CA3048051C - Superalliage soudable a base de nickel a teneur elevee en gamma prime et procede de reparation et de fabrication de elements de moteur a turbine utilisant ledit superalliage - Google Patents

Superalliage soudable a base de nickel a teneur elevee en gamma prime et procede de reparation et de fabrication de elements de moteur a turbine utilisant ledit superalliage Download PDF

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CA3048051C
CA3048051C CA3048051A CA3048051A CA3048051C CA 3048051 C CA3048051 C CA 3048051C CA 3048051 A CA3048051 A CA 3048051A CA 3048051 A CA3048051 A CA 3048051A CA 3048051 C CA3048051 C CA 3048051C
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hours
per
welding
temperature
superalloy
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CA3048051A1 (fr
Inventor
Alexander Goncharov
Joseph Liburdi
Paul Lowden
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Liburdi Engineering Ltd
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Liburdi Engineering Ltd
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Classifications

    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C19/00—Alloys based on nickel or cobalt
    • C22C19/03—Alloys based on nickel or cobalt based on nickel
    • C22C19/05—Alloys based on nickel or cobalt based on nickel with chromium
    • C22C19/051—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
    • C22C19/057—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being less 10%
    • 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 or 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
    • B23K35/02—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape
    • B23K35/0255—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape for use in welding
    • B23K35/0261—Rods, electrodes or wires
    • 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°C
    • B23K35/3033—Ni as the principal constituent
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
    • B22F7/06—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools
    • B22F7/062—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools involving the connection or repairing of preformed parts
    • B22F2007/068—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools involving the connection or repairing of preformed parts repairing articles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F5/00—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
    • B22F5/009—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of turbine components other than turbine blades
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F5/00—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
    • B22F5/04—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of turbine blades
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B33—ADDITIVE MANUFACTURING TECHNOLOGY
    • B33Y—ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
    • B33Y80/00—Products made by additive manufacturing
    • 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
    • F05D2230/20—Manufacture essentially without removing material
    • F05D2230/23—Manufacture essentially without removing material by permanently joining parts together
    • F05D2230/232—Manufacture essentially without removing material by permanently joining parts together by welding
    • 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
    • F05D2240/00—Components
    • F05D2240/20—Rotors
    • F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
    • F05D2240/307—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor related to the tip of a rotor blade
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/10—Metals, alloys or intermetallic compounds
    • F05D2300/17—Alloys
    • F05D2300/175—Superalloys
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/70—Treatment or modification of materials
    • F05D2300/701—Heat treatment
    • 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

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

Selon l'invention, le superalliage à base de nickel à teneur élevée en gamma prime, comprenant 10 à 13 % en poids de Co, 3 à 10 % en poids de Cr, 0,5 à 2 % en poids de Mo, 3 à 7% en poids de W, 0,5 à 10 % en poids de Re, 5 à 6 % en poids de Al, 5 à 7 % en poids de Ta, 0,5 à 2 % en poids de Hf, 0,01 à 0,15 % en poids de C, 0,005 à 0,05 % en poids de B et 0,01 % en poids de Zr, a d'abord été décrit dans le brevet américain 4 169 742. Ultérieurement, la version optimisée de cet alliage comprenant 12 % en poids de Co, 6,8 % en poids de Cr, 1,5 % en poids de Mo, 4,9 % en poids de W, 2,8 % en poids de Re, 6,15 % en poids de Al, 6,35 % en poids de Ta, 1,5 % en poids de Hf, 0,12 % en poids de C, 0,015 % en poids de B et 0,02 % en poids de Zr est devenue connue en tant que superalliage Rene 142 ou R142. Ce dernier a été largement utilisé en tant que matériau de soudage et matériau structural pour une fabrication de pales de turbine à solidification directionnelle (DS) en raison d'une association unique de résistance à l'oxydation et de propriétés mécaniques élevées, qui ont été obtenues par l'optimisation de la teneur en Ta + Al + Cr couplée à l'absence d'ajout de titane et à une teneur élevée en aluminium associée au traitement thermique en plusieurs étapes spécial, auquel font référence Earl W. Ross et Kevin S. O'Hara dans "Rene 142: A high strength, oxidation resistant DS turbine airfoil alloy", Superalloys 1982, pp. 257 - 265. L'optimisation des propriétés de rupture de Rene 142 DS selon Earl W. Ross et Kevin S. O'Hara a été obtenue par une homogénéisation à 2335 °F pendant 2 heures suivi par un recuit à 2050 °F pendant 4 heures, un vieillissement primaire à 1975 °F pendant 4 heures et un vieillissement secondaire à 1650 °F pendant 4 heures (désigné sous le nom de R142 HT).
CA3048051A 2017-03-03 2017-03-03 Superalliage soudable a base de nickel a teneur elevee en gamma prime et procede de reparation et de fabrication de elements de moteur a turbine utilisant ledit superalliage Active CA3048051C (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/CA2017/050291 WO2018157228A1 (fr) 2017-03-03 2017-03-03 Superalliage soudable à base de nickel à teneur élevée en gamma prime et procédé de réparation et de fabrication de éléments de moteur à turbine utilisant ledit superalliage

