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 palhetas

Info

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
Application number
BR0200332-5A
Other languages
English (en)
Other versions
BR0200332B1 (pt
Inventor
Seetharamaiah Mannava
Jeffery Howard Nussbaum
Abraham S Assa
Andrea G M Cox
James R Zisson
Albert Everett Mcdaniel
William Dewaine Cowie
Original Assignee
Gen Electric
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Gen Electric filed Critical Gen Electric
Publication of BR0200332A publication Critical patent/BR0200332A/pt
Publication of BR0200332B1 publication Critical patent/BR0200332B1/pt

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/28Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/286Particular treatment of blades, e.g. to increase durability or resistance against corrosion or erosion
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING 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
    • C21D10/00Modifying the physical properties by methods other than heat treatment or deformation
    • C21D10/005Modifying the physical properties by methods other than heat treatment or deformation by laser shock processing
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient 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%.
BRPI0200332-5A 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. BR0200332B1 (pt)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

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

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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.