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ES2144710T3 - Procedimiento de ensamblaje por sinterizacion reactiva de piezas de material intermetalico y aplicaciones derivadas. - Google Patents

Procedimiento de ensamblaje por sinterizacion reactiva de piezas de material intermetalico y aplicaciones derivadas.

Info

Publication number
ES2144710T3
ES2144710T3 ES96402107T ES96402107T ES2144710T3 ES 2144710 T3 ES2144710 T3 ES 2144710T3 ES 96402107 T ES96402107 T ES 96402107T ES 96402107 T ES96402107 T ES 96402107T ES 2144710 T3 ES2144710 T3 ES 2144710T3
Authority
ES
Spain
Prior art keywords
piece
parts
assembly procedure
reactive sintering
section
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
ES96402107T
Other languages
English (en)
Inventor
Yves Bigay
Alain Lasalmonie
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
Commissariat a lEnergie Atomique et aux Energies Alternatives CEA
Original Assignee
Commissariat a lEnergie Atomique CEA
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
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 Commissariat a lEnergie Atomique CEA, Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Commissariat a lEnergie Atomique CEA
Application granted granted Critical
Publication of ES2144710T3 publication Critical patent/ES2144710T3/es
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
    • 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
    • B23K20/00—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
    • B23K20/16—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating with interposition of special material to facilitate connection of the parts, e.g. material for absorbing or producing gas
    • 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
    • B23K35/001—Interlayers, transition pieces for metallurgical bonding of workpieces
    • B23K35/004—Interlayers, transition pieces for metallurgical bonding of workpieces at least one of the workpieces being of a metal of the iron group
    • 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
    • B23K35/001—Interlayers, transition pieces for metallurgical bonding of workpieces
    • B23K35/005—Interlayers, transition pieces for metallurgical bonding of workpieces at least one of the workpieces being of a refractory metal
    • 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
    • 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
    • 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
    • B23K35/22—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by the composition or nature of the material
    • B23K35/24—Selection of soldering or welding materials proper
    • B23K35/30—Selection of soldering or welding materials proper with the principal constituent melting at less than 1550 degrees C
    • B23K35/3033—Ni as the principal constituent
    • 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
    • B23K35/22—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by the composition or nature of the material
    • B23K35/24—Selection of soldering or welding materials proper
    • B23K35/30—Selection of soldering or welding materials proper with the principal constituent melting at less than 1550 degrees C
    • B23K35/3053—Fe as the principal constituent
    • B23K35/3093—Fe as the principal constituent with other elements as next major constituents
    • 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
    • B23K35/22—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by the composition or nature of the material
    • B23K35/24—Selection of soldering or welding materials proper
    • B23K35/32—Selection of soldering or welding materials proper with the principal constituent melting at more than 1550 degrees C
    • B23K35/325—Ti as the principal constituent

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Powder Metallurgy (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)

Abstract

UN PROCEDIMIENTO DE ENSAMBLAJE DE DOS ELEMENTOS QUE COMPRENDEN AL MENOS UN MATERIAL INTERMETALICO QUE LLEVA LAS SIGUIENTES ETAPAS: - MEZCLA DE POLVOS ELEMENTALES DE UN COMPUESTO INTERMETALICO DEL MISMO TIPO QUE DICHO MATERIAL A ENSAMBLAR, COMPACTACION Y CONFORMACION DE UN ELEMENTO INTERMEDIARIO A PARTIR DE DICHO COMPUESTO, A UNA TEMPERATURA INFERIOR A LA DE SINTERIZACION REACTIVA DEL COMPUESTO. - COLOCACION DEL ELEMENTO INTERMEDIO ENTRE LAS SUPERFICIES A ENSAMBLAR, - TRATAMIENTO TERMICO SEGUN UN PRIMER CICLO TERMICO ADAPTADO AL COMPUESTO INTERMETALICO PARA OBTENER UNA SINTERIZACION REACTIVA DEL ELEMENTO INTERMEDIO Y UNA CONSOLIDACION DEL ENSAMBLAJE. TRATAMIENTO DE DIFUSION SEGUN UN SEGUNDO CICLO TERMICO, A UNA TEMPERATURA SUPERIOR A 0,8 VECES LA TEMPERATURA DE FUSION DEL COMPUESTO PARA CONSOLIDAR MECANICAMENTE EL ENSAMBLAJE. EL PROCEDIMIENTO SE UTILIZA TAMBIEN PARA LA REALIZACION DE UN REVESTIMIENTO O PARA UNA REPARACION POR APORTACION DE MATERIA.
ES96402107T 1995-10-04 1996-10-03 Procedimiento de ensamblaje por sinterizacion reactiva de piezas de material intermetalico y aplicaciones derivadas. Expired - Lifetime ES2144710T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9511650A FR2739583B1 (fr) 1995-10-04 1995-10-04 Procede d'assemblage par frittage reactif de pieces en materiau intermetallique et applications derivees

Publications (1)

Publication Number Publication Date
ES2144710T3 true ES2144710T3 (es) 2000-06-16

Family

ID=9483217

Family Applications (1)

Application Number Title Priority Date Filing Date
ES96402107T Expired - Lifetime ES2144710T3 (es) 1995-10-04 1996-10-03 Procedimiento de ensamblaje por sinterizacion reactiva de piezas de material intermetalico y aplicaciones derivadas.

