JP5350603B2 - 超合金タービンブレードを熱処理するための固定治具の使用方法 - Google Patents

超合金タービンブレードを熱処理するための固定治具の使用方法 Download PDF

Info

Publication number
JP5350603B2
JP5350603B2 JP2007127488A JP2007127488A JP5350603B2 JP 5350603 B2 JP5350603 B2 JP 5350603B2 JP 2007127488 A JP2007127488 A JP 2007127488A JP 2007127488 A JP2007127488 A JP 2007127488A JP 5350603 B2 JP5350603 B2 JP 5350603B2
Authority
JP
Japan
Prior art keywords
blade
airfoil
fixture
temperature
platform
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
Application number
JP2007127488A
Other languages
English (en)
Japanese (ja)
Other versions
JP2007308798A5 (enExample
JP2007308798A (ja
Inventor
トーマス・ジェイ・ケリー
ウォーレン・ディー・グロスクラウス，ジュニア
ブレント・アール・ソルク
クリスティーヌ・ガヴァン・ウォルストン
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of JP2007308798A publication Critical patent/JP2007308798A/ja
Publication of JP2007308798A5 publication Critical patent/JP2007308798A5/ja
Application granted granted Critical
Publication of JP5350603B2 publication Critical patent/JP5350603B2/ja
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • 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
    • B23P6/00—Restoring or reconditioning objects
    • B23P6/002—Repairing turbine components, e.g. moving or stationary blades, rotors
    • B23P6/007—Repairing turbine components, e.g. moving or stationary blades, rotors using only additive methods, e.g. build-up welding
    • 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
    • C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
    • C21D9/0068—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for particular articles not mentioned below
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/10—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of nickel or cobalt or alloys based thereon
    • 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
    • F01D5/005—Repairing methods or devices
    • 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
    • F05D2230/40—Heat treatment
    • 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
    • F05D2230/80—Repairing, retrofitting or upgrading methods
    • 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)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Heat Treatment Of Articles (AREA)
JP2007127488A 2006-05-17 2007-05-14 超合金タービンブレードを熱処理するための固定治具の使用方法 Expired - Fee Related JP5350603B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US11/383,783 2006-05-17
US11/383,783 US20070267109A1 (en) 2006-05-17 2006-05-17 High pressure turbine airfoil recovery device and method of heat treatment

Publications (3)

Publication Number Publication Date
JP2007308798A JP2007308798A (ja) 2007-11-29
JP2007308798A5 JP2007308798A5 (enExample) 2012-08-30
JP5350603B2 true JP5350603B2 (ja) 2013-11-27

Family

ID=38420608

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2007127488A Expired - Fee Related JP5350603B2 (ja) 2006-05-17 2007-05-14 超合金タービンブレードを熱処理するための固定治具の使用方法

Country Status (6)

Country Link
US (2) US20070267109A1 (enExample)
EP (1) EP1857217B1 (enExample)
JP (1) JP5350603B2 (enExample)
BR (1) BRPI0701724A (enExample)
CA (1) CA2587311C (enExample)
SG (3) SG137786A1 (enExample)

