DE69920153D1 - Verfahren zur Reparatur eines Turbinebauteiles aus einer Superlegierung - Google Patents

Verfahren zur Reparatur eines Turbinebauteiles aus einer Superlegierung

Info

Publication number
DE69920153D1
DE69920153D1 DE69920153T DE69920153T DE69920153D1 DE 69920153 D1 DE69920153 D1 DE 69920153D1 DE 69920153 T DE69920153 T DE 69920153T DE 69920153 T DE69920153 T DE 69920153T DE 69920153 D1 DE69920153 D1 DE 69920153D1
Authority
DE
Germany
Prior art keywords
superalloy
repairing
component made
turbine component
turbine
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
DE69920153T
Other languages
English (en)
Other versions
DE69920153T2 (de
Inventor
Keng Nam Chen
Genfa Hu
Shih Tung Ngiam
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.)
GE Aviation Service Operation LLP
Original Assignee
GE Aviation Service Operation LLP
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 GE Aviation Service Operation LLP filed Critical GE Aviation Service Operation LLP
Application granted granted Critical
Publication of DE69920153D1 publication Critical patent/DE69920153D1/de
Publication of DE69920153T2 publication Critical patent/DE69920153T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C10/00—Solid state diffusion of only metal elements or silicon into metallic material surfaces
    • C23C10/02—Pretreatment of the material to be coated
    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/01—Selective coating, e.g. pattern coating, without pre-treatment of the material to be coated
    • 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
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12535—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.] with additional, spatially distinct nonmetal component
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12736—Al-base component
    • Y10T428/1275—Next to Group VIII or IB metal-base component
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12771—Transition metal-base component
    • Y10T428/12861—Group VIII or IB metal-base component
    • Y10T428/12875—Platinum group metal-base component
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12771—Transition metal-base component
    • Y10T428/12861—Group VIII or IB metal-base component
    • Y10T428/12931—Co-, Fe-, or Ni-base components, alternative to each other
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12771—Transition metal-base component
    • Y10T428/12861—Group VIII or IB metal-base component
    • Y10T428/12944—Ni-base component
DE69920153T 1998-12-22 1999-12-10 Verfahren zur Reparatur eines Turbinebauteiles aus einer Superlegierung Expired - Fee Related DE69920153T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US219158 1994-03-29
US09/219,158 US6228510B1 (en) 1998-12-22 1998-12-22 Coating and method for minimizing consumption of base material during high temperature service

Publications (2)

Publication Number Publication Date
DE69920153D1 true DE69920153D1 (de) 2004-10-21
DE69920153T2 DE69920153T2 (de) 2005-09-29

Family

ID=22818121

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69920153T Expired - Fee Related DE69920153T2 (de) 1998-12-22 1999-12-10 Verfahren zur Reparatur eines Turbinebauteiles aus einer Superlegierung

Country Status (8)

