BR0200332A - Martelamento por choque a laser de arestas de palheta de rotor integralmente equipado com palhetas - Google Patents
Martelamento por choque a laser de arestas de palheta de rotor integralmente equipado com palhetasInfo
- Publication number
- BR0200332A BR0200332A BR0200332-5A BR0200332A BR0200332A BR 0200332 A BR0200332 A BR 0200332A BR 0200332 A BR0200332 A BR 0200332A BR 0200332 A BR0200332 A BR 0200332A
- Authority
- BR
- Brazil
- Prior art keywords
- laser
- vane
- rotor
- fully equipped
- laser beam
- Prior art date
Links
- 230000035939 shock Effects 0.000 title abstract 3
- 238000000034 method Methods 0.000 abstract 4
- 235000014676 Phragmites communis Nutrition 0.000 abstract 2
- 238000010304 firing Methods 0.000 abstract 2
- 230000003252 repetitive effect Effects 0.000 abstract 2
- 238000012790 confirmation Methods 0.000 abstract 1
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
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/286—Particular treatment of blades, e.g. to increase durability or resistance against corrosion or erosion
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D10/00—Modifying the physical properties by methods other than heat treatment or deformation
- C21D10/005—Modifying the physical properties by methods other than heat treatment or deformation by laser shock processing
-
- 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
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Materials Engineering (AREA)
- Thermal Sciences (AREA)
- Optics & Photonics (AREA)
- Crystallography & Structural Chemistry (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- General Engineering & Computer Science (AREA)
- Laser Beam Processing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
"MARTELAMENTO POR CHOQUE A LASER DE ARESTAS DE PALHETA DE ROTOR INTEGRALMENTE EQUIPADO COM PALHETAS". Processo para martelar por choque a laser arestas dianteira e traseira (LE, TE) de palheta de rotor (108) de discos e rotores de motor turbina a gás integralmente equipados com palhetas que não são bloqueados por outras fileiras de palhetas. O processo inclui disparar continuamente um feixe laser estacionário (102), cujos pulsos repetitivos entre períodos relativamente constantes, ao longo de no mínimo uma porção de arestas dianteira ou traseira (LE, TE) da palheta (108), com o feixe laser (102) projetado com um ângulo oblíquo (110) com relação a uma superfície da aresta de tal modo que pulsos laser formem pontos de laser de conformação elíptica (60) que se superpõem. Na configuração da invenção tomada como exemplo, os pontos de laser de confirmação elíptica (60) têm uma superposição de cerca de 50% e são da ordem de 11,7 mm por 4 mm em diâmetro. Um outro processo é para martelar por choque a laser arestas dianteira e traseira de palheta de rotor (LE, TE) de motor turbina a gás com rotores e discos integralmente equipados com palhetas que são bloqueados por outras fileiras de palhetas. O processo inclui disparar continuamente o feixe laser estacionário (102) que pulsa de maneira repetitiva entre períodos relativamente constantes, ao longo de no mínimo uma porção das arestas dianteira ou traseira (LE, TE) da palheta (108), com o feixe laser (102) inclinado de maneira composta de tal modo que ele seja projetado em um primeiro ângulo oblíquo (110) com relação a uma superfície da aresta e em um segundo ângulo oblíquo (114) com relação a um eixo ao redor do qual o rotor é circunscrito. Pulsos laser formam pontos de laser de conformação elíptica (60) que são inclinados a partir da aresta dianteira (LE) radialmente para dentro no sentido do eixo. Na configuração tomada como exemplo, os pontos de laser de conformação elíptica (60) têm uma superposição de cerca de 50%.