Families Citing this family (36)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1595968A1 (de) * 2004-04-30 2005-11-16 Siemens Aktiengesellschaft Wärmebehandlungsverfahren für einkristalline oder direktional verfestigte Bauteile
US8986778B2 (en) * 2006-07-06 2015-03-24 Siemens Energy, Inc. Coating method for non-destructive examination of articles of manufacture
US9527169B2 (en) * 2007-02-27 2016-12-27 Siemens Energy, Inc. Process and apparatus for cooling a metal part during a welding operation
US8141249B2 (en) * 2007-10-11 2012-03-27 United Technologies Corporation Heat treating apparatus and method of using same
GB0800294D0 (en) * 2008-01-09 2008-02-20 Rolls Royce Plc Gas heater
SG155788A1 (en) * 2008-03-18 2009-10-29 Turbine Overhaul Services Pte Methods and apparatuses for correcting twist angle in a gas turbine engine blade
US8887390B2 (en) * 2008-08-15 2014-11-18 Dresser-Rand Company Method for correcting downstream deflection in gas turbine nozzles
US20110171394A1 (en) * 2008-08-26 2011-07-14 Allen David B Method of making a combustion turbine component using thermally sprayed transient liquid phase forming layer
DE102009040324B4 (de) 2009-09-05 2016-11-17 MTU Aero Engines AG Verfahren zur Wärmebehandlung von Gasturbinenschaufeln
DE102011086524A1 (de) 2011-11-17 2013-05-23 Mtu Aero Engines Gmbh Panzerung von Dichtfins von TiAl-Schaufeln durch induktives Auftragslöten von Hartstoffpartikeln
US8959738B2 (en) 2012-03-21 2015-02-24 General Electric Company Process of repairing a component, a repair tool for a component, and a component
WO2013167513A1 (en) * 2012-05-07 2013-11-14 Alstom Technology Ltd Method for manufacturing of components made of single crystal (sx) or directionally solidified (ds) superalloys
JP2014047389A (ja) * 2012-08-31 2014-03-17 Hitachi Ltd 発電用ガスタービン用動翼と、熱処理方法
US10293437B2 (en) * 2012-10-12 2019-05-21 United Technologies Corporation Method of working a gas turbine engine airfoil
JP6534379B2 (ja) * 2013-03-15 2019-06-26 ユナイテッド テクノロジーズ コーポレイションＵｎｉｔｅｄ Ｔｅｃｈｎｏｌｏｇｉｅｓ Ｃｏｒｐｏｒａｔｉｏｎ 再結晶化を抑制するコーナー半径を有する鋳造部品
EP2815841B1 (en) * 2013-06-18 2016-02-10 Alstom Technology Ltd Method for post-weld heat treatment of welded components made of gamma prime strengthened superalloys
CN105705278B (zh) * 2013-11-14 2018-06-22 通用电气公司 单晶合金构件的分层制造
KR101557406B1 (ko) 2013-12-24 2015-10-20 두산중공업 주식회사 최종단 블레이드 열처리 장치 및 열처리 방법, 그리고 그를 이용한 최종단 블레이드 제조 방법
US9797253B2 (en) * 2014-09-17 2017-10-24 General Electric Company System and method for repairing blades
US10385433B2 (en) 2016-03-16 2019-08-20 Honeywell International Inc. Methods for processing bonded dual alloy rotors including differential heat treatment processes
DE102016206558A1 (de) 2016-04-19 2017-10-19 MTU Aero Engines AG Verfahren und Vorrichtung zum Herstellen zumindest eines Bauteilbereichs eines Bauteils
JP6754682B2 (ja) 2016-11-28 2020-09-16 三菱日立パワーシステムズ株式会社 ニッケル基合金再生部材の製造方法
US20180238173A1 (en) * 2017-02-22 2018-08-23 General Electric Company Method of manufacturing turbine airfoil and tip component thereof
US10625342B2 (en) 2017-02-22 2020-04-21 General Electric Company Method of repairing turbine component
US10717130B2 (en) 2017-02-22 2020-07-21 General Electric Company Method of manufacturing turbine airfoil and tip component thereof
US11154956B2 (en) 2017-02-22 2021-10-26 General Electric Company Method of repairing turbine component using ultra-thin plate
US10610933B2 (en) 2017-02-22 2020-04-07 General Electric Company Method of manufacturing turbine airfoil with open tip casting and tip component thereof
US10702958B2 (en) 2017-02-22 2020-07-07 General Electric Company Method of manufacturing turbine airfoil and tip component thereof using ceramic core with witness feature
US11371349B2 (en) 2019-04-05 2022-06-28 Raytheon Technologies Corporation Gas impingement in-process cooling system
US11242588B2 (en) * 2019-12-12 2022-02-08 General Electric Company System and method to apply multiple thermal treatments to workpiece and related turbomachine components
US11199101B2 (en) 2019-12-12 2021-12-14 General Electric Company System and method to apply multiple thermal treatments to workpiece and related turbomachine components
CN111575671B (zh) * 2020-06-12 2022-03-29 中国人民解放军空军工程大学 用于叶片表面选区制备涂层的夹具及涂层的制备方法
KR102252487B1 (ko) * 2020-12-07 2021-05-14 한전케이피에스 주식회사 가스터빈 회전익 코팅용 지그
CN113046528B (zh) * 2021-02-03 2022-05-10 东方电气集团东方汽轮机有限公司 一种叶片热处理加热装置
US11828190B2 (en) 2021-11-18 2023-11-28 General Electric Company Airfoil joining apparatus and methods
CN119525870B (zh) * 2024-12-02 2025-10-24 湖北辉创重型工程有限公司 一种钢结构桥梁焊接施工用工作平台

