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WO2010089516A3 - Method for producing a piece made from a superalloy based on nickel and corresponding piece - Google Patents

Method for producing a piece made from a superalloy based on nickel and corresponding piece Download PDF

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Publication number
WO2010089516A3
WO2010089516A3 PCT/FR2010/050191 FR2010050191W WO2010089516A3 WO 2010089516 A3 WO2010089516 A3 WO 2010089516A3 FR 2010050191 W FR2010050191 W FR 2010050191W WO 2010089516 A3 WO2010089516 A3 WO 2010089516A3
Authority
WO
WIPO (PCT)
Prior art keywords
piece
producing
nickel
superalloy
superalloy based
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.)
Ceased
Application number
PCT/FR2010/050191
Other languages
French (fr)
Other versions
WO2010089516A2 (en
Inventor
Alexandre Devaux
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.)
Aubert and Duval SA
Safran Aircraft Engines SAS
Safran Helicopter Engines SAS
Original Assignee
Aubert and Duval SA
Turbomeca SA
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 Aubert and Duval SA, Turbomeca SA, SNECMA SAS filed Critical Aubert and Duval SA
Priority to RU2011136846/02A priority Critical patent/RU2531217C2/en
Priority to CN201080015088.4A priority patent/CN102439191B/en
Priority to PL10708291T priority patent/PL2393951T3/en
Priority to JP2011548756A priority patent/JP2012517524A/en
Priority to BRPI1005418A priority patent/BRPI1005418A2/en
Priority to CA2751681A priority patent/CA2751681A1/en
Priority to US13/148,298 priority patent/US20120037280A1/en
Priority to EP10708291.9A priority patent/EP2393951B1/en
Publication of WO2010089516A2 publication Critical patent/WO2010089516A2/en
Publication of WO2010089516A3 publication Critical patent/WO2010089516A3/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • 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
    • 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
    • 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
    • C22C19/055—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 20% but less than 30%

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Powder Metallurgy (AREA)
  • Heat Treatment Of Nonferrous Metals Or Alloys (AREA)
  • Heat Treatment Of Articles (AREA)

Abstract

The invention relates to a method for producing a blank for a piece made from a superalloy based on Ni, wherein an alloy is produced and thermal treatments are carried out, characterised in that: said superalloy contains at least 2.5% of the total as Nb and Ta, a thermal treatment is carried out in a number of steps, a first step between 850 and 1,0000C for at least 20 minutes to precipitate the phase δ on the grain joints, a second step at a temperature above that of the first step, permitting a partial dissolution of the phase δ obtained in the first step, an aging treatment comprising a third step and optionally one or more supplementary steps at a temperature mower than that of the first step and which permit a precipitation of the hardening phases γ' and γ". The invention further relates to a corresponding piece.
PCT/FR2010/050191 2009-02-06 2010-02-05 Method for producing a piece made from a superalloy based on nickel and corresponding piece Ceased WO2010089516A2 (en)

Priority Applications (8)

Application Number Priority Date Filing Date Title
RU2011136846/02A RU2531217C2 (en) 2009-02-06 2010-02-05 Method of manufacture of detail from nickel-based superalloy and detail obtained by named method
CN201080015088.4A CN102439191B (en) 2009-02-06 2010-02-05 Method for producing a piece made from a superalloy based on nickel and corresponding piece
PL10708291T PL2393951T3 (en) 2009-02-06 2010-02-05 Method for producing a piece made from a superalloy based on nickel and corresponding piece
JP2011548756A JP2012517524A (en) 2009-02-06 2010-02-05 Method for manufacturing parts made from nickel-based superalloys and corresponding parts
BRPI1005418A BRPI1005418A2 (en) 2009-02-06 2010-02-05 process of making a sketch of superalloy part and nickel based superalloy part
CA2751681A CA2751681A1 (en) 2009-02-06 2010-02-05 Method for producing a piece made from a superalloy based on nickel and corresponding piece
US13/148,298 US20120037280A1 (en) 2009-02-06 2010-02-05 Method for producing a part made from a superalloy based on nickel and corresponding part
EP10708291.9A EP2393951B1 (en) 2009-02-06 2010-02-05 Method for producing a piece made from a superalloy based on nickel and corresponding piece

