DE69710622D1 - Verfahren zum Herstellen von Ablagerungen auf lokalen Stellen von Werkstücken aus Superlegierungen - Google Patents

Verfahren zum Herstellen von Ablagerungen auf lokalen Stellen von Werkstücken aus Superlegierungen

Info

Publication number
DE69710622D1
DE69710622D1 DE69710622T DE69710622T DE69710622D1 DE 69710622 D1 DE69710622 D1 DE 69710622D1 DE 69710622 T DE69710622 T DE 69710622T DE 69710622 T DE69710622 T DE 69710622T DE 69710622 D1 DE69710622 D1 DE 69710622D1
Authority
DE
Germany
Prior art keywords
superalloys
workpieces made
local locations
producing deposits
deposits
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 - Lifetime
Application number
DE69710622T
Other languages
English (en)
Other versions
DE69710622T2 (de
Inventor
Jean-Francois Clement
Jean-Pierre Ferte
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA Moteurs SA
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 SNECMA Moteurs SA filed Critical SNECMA Moteurs SA
Publication of DE69710622D1 publication Critical patent/DE69710622D1/de
Application granted granted Critical
Publication of DE69710622T2 publication Critical patent/DE69710622T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

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
    • B23P6/005—Repairing turbine components, e.g. moving or stationary blades, rotors using only replacement pieces of a particular form
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
    • B23K35/02—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape
    • B23K35/0222—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape for use in soldering, brazing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
    • B23K35/02—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape
    • B23K35/0222—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape for use in soldering, brazing
    • B23K35/0244—Powders, particles or spheres; Preforms made therefrom
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2101/00—Articles made by soldering, welding or cutting
    • B23K2101/001—Turbines
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
    • B23K35/02—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape
    • B23K35/0222—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape for use in soldering, brazing
    • B23K35/0233—Sheets, foils
    • B23K35/0238—Sheets, foils layered
    • 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
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/49336—Blade making
    • 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
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/4998—Combined manufacture including applying or shaping of fluent material
    • Y10T29/49982—Coating

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Powder Metallurgy (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Welding Or Cutting Using Electron Beams (AREA)
DE69710622T 1996-03-14 1997-03-13 Verfahren zum Herstellen von Ablagerungen auf lokalen Stellen von Werkstücken aus Superlegierungen Expired - Lifetime DE69710622T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9603202A FR2746043B1 (fr) 1996-03-14 1996-03-14 Procede de realisation d'un apport sur une zone localisee de piece en superalliage

Publications (2)

Publication Number Publication Date
DE69710622D1 true DE69710622D1 (de) 2002-04-04
DE69710622T2 DE69710622T2 (de) 2002-09-12

Family

ID=9490177

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69710622T Expired - Lifetime DE69710622T2 (de) 1996-03-14 1997-03-13 Verfahren zum Herstellen von Ablagerungen auf lokalen Stellen von Werkstücken aus Superlegierungen

Country Status (6)

Country Link
US (1) US5890274A (de)
EP (1) EP0795377B1 (de)
CA (1) CA2199691C (de)
DE (1) DE69710622T2 (de)
FR (1) FR2746043B1 (de)
ZA (1) ZA972245B (de)

Families Citing this family (28)