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US09/771,856 US6541733B1 (en) | 2001-01-29 | 2001-01-29 | Laser shock peening integrally bladed rotor blade edges |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| BR0200332A true BR0200332A (pt) | 2002-10-29 |
| BR0200332B1 BR0200332B1 (pt) | 2012-01-24 |
Family
ID=25093154
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BRPI0200332-5A BR0200332B1 (pt) | 2001-01-29 | 2002-01-29 | processo para martelar por choque a laser arestas dianteira ou traseira de palhetas de motor de turbina a gás. |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US6541733B1 (pt) |
| EP (1) | EP1227164B1 (pt) |
| BR (1) | BR0200332B1 (pt) |
| CA (1) | CA2368288C (pt) |
| DE (1) | DE60233536D1 (pt) |
| SG (1) | SG109489A1 (pt) |
Families Citing this family (32)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6653755B2 (en) * | 2001-05-30 | 2003-11-25 | Intel Corporation | Radial air flow fan assembly having stator fins surrounding rotor blades |
| GB2398034B (en) * | 2003-02-04 | 2005-08-10 | Rolls Royce Plc | Laser shock peening |
| US7097720B2 (en) * | 2003-04-30 | 2006-08-29 | General Electric Company | Lower fluence boundary laser shock peening |
| US6713716B1 (en) | 2003-05-30 | 2004-03-30 | General Electric Company | Reduced mist laser shock peening |
| US6917012B2 (en) * | 2003-07-03 | 2005-07-12 | General Electric Company | Reducing electromagnetic feedback during laser shock peening |
| US6900409B2 (en) * | 2003-08-22 | 2005-05-31 | General Electric Company | Single head laser high throughput laser shock peening |
| US20050194070A1 (en) * | 2004-03-02 | 2005-09-08 | Mannava Seetha R. | Lower fluence boundary oblique laser shock peening |
| WO2007055864A2 (en) * | 2005-10-12 | 2007-05-18 | Surface Technology Holdings, Ltd | Improved integrally bladed rotating turbo machinery and method and apparatus for achieving the same |
| US20070157447A1 (en) * | 2006-01-09 | 2007-07-12 | Prevey Paul S | Method of improving the properties of a repaired component and a component improved thereby |
| US8330070B2 (en) * | 2006-05-11 | 2012-12-11 | Kabushiki Kaisha Toshiba | Laser shock hardening method and apparatus |
| US20100136296A1 (en) * | 2006-11-30 | 2010-06-03 | United Technologies Corporation | Densification of coating using laser peening |
| US9133720B2 (en) * | 2007-12-28 | 2015-09-15 | United Technologies Corporation | Integrally bladed rotor with slotted outer rim |
| DE102008010847A1 (de) * | 2008-02-25 | 2009-08-27 | Rolls-Royce Deutschland Ltd & Co Kg | Verfahren und Vorrichtung zum Kugelstrahlverfestigen von Bliskschaufeln |
| DE102010001287A1 (de) * | 2010-01-27 | 2011-07-28 | Rolls-Royce Deutschland Ltd & Co KG, 15827 | Verfahren und Vorrichtung zur Oberflächenverfestigung von Bliskschaufeln |
| WO2013049797A1 (en) * | 2011-09-30 | 2013-04-04 | Fosdick George A | Wheel turbine rotor |
| US9533371B2 (en) | 2012-01-17 | 2017-01-03 | United Technologies Corporation | Apparatus and method for on line surface enhancement of a workpiece |
| EP2903776B8 (en) | 2012-10-01 | 2021-04-07 | Raytheon Technologies Corporation | Methods for testing laser shock peening |
| CN103898297B (zh) * | 2012-12-24 | 2016-07-06 | 中国科学院沈阳自动化研究所 | 一种整体叶盘激光冲击强化方法 |
