FR2557148B1 - Procede pour augmenter la forgeabilite d'un article en superalliage a base de nickel - Google Patents

Procede pour augmenter la forgeabilite d'un article en superalliage a base de nickel

Info

Publication number
FR2557148B1
FR2557148B1 FR848419770A FR8419770A FR2557148B1 FR 2557148 B1 FR2557148 B1 FR 2557148B1 FR 848419770 A FR848419770 A FR 848419770A FR 8419770 A FR8419770 A FR 8419770A FR 2557148 B1 FR2557148 B1 FR 2557148B1
Authority
FR
France
Prior art keywords
forgeability
nickel
increasing
based superalloy
superalloy article
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
FR848419770A
Other languages
English (en)
Other versions
FR2557148A1 (fr
Inventor
Paul D Genereux
Daniel F Paulonis
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.)
Raytheon Technologies Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of FR2557148A1 publication Critical patent/FR2557148A1/fr
Application granted granted Critical
Publication of FR2557148B1 publication Critical patent/FR2557148B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/10Changing 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

Landscapes

  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Forging (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Manufacture And Refinement Of Metals (AREA)
  • Inorganic Fibers (AREA)
  • Chemically Coating (AREA)
FR848419770A 1983-12-27 1984-12-24 Procede pour augmenter la forgeabilite d'un article en superalliage a base de nickel Expired - Lifetime FR2557148B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/565,490 US4574015A (en) 1983-12-27 1983-12-27 Nickle base superalloy articles and method for making

Publications (2)

Publication Number Publication Date
FR2557148A1 FR2557148A1 (fr) 1985-06-28
FR2557148B1 true FR2557148B1 (fr) 1992-09-11

Family

ID=24258841

Family Applications (1)

Application Number Title Priority Date Filing Date
FR848419770A Expired - Lifetime FR2557148B1 (fr) 1983-12-27 1984-12-24 Procede pour augmenter la forgeabilite d'un article en superalliage a base de nickel

Country Status (15)

Country Link
US (1) US4574015A (fr)
JP (1) JPS60228659A (fr)
AT (1) AT393842B (fr)
AU (1) AU568895B2 (fr)
BE (1) BE901393A (fr)
BR (1) BR8406657A (fr)
CA (1) CA1231632A (fr)
DD (2) DD232071A5 (fr)
DE (1) DE3445767A1 (fr)
FR (1) FR2557148B1 (fr)
GB (1) GB2152076B (fr)
IL (1) IL73866A (fr)
IT (1) IT1179547B (fr)
NO (1) NO163022C (fr)
SE (1) SE8406562L (fr)

