FR3073526B1 - Superalliage a base de nickel, aube monocristalline et turbomachine - Google Patents

Superalliage a base de nickel, aube monocristalline et turbomachine Download PDF

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Publication number
FR3073526B1
FR3073526B1 FR1760675A FR1760675A FR3073526B1 FR 3073526 B1 FR3073526 B1 FR 3073526B1 FR 1760675 A FR1760675 A FR 1760675A FR 1760675 A FR1760675 A FR 1760675A FR 3073526 B1 FR3073526 B1 FR 3073526B1
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FR
France
Prior art keywords
nickel
turbomachine
based superalloy
blade
crystalline
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.)
Active
Application number
FR1760675A
Other languages
English (en)
Other versions
FR3073526A1 (fr
Inventor
Jeremy Rame
Virginie Jaquet
Joel Delautre
Jean-Yves Guedou
Pierre Caron
Odile Lavigne
Didier Locq
Mikael Perrut
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.)
Office National dEtudes et de Recherches Aerospatiales ONERA
Safran SA
Original Assignee
Office National dEtudes et de Recherches Aerospatiales ONERA
Safran 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
Priority to FR1760675A priority Critical patent/FR3073526B1/fr
Application filed by Office National dEtudes et de Recherches Aerospatiales ONERA, Safran SA filed Critical Office National dEtudes et de Recherches Aerospatiales ONERA
Priority to CA3081885A priority patent/CA3081885A1/fr
Priority to PCT/FR2018/052840 priority patent/WO2019097163A1/fr
Priority to RU2020119484A priority patent/RU2780326C2/ru
Priority to JP2020544982A priority patent/JP7305662B2/ja
Priority to EP18821711.1A priority patent/EP3710611B1/fr
Priority to BR112020009492-7A priority patent/BR112020009492B1/pt
Priority to US16/763,713 priority patent/US11268170B2/en
Priority to CN201880073598.3A priority patent/CN111655881A/zh
Publication of FR3073526A1 publication Critical patent/FR3073526A1/fr
Application granted granted Critical
Publication of FR3073526B1 publication Critical patent/FR3073526B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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%
    • 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
    • F01D5/12—Blades
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/288—Protective coatings for blades

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

L'invention concerne un superalliage à base de nickel comprenant, en pourcentages massiques, 4,0 à 5,5 % de rhénium, 3,5 à 12,5 % de cobalt, 0,30 à 1,50 % de molybdène, 3,5 à 5,5 % de chrome, 3,5 à 5,5 % de tungstène, 4,5 à 6,0 % d'aluminium, 0,35 à 1,50 % de titane, 8,0 à 10,5 % de tantale, 0,15 à 0,30 % de hafnium, 0,05 à 0,15 % de silicium, le complément étant constitué par du nickel et des impuretés inévitables. L'invention concerne également une aube (20A, 20B) monocristalline comprenant un tel alliage et une turbomachine (10) comprenant une telle aube (20A, 20B).
FR1760675A 2017-11-14 2017-11-14 Superalliage a base de nickel, aube monocristalline et turbomachine Active FR3073526B1 (fr)

Priority Applications (9)

Application Number Priority Date Filing Date Title
FR1760675A FR3073526B1 (fr) 2017-11-14 2017-11-14 Superalliage a base de nickel, aube monocristalline et turbomachine
PCT/FR2018/052840 WO2019097163A1 (fr) 2017-11-14 2018-11-14 Superalliage a base de nickel, aube monocristalline et turbomachine
RU2020119484A RU2780326C2 (ru) 2017-11-14 2018-11-14 Суперсплав на никелевой основе, монокристаллическая лопатка и турбомашина
JP2020544982A JP7305662B2 (ja) 2017-11-14 2018-11-14 ニッケル基超合金、単結晶ブレード及びターボ機械
CA3081885A CA3081885A1 (fr) 2017-11-14 2018-11-14 Superalliage a base de nickel, aube monocristalline et turbomachine
EP18821711.1A EP3710611B1 (fr) 2017-11-14 2018-11-14 Superalliage a base de nickel, aube monocristalline et turbomachine
BR112020009492-7A BR112020009492B1 (pt) 2017-11-14 2018-11-14 Superliga à base de níquel, pá monocristalina, e, turbomáquina
US16/763,713 US11268170B2 (en) 2017-11-14 2018-11-14 Nickel-based superalloy, single-crystal blade and turbomachine
CN201880073598.3A CN111655881A (zh) 2017-11-14 2018-11-14 镍基超级合金、单晶体叶片和涡轮机