| US9914985B2 (en) * | 2014-09-09 | 2018-03-13 | G.C. Laser Systems, Inc. | Laser ablation and processing methods and systems |
| US11047017B2 (en) | 2014-09-09 | 2021-06-29 | G.C. Laser Systems, Inc. | Laser ablation devices that utilize beam profiling assemblies to clean and process surfaces |
| CN106282532B (zh) * | 2016-08-18 | 2018-01-16 | 江苏大学 | 一种获得金属表层晶粒混合分布的激光冲击强化组合方法 |
| CN106467933B (zh) * | 2016-08-29 | 2018-10-09 | 江苏大学 | 一种基于梯度晶粒的激光冲击强化方法 |
| US11298799B2 (en) * | 2018-05-03 | 2022-04-12 | General Electric Company | Dual sided shot peening of BLISK airfoils |
| CN111575476B (zh) * | 2020-04-09 | 2021-10-26 | 广东镭奔激光科技有限公司 | 一种叶片边缘激光冲击强化的方法 |
| JP7609589B2 (ja) * | 2020-09-24 | 2025-01-07 | 浜松ホトニクス株式会社 | レーザ加工方法及びレーザ加工装置 |
| LU102198B1 (en) * | 2020-11-05 | 2022-05-05 | Centrum Vyzkumu Rez S R O | A method for extending a fatigue life of a turbine blade affected by pitting and product thereof |
| CN113426899B (zh) * | 2021-06-25 | 2024-03-08 | 南通艾郎风电科技发展有限公司 | 一种风电叶片的铺设方法 |
| CN114250356B (zh) * | 2021-12-16 | 2023-08-29 | 江苏大学 | 一种提高纤维金属层板机械连接件疲劳性能的方法 |
| CN114592119A (zh) * | 2022-03-14 | 2022-06-07 | 中国航空制造技术研究院 | 一种基于预应力的激光冲击强化方法 |
| CN115870699B (zh) * | 2022-10-25 | 2024-11-12 | 杭州汽轮动力集团股份有限公司 | 一种燃气轮机压气机静叶环装焊定位夹具及相关装焊方法 |
| CN117403053A (zh) * | 2023-09-19 | 2024-01-16 | 中国航发北京航空材料研究院 | 一种构建叶片表面微织构的激光冲击强化方法 |
| CN118181338B (zh) * | 2024-05-17 | 2024-07-19 | 西北工业大学 | 一种整体叶盘装夹机构、移动组件及激光强化系统 |
Family Cites Families (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2724003B2 (ja) | 1989-11-10 | 1998-03-09 | キヤノン株式会社 | 光磁気記録媒体 |
| US5067876A (en) | 1990-03-29 | 1991-11-26 | General Electric Company | Gas turbine bladed disk |
| AU5717894A (en) | 1992-12-21 | 1994-07-19 | Chong Kun Dang Corporation | 2-(2-substituted pyrrolidin-4-yl)thio-carbapenem derivatives |
| US5492447A (en) | 1994-10-06 | 1996-02-20 | General Electric Company | Laser shock peened rotor components for turbomachinery |
| US5591009A (en) | 1995-01-17 | 1997-01-07 | General Electric Company | Laser shock peened gas turbine engine fan blade edges |
| US5674329A (en) | 1996-04-26 | 1997-10-07 | General Electric Company | Adhesive tape covered laser shock peening |
| US5674328A (en) | 1996-04-26 | 1997-10-07 | General Electric Company | Dry tape covered laser shock peening |
| US5911890A (en) * | 1997-02-25 | 1999-06-15 | Lsp Technologies, Inc. | Oblique angle laser shock processing |
| US5932120A (en) | 1997-12-18 | 1999-08-03 | General Electric Company | Laser shock peening using low energy laser |
| US5951790A (en) * | 1998-06-26 | 1999-09-14 | General Electric Company | Method of monitoring and controlling laser shock peening using an in plane deflection test coupon |
| US6183882B1 (en) * | 1998-06-29 | 2001-02-06 | General Electric Company | In plane deflection coupon for monitoring and controlling of laser shock peening |
| US6200689B1 (en) * | 1998-10-14 | 2001-03-13 | General Electric Company | Laser shock peened gas turbine engine seal teeth |
| US5948293A (en) * | 1998-12-03 | 1999-09-07 | General Electric Company | Laser shock peening quality assurance by volumetric analysis of laser shock peened dimple |
| US6296448B1 (en) * | 1999-09-30 | 2001-10-02 | General Electric Company | Simultaneous offset dual sided laser shock peening |
-
2001
- 2001-01-29 US US09/771,856 patent/US6541733B1/en not_active Expired - Fee Related
-
2002
- 2002-01-17 CA CA002368288A patent/CA2368288C/en not_active Expired - Fee Related