Country Status (8)

Country Link
US (1) US5788142A (es)
EP (1) EP0767028B1 (es)
JP (1) JP3267874B2 (es)
AT (1) ATE188409T1 (es)
CA (1) CA2186989C (es)
DE (1) DE69606001T2 (es)
ES (1) ES2144710T3 (es)
FR (1) FR2739583B1 (es)

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* Cited by examiner, † Cited by third party
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US6551551B1 (en) 2001-11-16 2003-04-22 Caterpillar Inc Sinter bonding using a bonding agent
US6805971B2 (en) 2002-05-02 2004-10-19 George E. Talia Method of making coatings comprising an intermetallic compound and coatings made therewith
DE10261073A1 (de) 2002-12-24 2004-07-08 Rolls-Royce Deutschland Ltd & Co Kg Verfahren zum Fügen von Werkstücken aus Titanaluminid mittels eines Lötverfahrens
US7241416B2 (en) * 2003-08-12 2007-07-10 Borg Warner Inc. Metal injection molded turbine rotor and metal injection molded shaft connection attachment thereto
US7052241B2 (en) * 2003-08-12 2006-05-30 Borgwarner Inc. Metal injection molded turbine rotor and metal shaft connection attachment thereto
GB0701904D0 (en) 2007-02-01 2007-03-14 Rolls Royce Plc A method of manufacturing a component by consolidating powder material
US20090113706A1 (en) * 2007-11-06 2009-05-07 General Electric Company Craze crack repair of combustor liners
JP2010163889A (ja) * 2009-01-13 2010-07-29 Ihi Corp チタニウム−アルミニウム金属間化合物よりなる低圧タービン部品の修復方法および修復された低圧タービン部品
GB0913887D0 (en) * 2009-08-10 2009-09-16 A method of joining components
GB0913924D0 (en) * 2009-08-11 2009-09-16 Rolls Royce Plc Developments in or relating to drum rotors
US8230899B2 (en) * 2010-02-05 2012-07-31 Ati Properties, Inc. Systems and methods for forming and processing alloy ingots
US9267184B2 (en) 2010-02-05 2016-02-23 Ati Properties, Inc. Systems and methods for processing alloy ingots
US10207312B2 (en) 2010-06-14 2019-02-19 Ati Properties Llc Lubrication processes for enhanced forgeability
US8789254B2 (en) 2011-01-17 2014-07-29 Ati Properties, Inc. Modifying hot workability of metal alloys via surface coating
US9283621B2 (en) 2012-06-21 2016-03-15 Deere & Company Method for forming a composite article
US9539636B2 (en) 2013-03-15 2017-01-10 Ati Properties Llc Articles, systems, and methods for forging alloys
US9027374B2 (en) 2013-03-15 2015-05-12 Ati Properties, Inc. Methods to improve hot workability of metal alloys
CN106808079B (zh) * 2017-01-11 2021-01-01 西北工业大学 一种TiAl合金与Ti2AlNb合金的扩散连接方法
CN110625223B (zh) * 2019-08-30 2021-05-07 中国航发北京航空材料研究院 一种用于TiAl基铸件铸造缺陷的氩弧焊修补方法
CN114619035B (zh) * 2022-03-18 2023-12-08 湖南湘投轻材科技股份有限公司 异体分陶瓷增强铝基材料预制件冶金结合方法

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB955675A (en) * 1959-06-30 1964-04-15 Commw Scient Ind Res Org Improvements in or relating to compacts and seals
US3335002A (en) * 1965-10-13 1967-08-08 Texas Instruments Inc Manufacture of alloy foils
US3716347A (en) * 1970-09-21 1973-02-13 Minnesota Mining & Mfg Metal parts joined with sintered powdered metal
US4294615A (en) * 1979-07-25 1981-10-13 United Technologies Corporation Titanium alloys of the TiAl type
DE3316807A1 (de) * 1983-05-07 1984-11-08 Robert Bosch Gmbh, 7000 Stuttgart Hartlot-legierung zum verbinden von oxidkeramiken unter sich oder mit metallen
EP0155490B1 (de) * 1984-02-23 1988-04-06 BBC Brown Boveri AG Verfahren zum Verbinden von Teil-Werkstücken aus einer Superlegierung nach dem Diffusions-Fügeprocess
US5040718A (en) * 1987-10-16 1991-08-20 Avco Corporation Method of repairing damages in superalloys
US5318214A (en) * 1987-11-18 1994-06-07 The United States Of America As Represented By The Secretary Of The Air Force Activated brazing system for joining titanium aluminide
JP3259959B2 (ja) * 1990-05-29 2002-02-25 日本発条株式会社 複合材とその製造方法
US5564620A (en) * 1993-10-22 1996-10-15 Rawers; James C. Forming metal-intermetallic or metal-ceramic composites by self-propagating high-temperature reactions
JP3250582B2 (ja) * 1993-10-28 2002-01-28 アイシン精機株式会社 Ｔｉ−Ａｌ系金属間化合物の接合方法

Also Published As

Publication number Publication date
CA2186989A1 (fr) 1997-04-05
EP0767028A1 (fr) 1997-04-09
DE69606001D1 (de) 2000-02-10
FR2739583A1 (fr) 1997-04-11
FR2739583B1 (fr) 1997-12-12
US5788142A (en) 1998-08-04
JP3267874B2 (ja) 2002-03-25
JPH09164490A (ja) 1997-06-24
DE69606001T2 (de) 2000-06-08
CA2186989C (fr) 2003-01-14
ATE188409T1 (de) 2000-01-15
EP0767028B1 (fr) 2000-01-05

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