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0950767A FR2941962B1 (en) 2009-02-06 2009-02-06 PROCESS FOR MANUFACTURING A NICKEL-BASED SUPERALLIANCE WORKPIECE, AND A PRODUCT OBTAINED THEREBY
FR0950767 2009-02-06

Publications (2)

Publication Number Publication Date
WO2010089516A2 WO2010089516A2 (en) 2010-08-12
WO2010089516A3 true WO2010089516A3 (en) 2010-10-21

Family

ID=41092077

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/FR2010/050191 Ceased WO2010089516A2 (en) 2009-02-06 2010-02-05 Method for producing a piece made from a superalloy based on nickel and corresponding piece

Country Status (10)

Country Link
US (1) US20120037280A1 (en)
EP (1) EP2393951B1 (en)
JP (1) JP2012517524A (en)
CN (1) CN102439191B (en)
BR (1) BRPI1005418A2 (en)
CA (1) CA2751681A1 (en)
FR (1) FR2941962B1 (en)
PL (1) PL2393951T3 (en)
RU (1) RU2531217C2 (en)
WO (1) WO2010089516A2 (en)

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US7985304B2 (en) * 2007-04-19 2011-07-26 Ati Properties, Inc. Nickel-base alloys and articles made therefrom
US20130133793A1 (en) * 2011-11-30 2013-05-30 Ati Properties, Inc. Nickel-base alloy heat treatments, nickel-base alloys, and articles including nickel-base alloys
JP2014051698A (en) * 2012-09-06 2014-03-20 Hitachi Ltd Ni-BASED FORGING ALLOY, AND GAS TURBINE USING THE SAME
JP6148843B2 (en) * 2012-10-02 2017-06-14 三菱日立パワーシステムズ株式会社 Large cast member made of nickel base alloy and method for producing the same
JP6079294B2 (en) * 2013-02-22 2017-02-15 大同特殊鋼株式会社 Free forging method of Ni-base heat-resistant alloy member
JP6315319B2 (en) * 2013-04-19 2018-04-25 日立金属株式会社 Method for producing Fe-Ni base superalloy
WO2015151318A1 (en) * 2014-03-31 2015-10-08 日立金属株式会社 METHOD FOR PRODUCING Fe-Ni-BASED SUPER HEAT-RESISTANT ALLOY
CN104805259A (en) * 2015-04-22 2015-07-29 绍兴文理学院 Nickel base alloy composition matching and delta-phase spheroidizing heat treatment process
US10563293B2 (en) 2015-12-07 2020-02-18 Ati Properties Llc Methods for processing nickel-base alloys
CN105506390B (en) * 2015-12-30 2017-06-23 钢铁研究总院 A kind of nickel base superalloy containing zirconium and preparation method
US10640858B2 (en) 2016-06-30 2020-05-05 General Electric Company Methods for preparing superalloy articles and related articles
US10184166B2 (en) 2016-06-30 2019-01-22 General Electric Company Methods for preparing superalloy articles and related articles
JP6793689B2 (en) * 2017-08-10 2020-12-02 三菱パワー株式会社 Manufacturing method of Ni-based alloy member
EP3611280B1 (en) * 2017-11-17 2022-07-13 Mitsubishi Heavy Industries, Ltd. Ni-based wrought alloy material, high-temperature turbine member using same, and method of manufacturing same
JP7228124B2 (en) * 2018-10-02 2023-02-24 大同特殊鋼株式会社 Method for manufacturing hot worked material
DE102020106433A1 (en) * 2019-03-18 2020-09-24 Vdm Metals International Gmbh Nickel alloy with good corrosion resistance and high tensile strength as well as a process for the production of semi-finished products
CN111575619B (en) * 2020-05-29 2021-04-27 北京科技大学 A method for rapid elimination of dendrite segregation in deformed superalloy ingots by pulsed current
US11921046B2 (en) 2020-08-31 2024-03-05 Honeywell International Inc. Filter media and system using the same
CN112705700B (en) * 2020-12-18 2022-02-08 山东大学 Method for improving high-temperature strength of Inconel 718 laser deposition layer
CN115261753B (en) * 2021-04-29 2025-02-14 中国科学院金属研究所 A hot working method for producing high uniformity ultrafine-grained nickel-based high-temperature alloy
JP7339412B2 (en) * 2021-10-25 2023-09-05 山陽特殊製鋼株式会社 Ni-based alloy powder for additive manufacturing and additive manufacturing
WO2023074613A1 (en) * 2021-10-25 2023-05-04 山陽特殊製鋼株式会社 Ni alloy powder suited to additive manufacturing and additively manufactured article obtained using same
CN115011825B (en) * 2022-08-09 2022-11-22 无锡凯斯特铸业有限公司 0Cr20Ni55Mo3Nb5Ti nickel-based alloy forming method
CN115635027B (en) * 2022-11-03 2025-07-22 豪梅特航空机件(苏州)有限公司 Method for solving In718plus punching cracking
CN116657067B (en) * 2023-06-01 2025-07-04 中南大学 Heat treatment method for uniformly refining mixed crystal structure of GH4169 alloy forging and regulating delta phase content
CN117467868A (en) * 2023-09-19 2024-01-30 中国科学院金属研究所 A high-strength, oxygen-rich ablation-resistant nickel-based high-temperature alloy and its preparation method

