CA2011414A1 - Procede de reparation d'aubes de turbines - Google Patents

Procede de reparation d'aubes de turbines

Info

Publication number
CA2011414A1
CA2011414A1 CA2011414A CA2011414A CA2011414A1 CA 2011414 A1 CA2011414 A1 CA 2011414A1 CA 2011414 A CA2011414 A CA 2011414A CA 2011414 A CA2011414 A CA 2011414A CA 2011414 A1 CA2011414 A1 CA 2011414A1
Authority
CA
Canada
Prior art keywords
turbine blade
insert
blade repair
securing
hardened
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.)
Granted
Application number
CA2011414A
Other languages
English (en)
Other versions
CA2011414C (fr
Inventor
Raymond Donald Legros
Michael James Fraser
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.)
Refurbished Turbine Components Ltd
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of CA2011414A1 publication Critical patent/CA2011414A1/fr
Application granted granted Critical
Publication of CA2011414C publication Critical patent/CA2011414C/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P6/00Restoring or reconditioning objects
    • B23P6/002Repairing turbine components, e.g. moving or stationary blades, rotors
    • B23P6/005Repairing turbine components, e.g. moving or stationary blades, rotors using only replacement pieces of a particular form
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/04Making specific metal objects by operations not covered by a single other subclass or a group in this subclass turbine or like blades from several pieces
    • 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
    • F01D5/005Repairing methods or devices
    • 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49316Impeller making
    • Y10T29/49318Repairing or disassembling
    • 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49316Impeller making
    • Y10T29/49336Blade making
    • 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49718Repairing
    • Y10T29/49721Repairing with disassembling
    • Y10T29/49723Repairing with disassembling including reconditioning of part
    • Y10T29/49725Repairing with disassembling including reconditioning of part by shaping
    • Y10T29/49726Removing material
    • Y10T29/49728Removing material and by a metallurgical operation, e.g., welding, diffusion bonding, casting
    • 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49718Repairing
    • Y10T29/49732Repairing by attaching repair preform, e.g., remaking, restoring, or patching
    • Y10T29/49734Repairing by attaching repair preform, e.g., remaking, restoring, or patching and removing damaged material
    • Y10T29/49737Metallurgically attaching preform

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Heat Treatment Of Articles (AREA)
CA002011414A 1989-03-04 1990-03-02 Procede de reparation d'aubes de turbines Expired - Fee Related CA2011414C (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB898904988A GB8904988D0 (en) 1989-03-04 1989-03-04 Turbine blade repair
GB8904988.6 1989-03-04

Publications (2)

Publication Number Publication Date
CA2011414A1 true CA2011414A1 (fr) 1990-09-04
CA2011414C CA2011414C (fr) 2000-05-02

Family

ID=10652746

Family Applications (1)

Application Number Title Priority Date Filing Date
CA002011414A Expired - Fee Related CA2011414C (fr) 1989-03-04 1990-03-02 Procede de reparation d'aubes de turbines

Country Status (4)

Country Link
US (1) US5033938A (fr)
EP (1) EP0392656A1 (fr)
CA (1) CA2011414C (fr)
GB (2) GB8904988D0 (fr)