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US20010001042A1 (en) * 1998-04-07 2001-05-10 Sinatra Raymond J. Method for depositing braze alloy
US6164916A (en) * 1998-11-02 2000-12-26 General Electric Company Method of applying wear-resistant materials to turbine blades, and turbine blades having wear-resistant materials
DE10000988A1 (de) * 1999-02-17 2001-07-19 Euromat Gmbh Verfahren zum Herstellen einer Schutzschicht auf der Oberfläche eines Bauteils o. dgl. Werkstückes, Lotwerkstoff dafür sowie deren Verwendung
US6302318B1 (en) * 1999-06-29 2001-10-16 General Electric Company Method of providing wear-resistant coatings, and related articles
DE10000989A1 (de) * 2000-01-13 2001-07-19 Euromat Gmbh Verfahren zum Herstellen einer Schutzschicht auf der Oberfläche eines Bauteils o. dgl. Werkstückes, Lotwerkstoff dafür sowie deren Verwendung
US6468040B1 (en) 2000-07-24 2002-10-22 General Electric Company Environmentally resistant squealer tips and method for making
US6612480B1 (en) * 2000-11-21 2003-09-02 C.A. Patents, L.L.C. Method of forming preforms for metal repairs
DE10161824B4 (de) * 2001-12-15 2004-02-12 Mtu Aero Engines Gmbh Verfahren zum Instandsetzen von verschlissenen oder außer Maß gefertigten Bauteilen
US7051435B1 (en) * 2003-06-13 2006-05-30 General Electric Company Process for repairing turbine components
EP1867423A1 (de) * 2006-06-12 2007-12-19 Siemens Aktiengesellschaft Verfahren zum Reparieren eines Bauteils durch Verlöten eines mit Lot beschichteten Bleches
US20100237134A1 (en) * 2006-07-17 2010-09-23 David Vincent Bucci Repair process for coated articles
US20080011813A1 (en) * 2006-07-17 2008-01-17 David Vincent Bucci Repair process for coated articles
US7771171B2 (en) * 2006-12-14 2010-08-10 General Electric Company Systems for preventing wear on turbine blade tip shrouds
US20110180199A1 (en) * 2007-04-17 2011-07-28 United Technologies Corporation Powder -metallurgy braze preform and method of use
EP2456957B1 (de) 2009-07-22 2016-05-04 MTU Aero Engines GmbH Verfahren zur beschichtung von turbinenschaufel
US8573949B2 (en) * 2009-09-30 2013-11-05 General Electric Company Method and system for focused energy brazing
US8652650B2 (en) * 2009-10-22 2014-02-18 Honeywell International Inc. Platinum-modified nickel-based superalloys, methods of repairing turbine engine components, and turbine engine components
US8708655B2 (en) 2010-09-24 2014-04-29 United Technologies Corporation Blade for a gas turbine engine
DE102011086524A1 (de) * 2011-11-17 2013-05-23 Mtu Aero Engines Gmbh Panzerung von Dichtfins von TiAl-Schaufeln durch induktives Auftragslöten von Hartstoffpartikeln
DE102011087158A1 (de) * 2011-11-25 2013-05-29 Mtu Aero Engines Gmbh Verfahren zur Panzerung der Z-Notch von TiAl-Schaufeln
US9056443B2 (en) * 2013-02-04 2015-06-16 General Electric Company Brazing process, braze arrangement, and brazed article
US9862029B2 (en) 2013-03-15 2018-01-09 Kennametal Inc Methods of making metal matrix composite and alloy articles
US9346101B2 (en) 2013-03-15 2016-05-24 Kennametal Inc. Cladded articles and methods of making the same
DE102014204527A1 (de) * 2014-03-12 2015-09-17 Siemens Aktiengesellschaft Lötverfahren mit Couponfixierung zum Reparieren eines Turbinenbauteils
DE102014224156B4 (de) * 2014-11-26 2024-05-23 MTU Aero Engines AG Lötverfahren zur Panzerung der Z-Notch von TIAL-Schaufeln und Bauteil einer Strömungsmaschine mit einer solchen Panzerung
EP3216554B1 (de) * 2016-03-09 2020-05-06 MTU Aero Engines GmbH Bauteil mit verschleissgeschützten öffnungen und vertiefungen sowie verfahren zur herstellung derselben
US11117208B2 (en) * 2017-03-21 2021-09-14 Kennametal Inc. Imparting wear resistance to superalloy articles
FR3079847B1 (fr) * 2018-04-10 2023-11-10 Safran Aircraft Engines Procede de fabrication d'un element aubage metallique d'une turbomachine d'aeronef

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4101715A (en) * 1977-06-09 1978-07-18 General Electric Company High integrity CoCrAl(Y) coated nickel-base superalloys
US4219592A (en) * 1977-07-11 1980-08-26 United Technologies Corporation Two-way surfacing process by fusion welding
US4198442A (en) * 1977-10-31 1980-04-15 Howmet Turbine Components Corporation Method for producing elevated temperature corrosion resistant articles
FR2511908A1 (fr) * 1981-08-26 1983-03-04 Snecma Procede de brasage-diffusion destine aux pieces en superalliages
US4726101A (en) * 1986-09-25 1988-02-23 United Technologies Corporation Turbine vane nozzle reclassification
US4861618A (en) * 1986-10-30 1989-08-29 United Technologies Corporation Thermal barrier coating system
GB2198667B (en) * 1986-12-20 1991-08-07 Refurbished Turbine Components Parts for and methods of repairing machines
FR2691658B1 (fr) * 1992-05-27 1994-07-22 Snecma Piece en superalliage comportant un apport et procede de realisation de l'apport.
DE4411680C1 (de) * 1994-04-05 1995-08-17 Mtu Muenchen Gmbh Verfahren zur Reparatur von Fehlstellen in Bauteiloberflächen

Also Published As

Publication number Publication date
ZA972245B (en) 1997-09-17
US5890274A (en) 1999-04-06
CA2199691A1 (fr) 1997-09-14
FR2746043B1 (fr) 1998-04-17
DE69710622T2 (de) 2002-09-12
FR2746043A1 (fr) 1997-09-19
EP0795377A1 (de) 1997-09-17
CA2199691C (fr) 2002-11-19
EP0795377B1 (de) 2002-02-27

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: SNECMA, PARIS, FR