Publications (2)

Publication Number Publication Date
CA3048051A1 CA3048051A1 (fr) 2018-09-07
CA3048051C true CA3048051C (fr) 2021-11-16

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CA3048051A Active CA3048051C (fr) 2017-03-03 2017-03-03 Superalliage soudable a base de nickel a teneur elevee en gamma prime et procede de reparation et de fabrication de elements de moteur a turbine utilisant ledit superalliage

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WO (1) WO2018157228A1 (fr)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102018218017A1 (de) * 2018-10-22 2020-04-23 Siemens Aktiengesellschaft Reparatur einer Schaufelspitze mittels Coupon und Turbinenschaufel
CN109465570B (zh) * 2018-12-13 2022-02-01 郑州机械研究所有限公司 一种Ti-Si高温钎料
FR3091708B1 (fr) 2019-01-16 2021-01-22 Safran Superalliage à base de nickel à faible densité et avec une tenue mécanique et environnementale élevée à haute température
CN113414519B (zh) * 2021-08-06 2022-11-29 四川大西洋焊接材料股份有限公司 交流用ENi6620镍基焊条及其制备方法与焊接方法
CN113814660A (zh) * 2021-09-23 2021-12-21 南通光明钼制品有限公司 一种金属钼端帽
CN114589429B (zh) * 2022-03-31 2022-08-30 广东省科学院中乌焊接研究所 一种用于叶轮增材修复的超级双相不锈钢药芯焊丝及其制备方法和应用
CN115488342B (zh) * 2022-08-31 2024-04-02 中国机械总院集团北京机电研究所有限公司 异种金属整体叶盘增等材短流程制备方法
CN117344187B (zh) * 2023-09-05 2025-10-17 东方电气集团东方汽轮机有限公司 薄壁贯穿性缺陷修复的活化剂、预制膏体、预制件及工艺
CN117488110A (zh) * 2023-09-27 2024-02-02 中国航发沈阳黎明航空发动机有限责任公司 一种精密电解静子叶片用优质gh4169合金型材设计方法

Family Cites Families (6)

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US5897801A (en) * 1997-01-22 1999-04-27 General Electric Company Welding of nickel-base superalloys having a nil-ductility range
US6054672A (en) * 1998-09-15 2000-04-25 Chromalloy Gas Turbine Corporation Laser welding superalloy articles
US6333484B1 (en) * 2000-03-17 2001-12-25 Chromalloy Gas Turbine Corporation Welding superalloy articles
JP4230970B2 (ja) * 2004-08-09 2009-02-25 株式会社日立製作所 凝固方向強度と結晶粒界強度の優れた一方向凝固用Ｎｉ基超合金、鋳造物およびガスタービン用高温部品
WO2014085892A1 (fr) * 2012-12-05 2014-06-12 Liburdi Engineering Limited Procédé de rechargement et de soudage par fusion de superalliages au moyen d'une poudre d'apport composite
ES2805796T3 (es) * 2013-12-24 2021-02-15 Liburdi Engineering Material de soldadura basado en níquel reforzado por precipitación para soldadura por fusión de superaleaciones

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WO2018157228A1 (fr) 2018-09-07
CA3048051A1 (fr) 2018-09-07

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