Families Citing this family (41)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2244943B (en) * 1990-06-12 1994-03-30 Turbine Blading Ltd Method of repair of turbines
US5140737A (en) * 1991-01-10 1992-08-25 Noland Edmund B In situ flywheel repair method
GB9109016D0 (en) * 1991-04-26 1991-06-12 Turbine Blading Ltd Turbine blade repair
US5183390A (en) * 1991-07-10 1993-02-02 Westinghouse Electric Corp. Method of forming a trailing edge on a steam turbine blade and the blade made thereby
US5233673A (en) 1991-10-09 1993-08-03 Hughes Aircraft Company Output steerable optical phased array
US5248241A (en) * 1991-10-21 1993-09-28 Southern California Edison Co. Components made of hardenable and non-hardenable materials
DE4225443C2 (de) * 1992-07-31 1995-11-16 Mtu Muenchen Gmbh Verfahren zur Herstellung einer Schweißverbindung von Bauteilen für Turbomaschinen, insbesondere zur Bauteilreperatur und Verwendung des Verfahrens
US5351395A (en) * 1992-12-30 1994-10-04 General Electric Company Process for producing turbine bucket with water droplet erosion protection
DE4327189C2 (de) * 1993-08-13 1996-02-01 Mtu Muenchen Gmbh Reparaturverfahren für im Kopf- oder Kantenbereich beschädigte Schaufelblätter von Turbomaschinen
US5522134A (en) * 1994-06-30 1996-06-04 United Technologies Corporation Turbine vane flow area restoration method
US5531570A (en) * 1995-03-06 1996-07-02 General Electric Company Distortion control for laser shock peened gas turbine engine compressor blade edges
IL117347A (en) * 1995-03-06 1999-10-28 Gen Electric Laser shock peened gas turbine engine compressor airfoil edges
IT1293734B1 (it) * 1997-07-18 1999-03-10 Voith Riva Hydro S P A Procedimento per la fabbricazione di ruote di turbine idrauliche e ruote cosi' ottenute
US5908522A (en) * 1997-11-07 1999-06-01 Composite Technology, Inc. Supplemental leading edge wear strip for a rotor blade
DE19803589A1 (de) * 1998-01-30 1999-08-12 Voith Hydro Gmbh & Co Kg Verfahren zum Herstellen eines Bauteiles einer Strömungsmaschine
US6339878B1 (en) 2000-03-27 2002-01-22 United Technologies Corporation Method of repairing an airfoil
AU2001259200A1 (en) * 2000-04-28 2001-11-12 Elliott Turbomachinery Co., Inc. Method of brazing and article made therefrom
US6568077B1 (en) * 2000-05-11 2003-05-27 General Electric Company Blisk weld repair
US6508000B2 (en) 2001-02-08 2003-01-21 Siemens Westinghouse Power Corporation Transient liquid phase bonding repair for advanced turbine blades and vanes
US6536110B2 (en) * 2001-04-17 2003-03-25 United Technologies Corporation Integrally bladed rotor airfoil fabrication and repair techniques
US6743350B2 (en) * 2002-03-18 2004-06-01 General Electric Company Apparatus and method for rejuvenating cooling passages within a turbine airfoil
US6925810B2 (en) * 2002-11-08 2005-08-09 Honeywell International, Inc. Gas turbine engine transition liner assembly and repair
US20050102835A1 (en) * 2003-11-14 2005-05-19 Trewiler Gary E. Method for repairing gas turbine rotor blades
FR2871399B1 (fr) * 2004-06-15 2006-09-22 Snecma Moteurs Sa Procede de reparation d'un element d'aube
US7509737B2 (en) * 2005-03-10 2009-03-31 Air Cool Industrial Co. Ltd. Fan blade manufacturing methods
US7761989B2 (en) * 2005-11-22 2010-07-27 United Technologies Corporation Methods for repairing gas turbine engine components
US7959409B2 (en) * 2007-03-01 2011-06-14 Honeywell International Inc. Repaired vane assemblies and methods of repairing vane assemblies
JP4898720B2 (ja) * 2008-02-14 2012-03-21 三菱重工業株式会社 タービン動翼の補修方法
US20100050407A1 (en) * 2008-08-28 2010-03-04 Buck David A Method of Repairing Tong Jaw
US8800145B2 (en) * 2008-12-30 2014-08-12 Sikorsky Aircraft Corporation Refurbishing method and system for a main rotor blade spar
DE102009043136A1 (de) * 2009-09-26 2011-03-31 Mtu Aero Engines Gmbh Verfahren zum Reparieren eines Bauteils einer Strömungsmaschine
GB2477154B (en) 2010-01-26 2012-03-21 Rolls Royce Plc A method of restoring a metallic component
FR2960463B1 (fr) * 2010-06-01 2013-03-29 Snecma Procede de reparation d'une bride d'un carter
US8672634B2 (en) 2010-08-30 2014-03-18 United Technologies Corporation Electroformed conforming rubstrip
RU2451589C1 (ru) * 2010-12-07 2012-05-27 Константин Владимирович Юферов Способ восстановления стальной детали
US9260978B2 (en) 2012-03-19 2016-02-16 General Electric Company System and method for heating a stator segment
US10428657B2 (en) 2013-06-21 2019-10-01 Pratt & Whitney Canada Corp. Method for repairing a blade
WO2015030674A1 (fr) * 2013-08-27 2015-03-05 Agency For Science, Technology And Research Procédé de traitement d'un revêtement formant barrière thermique
JP6178703B2 (ja) * 2013-11-13 2017-08-09 三菱日立パワーシステムズ株式会社 防食片を備えた蒸気タービン動翼の製造方法
PL3106257T3 (pl) * 2014-02-13 2018-09-28 The Chugoku Electric Power Co., Inc. Sposób naprawiania elementu ze staliwa
US11039507B2 (en) * 2017-02-23 2021-06-15 General Electric Company Method of brazing a treatment area of a load-bearing component

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AT293148B (de) * 1969-04-28 1971-09-27 Boehler & Co Ag Geb Verfahren zur Herstellung von Turbinenschaufeln
US4028787A (en) * 1975-09-15 1977-06-14 Cretella Salvatore Refurbished turbine vanes and method of refurbishment thereof
US4611744A (en) * 1982-06-23 1986-09-16 Refurbished Turbine Components Ltd. Turbine blade repair
JPS6245497A (ja) * 1985-08-23 1987-02-27 Mitsubishi Heavy Ind Ltd チタン動翼の補修方法
GB2198667B (en) * 1986-12-20 1991-08-07 Refurbished Turbine Components Parts for and methods of repairing machines

Also Published As

Publication number Publication date
GB2229944B (en) 1993-02-10
GB9004907D0 (en) 1990-05-02
GB8904988D0 (en) 1989-04-19
CA2011414C (fr) 2000-05-02
EP0392656A1 (fr) 1990-10-17
US5033938A (en) 1991-07-23
GB2229944A (en) 1990-10-10

Similar Documents

Publication Publication Date Title
CA2011414A1 (fr) Procede de reparation d'aubes de turbines
AU546843B2 (en) Turbine blade repair
GB2227190B (en) Turbine blade repair
DE69116440D1 (de) Verfahren zur Reparatur von Turbinen
AU557938B2 (en) Method of repairing turbine blade
ES2167919T3 (es) Metodo metalurgico para procesar superaleaciones basadas en niquel y hierro.
GB2245201B (en) Improvements in or relating to the repair of turbine blades
CA2407591A1 (fr) Traitements de surface devant ameliorer la resistance a la corrosion des aciers inoxydables austenitiques
JPS62161493A (ja) クラツクの補修方法
AU4838796A (en) Improvements in and relating to steel rails and methods of producing the same
JPS5633261A (en) Machining of crank shaft
Dorsch Eliminating the negative effects of EDM through the strategic selection of die steels
Fraser Repairing a Turbine Blade
SU699025A1 (ru) Способ восстановлени деталей из высокопрочных сталей
Fraser Turbine Blade Repair
Von Freeden et al. FE-modelling of the cooling behavior of a mechanically applied lead coating on steel components with multiple curvature
Kumanin et al. New Methods of Restoration Thermal Processing of Steel
JPS5922769B2 (ja) 鍛造品の熱処理法
Dorsch Strategic selection of die steels eliminates the negative effects of EDM
Reparaz et al. Failure of Steel Tools Upon Tempering: Causes and Remedies
Hara CONTROLLED SHOT PEENING FOR STRESS CORROSION RESISTANCE IN AIRCRAFT MAINTENANCE
Tanne Pulsed Surface Hardening
Migachev Effect of thickness of removed defective surface layer and predeformation degree on cast metal ductility
Kalna Influence of two-frequency low-cycle loading on fatigue life of steels and welded joints
Gotz Hardening Without Rework

Legal Events

Date Code Title Description
EEER Examination request
MKLA Lapsed