Citations (6)

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US4459160A (en) * 1980-03-13 1984-07-10 Rolls-Royce Limited Single crystal castings
US5059257A (en) * 1989-06-09 1991-10-22 Carpenter Technology Corporation Heat treatment of precipitation hardenable nickel and nickel-iron alloys
DE19617093A1 (en) * 1996-04-29 1997-10-30 Abb Research Ltd Heat treatment process for material bodies made of nickel-based superalloys
WO2000003053A1 (en) * 1998-07-09 2000-01-20 Inco Alloys International, Inc. Heat treatment for nickel-base alloys
US20030034098A1 (en) * 2001-04-24 2003-02-20 General Electric Company Nickel-base superalloys and articles formed therefrom
EP1398393A1 (en) * 2002-09-16 2004-03-17 ALSTOM (Switzerland) Ltd Property recovering method

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US4459160A (en) * 1980-03-13 1984-07-10 Rolls-Royce Limited Single crystal castings
US5059257A (en) * 1989-06-09 1991-10-22 Carpenter Technology Corporation Heat treatment of precipitation hardenable nickel and nickel-iron alloys
DE19617093A1 (en) * 1996-04-29 1997-10-30 Abb Research Ltd Heat treatment process for material bodies made of nickel-based superalloys
WO2000003053A1 (en) * 1998-07-09 2000-01-20 Inco Alloys International, Inc. Heat treatment for nickel-base alloys
US20030034098A1 (en) * 2001-04-24 2003-02-20 General Electric Company Nickel-base superalloys and articles formed therefrom
EP1398393A1 (en) * 2002-09-16 2004-03-17 ALSTOM (Switzerland) Ltd Property recovering method

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Title
DEVAUX A ET AL: "Gamma double prime precipitation kinetic in Alloy 718", MATERIALS SCIENCE AND ENGINEERING A: STRUCTURAL MATERIALS:PROPERTIES, MICROSTRUCTURE & PROCESSING, LAUSANNE, CH, vol. 486, no. 1-2, 15 July 2008 (2008-07-15), pages 117 - 122, XP022633343, ISSN: 0921-5093, [retrieved on 20080429] *
DONG, J. X. ET AL: "Microstructures and the structure stability of INCONEL 725, a new age-hardenable corrosion resistant superalloy", ACTA METALLURGICA SINICA (ENGLISH LETTERS) , 16(2), 145-150 CODEN: AMSIFZ; ISSN: 1006-7191, vol. 16, no. 2, April 2003 (2003-04-01), pages 145 - 150, XP002591337 *
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Also Published As

Publication number Publication date
US20120037280A1 (en) 2012-02-16
WO2010089516A2 (en) 2010-08-12
EP2393951A2 (en) 2011-12-14
JP2012517524A (en) 2012-08-02
CA2751681A1 (en) 2010-08-12
FR2941962B1 (en) 2013-05-31
BRPI1005418A2 (en) 2016-03-08
PL2393951T3 (en) 2021-10-04
RU2531217C2 (en) 2014-10-20
FR2941962A1 (en) 2010-08-13
CN102439191B (en) 2015-01-28
EP2393951B1 (en) 2021-06-16
CN102439191A (en) 2012-05-02
RU2011136846A (en) 2013-03-20

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