Country Link
US (1) US6228510B1 (de)
EP (1) EP1013786B1 (de)
JP (1) JP3881489B2 (de)
BR (1) BR9905920A (de)
CA (1) CA2292370C (de)
DE (1) DE69920153T2 (de)
SG (1) SG81340A1 (de)
TR (1) TR199903178A2 (de)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1123987A1 (de) * 2000-02-11 2001-08-16 General Electric Company Reparierbare Diffusionsaluminidbeschichtungen
EP1162284A1 (de) 2000-06-05 2001-12-12 Alstom (Switzerland) Ltd Verfahren zum Reparieren einer beschichteten Komponenten
FR2813318B1 (fr) * 2000-08-28 2003-04-25 Snecma Moteurs Formation d'un revetement aluminiure incorporant un element reactif, sur un substrat metallique
US6465040B2 (en) * 2001-02-06 2002-10-15 General Electric Company Method for refurbishing a coating including a thermally grown oxide
FR2827311B1 (fr) * 2001-07-12 2003-09-19 Snecma Moteurs Procede de reparation locale de pieces revetues d'une barriere thermique
US6886327B1 (en) 2002-03-20 2005-05-03 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration NiAl-based approach for rocket combustion chambers
CN100554494C (zh) 2003-05-30 2009-10-28 石川岛播磨重工业株式会社 反应抑制涡轮叶片
US20050035086A1 (en) * 2003-08-11 2005-02-17 Chen Keng Nam Upgrading aluminide coating on used turbine engine component
US7575039B2 (en) * 2003-10-15 2009-08-18 United Technologies Corporation Refractory metal core coatings
US20050118334A1 (en) * 2004-09-03 2005-06-02 General Electric Company Process for inhibiting srz formation and coating system therefor
GB2429465A (en) * 2005-08-24 2007-02-28 Univ Northumbria Newcastle Aluminide coating for a substrate and a method for providing same.
US8741381B2 (en) * 2012-05-04 2014-06-03 General Electric Company Method for removing a coating and a method for rejuvenating a coated superalloy component
US20130323066A1 (en) * 2012-05-31 2013-12-05 Monika D. Kinstler Maskant for fluoride ion cleaning
US9909202B2 (en) 2014-05-02 2018-03-06 General Electric Company Apparatus and methods for slurry aluminide coating repair
US10030298B2 (en) 2015-08-21 2018-07-24 General Electric Company Method for altering metal surfaces
US10533255B2 (en) * 2015-08-27 2020-01-14 Praxair S.T. Technology, Inc. Slurry formulations for formation of reactive element-doped aluminide coatings and methods of forming the same
US10202855B2 (en) * 2016-06-02 2019-02-12 General Electric Company Airfoil with improved coating system
US20200087794A1 (en) * 2018-09-14 2020-03-19 United Technologies Corporation Method of repairing a non-line of sight feature via a multi-layer coating
FR3138451A1 (fr) * 2022-07-28 2024-02-02 Safran Procédé d’application de revêtement et aube de turbine avec revêtement appliqué suivant ce procédé

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3544348A (en) 1968-10-25 1970-12-01 United Aircraft Corp Overhaul process for aluminide coated gas turbine engine components
US3640815A (en) * 1969-09-08 1972-02-08 Howmet Corp Method for surface treatment of nickel and cobalt base alloys
BE759275A (fr) * 1969-12-05 1971-04-30 Deutsche Edelstahlwerke Ag Procede d'application de couches protectrices diffusees sur despieces en alliage a base de cobalt
US3849865A (en) * 1972-10-16 1974-11-26 Nasa Method of protecting the surface of a substrate
US4241147A (en) * 1978-10-23 1980-12-23 Alloy Surfaces Company, Inc. Diffusion aluminized age-hardenable stainless steel
GB2009251B (en) * 1977-12-01 1982-08-18 Rolls Royce Coated metal part and the method of applying coating
US4176433A (en) 1978-06-29 1979-12-04 United Technologies Corporation Method of remanufacturing turbine vane clusters for gas turbine engines
JPS5518573A (en) * 1978-07-28 1980-02-08 Hitachi Ltd Diffusion-covering method for al on heat resistant alloy surface
US4965095A (en) 1979-03-30 1990-10-23 Alloy Surfaces Company, Inc. Method for refurbishing used jet engine hot section airfoils
JPS5675562A (en) * 1979-11-23 1981-06-22 Chobe Taguchi Heat treatment of metal for heat resisting
JPS59157272A (ja) * 1983-02-23 1984-09-06 Hitachi Zosen Corp 複合表面処理方法
US4897315A (en) 1985-10-15 1990-01-30 United Technologies Corporation Yttrium enriched aluminide coating for superalloys
JPH0432546A (ja) 1990-05-28 1992-02-04 Mitsubishi Heavy Ind Ltd ガスタービン動翼補修方法
US5116691A (en) * 1991-03-04 1992-05-26 General Electric Company Ductility microalloyed NiAl intermetallic compounds
FI96970C (fi) 1994-08-09 1996-09-25 Telatek Oy Menetelmä teräspintojen kunnostamiseksi
US5516380A (en) * 1994-10-14 1996-05-14 General Electric Company NiAl intermetallic alloy and article with improved high temperature strength
US5658614A (en) 1994-10-28 1997-08-19 Howmet Research Corporation Platinum aluminide CVD coating method
US5820337A (en) * 1995-01-03 1998-10-13 General Electric Company Double wall turbine parts
US5716720A (en) * 1995-03-21 1998-02-10 Howmet Corporation Thermal barrier coating system with intermediate phase bondcoat
US5824423A (en) * 1996-02-07 1998-10-20 N.V. Interturbine Thermal barrier coating system and methods
US5975852A (en) * 1997-03-31 1999-11-02 General Electric Company Thermal barrier coating system and method therefor
DE19824792B4 (de) * 1998-06-03 2005-06-30 Mtu Aero Engines Gmbh Verfahren zum Herstellen einer Haftschicht für eine Wärmedämmschicht