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AU590838B2 (en) * 1986-06-02 1989-11-16 United Technologies Corporation Nickel base superalloy articles and method for making
US4769087A (en) * 1986-06-02 1988-09-06 United Technologies Corporation Nickel base superalloy articles and method for making
US4816084A (en) * 1986-09-15 1989-03-28 General Electric Company Method of forming fatigue crack resistant nickel base superalloys
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US4803880A (en) * 1987-12-21 1989-02-14 United Technologies Corporation Hollow article forging process
US4957567A (en) * 1988-12-13 1990-09-18 General Electric Company Fatigue crack growth resistant nickel-base article and alloy and method for making
US5120373A (en) * 1991-04-15 1992-06-09 United Technologies Corporation Superalloy forging process
US5693159A (en) * 1991-04-15 1997-12-02 United Technologies Corporation Superalloy forging process
DE69218089T2 (de) * 1991-04-15 1997-06-19 United Technologies Corp Schmiedeverfahren für Superlegierungen und verwandte Zusammensetzung
US5938863A (en) * 1996-12-17 1999-08-17 United Technologies Corporation Low cycle fatigue strength nickel base superalloys
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DE10100790C2 (de) * 2001-01-10 2003-07-03 Mtu Aero Engines Gmbh Nickel-Basislegierung für die gießtechnische Herstellung einkristallin erstarrter Bauteile
WO2002092260A1 (fr) 2001-05-15 2002-11-21 Santoku America, Inc. Moulages par coulee d'alliages au moyen de moules en graphite isotrope
AU2002311959A1 (en) 2001-05-23 2002-12-03 Santoku America, Inc. Castings of metallic alloys fabricated in anisotropic pyrolytic graphite molds under vacuum
US6755239B2 (en) 2001-06-11 2004-06-29 Santoku America, Inc. Centrifugal casting of titanium alloys with improved surface quality, structural integrity and mechanical properties in isotropic graphite molds under vacuum
US6634413B2 (en) 2001-06-11 2003-10-21 Santoku America, Inc. Centrifugal casting of nickel base superalloys in isotropic graphite molds under vacuum
US6799627B2 (en) 2002-06-10 2004-10-05 Santoku America, Inc. Castings of metallic alloys with improved surface quality, structural integrity and mechanical properties fabricated in titanium carbide coated graphite molds under vacuum
EP1428897A1 (fr) * 2002-12-10 2004-06-16 Siemens Aktiengesellschaft Méthode de fabrication d'un composant en alliage à soudabilité et/ou formabilité améliorée
US6986381B2 (en) * 2003-07-23 2006-01-17 Santoku America, Inc. Castings of metallic alloys with improved surface quality, structural integrity and mechanical properties fabricated in refractory metals and refractory metal carbides coated graphite molds under vacuum
US7708846B2 (en) * 2005-11-28 2010-05-04 United Technologies Corporation Superalloy stabilization
DE602006017324D1 (de) * 2005-12-21 2010-11-18 Gen Electric Zusammensetzung einer Nickel-Basis-Superlegierung
EP1900839B1 (fr) 2006-09-07 2013-11-06 Alstom Technology Ltd Procédé pour le traitement thermique de superalliages à base de Ni
US7740724B2 (en) * 2006-10-18 2010-06-22 United Technologies Corporation Method for preventing formation of cellular gamma prime in cast nickel superalloys
EP2602336B1 (fr) 2010-11-10 2014-12-17 Honda Motor Co., Ltd. Alliage de nickel
RU2566697C2 (ru) * 2011-04-13 2015-10-27 Роллс-Ройс Корпорейшн Граничный барьерный для диффузии слой, включающий в себя иридий, на металлической подложке
CN102312118B (zh) * 2011-09-21 2013-04-03 北京科技大学 一种gh864镍基高温合金组织精确控制的热加工方法
CH705750A1 (de) * 2011-10-31 2013-05-15 Alstom Technology Ltd Verfahren zur Herstellung von Komponenten oder Abschnitten, die aus einer Hochtemperatur-Superlegierung bestehen.
EP2778241B1 (fr) * 2011-12-15 2017-08-30 National Institute for Materials Science Superalliage à base de nickel à haute résistance
JP5652730B1 (ja) 2013-03-28 2015-01-14 日立金属株式会社 Ni基超耐熱合金及びその製造方法
WO2015008343A1 (fr) 2013-07-17 2015-01-22 三菱日立パワーシステムズ株式会社 PRODUIT D'ALLIAGE À BASE DE Ni ET SON PROCÉDÉ DE PRODUCTION, ET ÉLÉMENT D'ALLIAGE À BASE DE Ni ET SON PROCÉDÉ DE PRODUCTION
GB201400352D0 (en) * 2014-01-09 2014-02-26 Rolls Royce Plc A nickel based alloy composition
EP2918705B1 (fr) 2014-03-12 2017-05-03 Rolls-Royce Corporation Revêtement comprenant une couche barrière de diffusion comprenant iridium et une couche d'oxyde et procédé de revêtement
JP5869624B2 (ja) 2014-06-18 2016-02-24 三菱日立パワーシステムズ株式会社 Ni基合金軟化材及びNi基合金部材の製造方法
EP3042973B1 (fr) 2015-01-07 2017-08-16 Rolls-Royce plc Alliage de nickel
GB2539957B (en) 2015-07-03 2017-12-27 Rolls Royce Plc A nickel-base superalloy
US10301711B2 (en) * 2015-09-28 2019-05-28 United Technologies Corporation Nickel based superalloy with high volume fraction of precipitate phase
US10184166B2 (en) 2016-06-30 2019-01-22 General Electric Company Methods for preparing superalloy articles and related articles
US10640858B2 (en) * 2016-06-30 2020-05-05 General Electric Company Methods for preparing superalloy articles and related articles
US20180051360A1 (en) * 2016-08-16 2018-02-22 United Technologies Corporation Formable Superalloy Single Crystal Composition
JP6809169B2 (ja) 2016-11-28 2021-01-06 大同特殊鋼株式会社 Ni基超合金素材の製造方法
JP6793689B2 (ja) * 2017-08-10 2020-12-02 三菱パワー株式会社 Ni基合金部材の製造方法
JP6942871B2 (ja) * 2017-11-17 2021-09-29 三菱パワー株式会社 Ni基鍛造合金材の製造方法
CN113106299B (zh) * 2017-11-17 2022-07-05 三菱重工业株式会社 Ni基锻造合金材料的制造方法
GB2571280A (en) * 2018-02-22 2019-08-28 Rolls Royce Plc Method of manufacture
US11306595B2 (en) 2018-09-14 2022-04-19 Raytheon Technologies Corporation Wrought root blade manufacture methods
US11098395B2 (en) * 2019-12-18 2021-08-24 General Electric Company Nickel-based superalloy with microstructure including rafting-resistant gamma prime phase and article prepared therefrom
CN112746231B (zh) * 2020-12-29 2021-10-15 北京钢研高纳科技股份有限公司 一种高性能高温合金的γ'相预调增塑的生产工艺
CN113789490B (zh) * 2021-08-26 2022-07-26 飞而康快速制造科技有限责任公司 一种增材制造用gh4169镍基高温合金及其热处理方法
CN115110013B (zh) * 2022-06-13 2023-04-25 大冶特殊钢有限公司 一种改善高温合金锻材全截面晶粒度均匀性的固溶处理方法