Family Cites Families (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3833207A (en) * 1971-07-22 1974-09-03 Gen Electric Apparatus for alloy microstructure control
US3772090A (en) * 1971-07-22 1973-11-13 Gen Electric Alloy microstructure control
US4818833A (en) * 1987-12-21 1989-04-04 United Technologies Corporation Apparatus for radiantly heating blade tips
DE4141927C2 (de) * 1991-12-19 1995-06-14 Mtu Maintenance Gmbh Verfahren und Vorrichtung zum Schweißen von Werkstücken
US5312497A (en) * 1991-12-31 1994-05-17 United Technologies Corporation Method of making superalloy turbine disks having graded coarse and fine grains
US5527402A (en) * 1992-03-13 1996-06-18 General Electric Company Differentially heat treated process for the manufacture thereof
JPH08225828A (ja) * 1995-02-15 1996-09-03 Toshiba Corp 蒸気タービン動翼のフレームハードニング装置及びフレームハードニング方法
DE19630703C2 (de) * 1996-07-30 2000-02-10 Mtu Muenchen Gmbh Verfahren und Vorrichtung zum Reparaturschweissen von Teilen aus Ni-Basis-Legierungen sowie Anwendung des Verfahrens und Vorrichtung
DE19642980C1 (de) * 1996-10-18 1998-08-13 Mtu Muenchen Gmbh Verfahren zur Instandsetzung verschlissener Schaufelspitzen von Verdichter- und Turbinenschaufel
JPH10180442A (ja) * 1996-12-25 1998-07-07 Hitachi Ltd ガスタービン翼の補修方法
US5794338A (en) * 1997-04-04 1998-08-18 General Electric Company Method for repairing a turbine engine member damaged tip
US5822852A (en) * 1997-07-14 1998-10-20 General Electric Company Method for replacing blade tips of directionally solidified and single crystal turbine blades
US6118098A (en) * 1997-10-10 2000-09-12 Siemens Westinghouse Power Corporation Turbine rotor modernization and repair method
US6003754A (en) * 1997-10-21 1999-12-21 Allison Advanced Development Co. Airfoil for a gas turbine engine and method of manufacture
US6020571A (en) * 1998-12-31 2000-02-01 General Electric Company Welding method and apparatus therefor
US6124568A (en) * 1998-12-31 2000-09-26 General Electric Company Heating apparatus for a welding operation and method therefor
US6333484B1 (en) * 2000-03-17 2001-12-25 Chromalloy Gas Turbine Corporation Welding superalloy articles
EP1143030A1 (en) * 2000-04-03 2001-10-10 ABB Alstom Power N.V. Tip material for a turbine blade and method of manufacturing or repairing a tip of a turbine blade
US6359267B1 (en) * 2000-05-31 2002-03-19 Ameritherm, Inc. Induction heating system
US6531005B1 (en) * 2000-11-17 2003-03-11 General Electric Co. Heat treatment of weld repaired gas turbine engine components
US6502304B2 (en) * 2001-05-15 2003-01-07 General Electric Company Turbine airfoil process sequencing for optimized tip performance
US6908288B2 (en) * 2001-10-31 2005-06-21 General Electric Company Repair of advanced gas turbine blades
US6755924B2 (en) * 2001-12-20 2004-06-29 General Electric Company Method of restoration of mechanical properties of a cast nickel-based super alloy for serviced aircraft components
US6660110B1 (en) * 2002-04-08 2003-12-09 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Heat treatment devices and method of operation thereof to produce dual microstructure superalloy disks
EP1595968A1 (de) * 2004-04-30 2005-11-16 Siemens Aktiengesellschaft Wärmebehandlungsverfahren für einkristalline oder direktional verfestigte Bauteile
DE102006010927A1 (de) * 2006-03-09 2007-09-13 Mtu Aero Engines Gmbh Gasturbinenbauteil sowie Verfahren zur Bearbeitung von Gasturbinenbauteilen im Rahmen der Herstellung oder Instandsetzung dieser Gasturbinenbauteile