Also Published As

Publication number Publication date
CA2292370A1 (en) 2000-06-22
BR9905920A (pt) 2000-12-19
JP2000192258A (ja) 2000-07-11
DE69920153T2 (de) 2005-09-29
EP1013786A1 (de) 2000-06-28
US6228510B1 (en) 2001-05-08
CA2292370C (en) 2005-11-15
SG81340A1 (en) 2001-06-19
TR199903178A3 (tr) 2000-07-21
EP1013786B1 (de) 2004-09-15
JP3881489B2 (ja) 2007-02-14
TR199903178A2 (xx) 2000-07-21

Similar Documents

Publication Publication Date Title
DE69920153D1 (de) Verfahren zur Reparatur eines Turbinebauteiles aus einer Superlegierung
DE50009860D1 (de) Verfahren zur Reparatur einer Gasturbinenkomponente
DE69919742D1 (de) Verfahren zur herstellung eines bauteiles
DE69912376D1 (de) Verfahren zur herstellung eines halbleiterbauelements
DE60013533D1 (de) Verfahren zur Erzeugung eines dreidimensionalen kinematischen Modells der Verformung einer Sedimentschicht
ATE297704T1 (de) Verfahren zur herstellung eines stents
DE69941652D1 (de) Verfahren zur Herstellung eines Silizium-auf-Isolator-Substrats
DE69928198D1 (de) Verfahren zur erzeugung eines überzugsfilms und überzugszusammensetzung
DE60038423D1 (de) Verfahren zur Herstellung eines Halbleiterbauelements
DE50106828D1 (de) Verfahren zur glättung der oberfläche einer gasturbinenschaufel
DE59809873D1 (de) Verfahren zur herstellung eines lichtemittierenden bauelementes
DE69804962D1 (de) Verfahren zur darstellung einer delamellierten vermiculit zur herstellung eines endproduktes
DE69509155T2 (de) Verfahren zur Herstellung einer Gasturbinenschaufel
DE19758977B8 (de) Verfahren zur Herstellung eines Halbleiterbauelements
DE59904234D1 (de) Verfahren zur innenbearbeitung eines hohlen bauteils
DE50009560D1 (de) Verfahren zur herstellung einer turbinenschaufel
DE50013554D1 (de) Verfahren zum Herstellen einer Schaufel einer Strömungsmaschine
DE59905336D1 (de) Verfahren und vorrichtung zur kühlung einer niederdruckstufe einer dampfturbine
DE59710734D1 (de) Verfahren zur Regelung einer Gasturbogruppe
DE69934680D1 (de) Verfahren zur herstellung einer schicht
DE69913673D1 (de) Verfahren zur verbesserung der cetanzahl einer gasölfraktion
DE69922617D1 (de) Verfahren zur Herstellung eines Halbleiterbauelementes
DE50010312D1 (de) Verfahren zur herstellung eines leichtbauteils in verbundbauweise
ATE297379T1 (de) Verfahren zur herstellung eines geschützten 4- aminomethyl-pyrrolidin-3-ons
DE69921914D1 (de) Verfahren zur herstellung eines uhrengehäuses

Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee