technologies Corporation | Multi-lobed cooling hole and method of manufacture |
| US8683814B2 (en) | 2012-02-15 | 2014-04-01 | United Technologies Corporation | Gas turbine engine component with impingement and lobed cooling hole |
| US9024226B2 (en) | 2012-02-15 | 2015-05-05 | United Technologies Corporation | EDM method for multi-lobed cooling hole |
| US8850828B2 (en) | 2012-02-15 | 2014-10-07 | United Technologies Corporation | Cooling hole with curved metering section |
| US8572983B2 (en) | 2012-02-15 | 2013-11-05 | United Technologies Corporation | Gas turbine engine component with impingement and diffusive cooling |
| US8707713B2 (en) | 2012-02-15 | 2014-04-29 | United Technologies Corporation | Cooling hole with crenellation features |
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| US20150160644A1 (en) * | 2013-12-05 | 2015-06-11 | General Electric Company | Repair method, system for automatic locating and clearing and tool for automated locating and modifying |
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| EP3157694B1 (en) * | 2014-06-18 | 2020-07-29 | Mikro Systems Inc. | Turbine blade investment casting using film hole protrusions for integral wall thickness control |
| US10101030B2 (en) * | 2014-09-02 | 2018-10-16 | Honeywell International Inc. | Gas turbine engines with plug resistant effusion cooling holes |
| US20160090843A1 (en) * | 2014-09-30 | 2016-03-31 | General Electric Company | Turbine components with stepped apertures |
| US20160298462A1 (en) * | 2015-04-09 | 2016-10-13 | United Technologies Corporation | Cooling passages for a gas turbine engine component |
| CN105458530B (zh) * | 2016-01-29 | 2018-05-15 | 孙树峰 | 一种飞秒激光加工航空发动机叶片气膜孔的装置及方法 |
| CN105643117B (zh) * | 2016-04-06 | 2017-07-18 | 中国南方航空工业(集团)有限公司 | 用于异形管状壁面上打孔的激光打孔加工夹具及方法 |
| US11021965B2 (en) | 2016-05-19 | 2021-06-01 | Honeywell International Inc. | Engine components with cooling holes having tailored metering and diffuser portions |
| US10605091B2 (en) * | 2016-06-28 | 2020-03-31 | General Electric Company | Airfoil with cast features and method of manufacture |
| US10605092B2 (en) | 2016-07-11 | 2020-03-31 | United Technologies Corporation | Cooling hole with shaped meter |
| EP3354849A1 (en) * | 2017-01-31 | 2018-08-01 | Siemens Aktiengesellschaft | Wall of a hot gas part and corresponding hot gas part for a gas turbine |
| US10577954B2 (en) | 2017-03-27 | 2020-03-03 | Honeywell International Inc. | Blockage-resistant vane impingement tubes and turbine nozzles containing the same |
| US10503148B2 (en) * | 2017-03-29 | 2019-12-10 | General Electric Company | System and method for diffuser hole creation |
| US10539026B2 (en) | 2017-09-21 | 2020-01-21 | United Technologies Corporation | Gas turbine engine component with cooling holes having variable roughness |
| US11085641B2 (en) | 2018-11-27 | 2021-08-10 | Honeywell International Inc. | Plug resistant effusion holes for gas turbine engine |
| US11021963B2 (en) * | 2019-05-03 | 2021-06-01 | Raytheon Technologies Corporation | Monolithic body including an internal passage with a generally teardrop shaped cross-sectional geometry |
| CN110328453B (zh) * | 2019-07-16 | 2021-11-16 | 江苏塑光汽车部件有限公司 | 一种汽车圆形油箱盖生产用连续切割装置 |
| EP4108883A1 (en) * | 2021-06-24 | 2022-12-28 | Doosan Enerbility Co., Ltd. | Turbine blade and turbine |
| CN115026906B (zh) * | 2022-06-23 | 2023-04-18 | 深圳市阿尔斯自动化科技有限公司 | 一种高速五金模切机用模切机构 |
| CN115740789B (zh) * | 2022-11-15 | 2024-10-29 | 西安中科微精光子科技股份有限公司 | 一种在涡轮叶片中加工气膜孔的方法和系统 |
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1996
- 1996-05-15 US US08/648,472 patent/US5609779A/en not_active Expired - Lifetime
-
1997
- 1997-05-09 EP EP97303194A patent/EP0807485B1/en not_active Expired - Lifetime
- 1997-05-09 DE DE69708744T patent/DE69708744T2/de not_active Expired - Fee Related
- 1997-05-14 JP JP12273197A patent/JP3719466B2/ja not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10060265B2 (en) | 2011-12-15 | 2018-08-28 | Ihi Corporation | Turbine blade |
| US9278408B2 (en) | 2013-02-27 | 2016-03-08 | Honda Motor Co., Ltd. | Laser machining apparatus |
| US10155288B2 (en) | 2013-02-27 | 2018-12-18 | Honda Motor Co., Ltd. | Laser machining apparatus |
Also Published As
| Publication number | Publication date |
|---|---|
| DE69708744T2 (de) | 2002-08-29 |
| JPH1085977A (ja) | 1998-04-07 |
| EP0807485B1 (en) | 2001-12-05 |
| EP0807485A3 (en) | 1999-04-28 |
| DE69708744D1 (de) | 2002-01-17 |
| US5609779A (en) | 1997-03-11 |
| EP0807485A2 (en) | 1997-11-19 |
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