Also Published As

Publication number Publication date
BRPI0701724A (pt) 2008-01-15
US20090314393A1 (en) 2009-12-24
SG157392A1 (en) 2009-12-29
EP1857217A1 (en) 2007-11-21
CA2587311C (en) 2015-06-30
JP2007308798A (ja) 2007-11-29
CA2587311A1 (en) 2007-11-17
SG137786A1 (en) 2007-12-28
SG190599A1 (en) 2013-06-28
US7875135B2 (en) 2011-01-25
EP1857217B1 (en) 2018-01-17
US20070267109A1 (en) 2007-11-22

Similar Documents

Publication Publication Date Title
JP5350603B2 (ja) 超合金タービンブレードを熱処理するための固定治具の使用方法
EP0478374B1 (en) Welding high-strength nickel base superalloys
RU2265505C2 (ru) Сварка изделий из суперсплавов
EP1258312B1 (en) Repair of a single crystal nickel based superalloy article
US7896986B2 (en) Heat treatment of superalloy components
JP3218567B2 (ja) 高強力ニッケル基超合金類の溶接
US5822852A (en) Method for replacing blade tips of directionally solidified and single crystal turbine blades
TW527251B (en) Weld repair of directionally solidified articles
US6084196A (en) Elevated-temperature, plasma-transferred arc welding of nickel-base superalloy articles
US8561298B2 (en) Superalloy component welding at ambient temperature
JP4731002B2 (ja) 超合金溶接組成物及び補修タービンエンジン部品
US10315264B2 (en) Joining process and joined article
CN101405416A (zh) 焊接添加材料和其应用以及焊接方法和构件
JP2001158929A (ja) 超合金溶接組成物および修復されたタービンエンジン部品
JP2007245238A (ja) ニッケル基超合金コンポーネントの修復用ニッケル合金ワイヤおよびワークピースのクラック修復方法
JP2006239775A (ja) ニッケル合金またはニッケルベース超合金から製造されたエアフォイル、およびｉｎ−１００から製造された一体型ブレード付ロータの溶接補修方法
JP2009090371A (ja) 溶接方法
JP2009090371A6 (ja) 溶接方法
US20120084980A1 (en) Extending Useful Life of a Cobalt-Based Gas Turbine Component
CN1977064A (zh) 用于单晶或定向凝固构件的热处理方法
JPH10180442A (ja) ガスタービン翼の補修方法
JP2016061292A (ja) ブレードを補修するためのシステムおよび方法
EP3366415B1 (en) Method of brazing a treatment area of a load-bearing gas turbine component
CN113226611A (zh) 焊接-钎焊技术
Frederick et al. Laser Weld Repair of Service Exposed IN738 and GTD111 Buckets

Legal Events

Date Code Title Description
A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20100507

RD04 Notification of resignation of power of attorney

Free format text: JAPANESE INTERMEDIATE CODE: A7424

Effective date: 20100507

A521 Written amendment

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20120713

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20130312

A521 Written amendment

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20130612

TRDD Decision of grant or rejection written
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20130723

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20130822

R150 Certificate of patent or registration of utility model

Free format text: JAPANESE INTERMEDIATE CODE: R150

Ref document number: 5350603

Country of ref document: JP

Free format text: JAPANESE INTERMEDIATE CODE: R150

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

LAPS Cancellation because of no payment of annual fees