- 2002-01-29 DE DE60233536T patent/DE60233536D1/de not_active Expired - Lifetime
- 2002-01-29 BR BRPI0200332-5A patent/BR0200332B1/pt not_active IP Right Cessation
- 2002-01-29 SG SG200200529A patent/SG109489A1/en unknown
- 2002-01-29 EP EP02250594A patent/EP1227164B1/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| EP1227164A3 (en) | 2003-11-26 |
| EP1227164B1 (en) | 2009-09-02 |
| EP1227164A2 (en) | 2002-07-31 |
| US6541733B1 (en) | 2003-04-01 |
| CA2368288A1 (en) | 2002-07-29 |
| CA2368288C (en) | 2009-12-22 |
| BR0200332B1 (pt) | 2012-01-24 |
| DE60233536D1 (de) | 2009-10-15 |
| SG109489A1 (en) | 2005-03-30 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| EP1227164A3 (en) | Laser shock peening integrally bladed rotor blade edges | |
| KR820000756B1 (ko) | 로우터블레이드 | |
| US5988982A (en) | Altering vibration frequencies of workpieces, such as gas turbine engine blades | |
| MY127492A (en) | Simultaneous offset dual sided laser shock peening with oblique angle laser beams | |
| US6336844B1 (en) | Method and machine for the ultrasonic peening of parts on a wheel | |
| US5620307A (en) | Laser shock peened gas turbine engine blade tip | |
| SE8503614D0 (sv) | Gas turbine bladed disk assembly | |
| EP1152122A2 (en) | Turbomachinery blade | |
| JP2000337294A (ja) | 応力除去された動翼支持構造 | |
| BR9905955B1 (pt) | processo para a restauração de um revestimento protetor de uma pá de motor de turbina a gás. | |
| CA2224204A1 (en) | High efficiency, low-noise, axial fan assembly | |
| US5746578A (en) | Retention system for bar-type damper of rotor | |
| AU1273088A (en) | Moving blade for steam turbines | |
| CA2358596A1 (en) | Hardwall fan case with structured bumper | |
| EP0731184B1 (en) | Laser shock peened gas turbine engine compressor airfoil edges | |
| US5749705A (en) | Retention system for bar-type damper of rotor blade | |
| EP3880936B1 (en) | Bladed rotor system and method of servicing a bladed rotor system | |
| ATE206487T1 (de) | Oberflächenbehandlung von rotoren | |
| EP1380657B1 (en) | Single sided laser shock peening | |
| GB2399866A (en) | A compressor blade | |
| US20100043512A1 (en) | Device and method for the surface peening of a component of a gas turbine | |
| JPH10184305A (ja) | シュラウド動翼を有するタービン | |
| JP4677203B2 (ja) | ガスタービンエンジンのロータ組立体を設計するための方法及び装置 | |
| US7029237B2 (en) | Retention capacity of blade having an asymmetrical hammerhead connection | |
| EP3659541B1 (en) | Reverse-flow brake for rotors in dental preparation instruments |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| B07A | Technical examination (opinion): publication of technical examination (opinion) | ||
| B06A | Notification to applicant to reply to the report for non-patentability or inadequacy of the application according art. 36 industrial patent law | ||
| B09A | Decision: intention to grant | ||
| B16A | Patent or certificate of addition of invention granted |
Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 29/01/2002, OBSERVADAS AS CONDICOES LEGAIS. |
|
| B21F | Lapse acc. art. 78, item iv - on non-payment of the annual fees in time |
Free format text: REFERENTE A 14A ANUIDADE. |
|
| B24J | Lapse because of non-payment of annual fees (definitively: art 78 iv lpi, resolution 113/2013 art. 12) |
Free format text: EM VIRTUDE DA EXTINCAO PUBLICADA NA RPI 2344 DE 08-12-2015 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDA A EXTINCAO DA PATENTE E SEUS CERTIFICADOS, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013. |