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US2798872A (en) * 1954-12-30 1957-07-09 Monsanto Chemicals Xanthine hydrobromides
US3519503A (en) * 1967-12-22 1970-07-07 United Aircraft Corp Fabrication method for the high temperature alloys
GB1253755A (en) * 1968-07-19 1971-11-17 United Aircraft Corp Method to improve the weldability and formability of nickel-base superalloys by heat treatment
US3649379A (en) * 1969-06-20 1972-03-14 Cabot Corp Co-precipitation-strengthened nickel base alloys and method for producing same
IL34792A (en) * 1969-07-14 1973-03-30 Martin Marietta Corp Heat treatable alloy
BE756652A (fr) * 1969-09-26 1971-03-01 United Aircraft Corp Superalliages contenant des phases precipitees topologiquement d'assemblage serre
BE756653A (fr) * 1969-09-26 1971-03-01 United Aircraft Corp Accroissement thermo-mecanique de la resistance des superalliages (
US3677830A (en) * 1970-02-26 1972-07-18 United Aircraft Corp Processing of the precipitation hardening nickel-base superalloys
US3676225A (en) * 1970-06-25 1972-07-11 United Aircraft Corp Thermomechanical processing of intermediate service temperature nickel-base superalloys
GB1376846A (en) * 1972-01-27 1974-12-11 Martin Marietta Corp Heat treatable alloy
US3753790A (en) * 1972-08-02 1973-08-21 Gen Electric Heat treatment to dissolve low melting phases in superalloys
US4328045A (en) * 1978-12-26 1982-05-04 United Technologies Corporation Heat treated single crystal articles and process
US4253884A (en) * 1979-08-29 1981-03-03 Special Metals Corporation Treating nickel base alloys

Also Published As

Publication number Publication date
AU3680484A (en) 1985-07-04
DE3445767C2 (fr) 1989-10-19
BE901393A (fr) 1985-04-16
NO845119L (no) 1985-06-28
NO163022B (no) 1989-12-11
FR2557148A1 (fr) 1985-06-28
US4574015A (en) 1986-03-04
GB2152076B (en) 1987-08-19
IT1179547B (it) 1987-09-16
IL73866A (en) 1987-07-31
GB2152076A (en) 1985-07-31
BR8406657A (pt) 1985-10-22
SE8406562D0 (sv) 1984-12-21
IT8424264A0 (it) 1984-12-27
NO163022C (no) 1990-03-21
JPS60228659A (ja) 1985-11-13
CA1231632A (fr) 1988-01-19
AU568895B2 (en) 1988-01-14
JPS6339662B2 (fr) 1988-08-05
DD243880A5 (de) 1987-03-18
AT393842B (de) 1991-12-27
IL73866A0 (en) 1985-03-31
IT8424264A1 (it) 1986-06-27
SE8406562L (sv) 1985-06-28
DE3445767A1 (de) 1985-07-04
DD232071A5 (de) 1986-01-15
GB8431279D0 (en) 1985-01-23
ATA411284A (de) 1991-06-15

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