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1760675A FR3073526B1 (fr) 2017-11-14 2017-11-14 Superalliage a base de nickel, aube monocristalline et turbomachine
FR1760675 2017-11-14

Publications (2)

Publication Number Publication Date
FR3073526A1 FR3073526A1 (fr) 2019-05-17
FR3073526B1 true FR3073526B1 (fr) 2022-04-29

Family

ID=61599306

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1760675A Active FR3073526B1 (fr) 2017-11-14 2017-11-14 Superalliage a base de nickel, aube monocristalline et turbomachine

Country Status (8)

Country Link
US (1) US11268170B2 (fr)
EP (1) EP3710611B1 (fr)
JP (1) JP7305662B2 (fr)
CN (1) CN111655881A (fr)
BR (1) BR112020009492B1 (fr)
CA (1) CA3081885A1 (fr)
FR (1) FR3073526B1 (fr)
WO (1) WO2019097163A1 (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3092340B1 (fr) 2019-01-31 2021-02-12 Safran Superalliage à base de nickel à tenue mécanique et environnementale élevée à haute température et à faible densitée
FR3108365B1 (fr) 2020-03-18 2022-09-09 Safran Helicopter Engines Aube pour turbomachine comprenant un revetement anticorrosion, turbomachine comprenant l’aube et procede de depot du revetement sur l’aube
FR3124195B1 (fr) * 2021-06-22 2023-08-25 Safran Superalliage a base de nickel, aube monocristalline et turbomachine

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5270123A (en) 1992-03-05 1993-12-14 General Electric Company Nickel-base superalloy and article with high temperature strength and improved stability
US5366695A (en) * 1992-06-29 1994-11-22 Cannon-Muskegon Corporation Single crystal nickel-based superalloy
EP0637476B1 (fr) * 1993-08-06 2000-02-23 Hitachi, Ltd. Aube de turbine à gaz, procédé de fabrication de celle-ci et turbine à gaz utilisant cette aube
DE19624055A1 (de) * 1996-06-17 1997-12-18 Abb Research Ltd Nickel-Basis-Superlegierung
JPH11310839A (ja) 1998-04-28 1999-11-09 Hitachi Ltd 高強度Ｎｉ基超合金方向性凝固鋳物
FR2780982B1 (fr) * 1998-07-07 2000-09-08 Onera (Off Nat Aerospatiale) Superalliage monocristallin a base de nickel a haut solvus
DE59904846D1 (de) * 1999-05-20 2003-05-08 Alstom Switzerland Ltd Nickel-Basis-Superlegierung
WO2003080882A1 (fr) 2002-03-27 2003-10-02 National Institute For Materials Science Superalliage a base de ni solidifie de maniere directionnelle et superalliage a cristal unique a base de ni
RU2293782C1 (ru) 2005-08-15 2007-02-20 Федеральное государственное унитарное предприятие "Всероссийский научно-исследовательский институт авиационных материалов" (ФГУП "ВИАМ") Никелевый жаропрочный сплав для монокристаллического литья и изделие, выполненное из него
JP5146867B2 (ja) 2006-08-18 2013-02-20 独立行政法人物質・材料研究機構 高温耐久性に優れた耐熱部材
RU2415190C2 (ru) 2006-09-13 2011-03-27 Нэшнл Инститьют Фор Матириалз Сайенс МОНОКРИСТАЛЛИЧЕСКИЙ СУПЕРСПЛАВ НА ОСНОВЕ Ni
US20100126014A1 (en) * 2008-11-26 2010-05-27 General Electric Company Repair method for tbc coated turbine components
EP2631324A4 (fr) 2010-10-19 2014-04-16 Nat Inst For Materials Science Élément en un superalliage à base de ni contenant une couche d'accrochage résistante à la chaleur
CN102732750B (zh) * 2011-04-08 2015-06-10 中国科学院金属研究所 一种低成本、低密度镍基单晶高温合金
US20130129522A1 (en) * 2011-11-17 2013-05-23 Kenneth Harris Rhenium-free single crystal superalloy for turbine blades and vane applications
US9518311B2 (en) * 2014-05-08 2016-12-13 Cannon-Muskegon Corporation High strength single crystal superalloy
GB2540964A (en) 2015-07-31 2017-02-08 Univ Oxford Innovation Ltd A nickel-based alloy
DE102016202837A1 (de) * 2016-02-24 2017-08-24 MTU Aero Engines AG Wärmebehandlungsverfahren für Bauteile aus Nickelbasis-Superlegierungen

Also Published As

Publication number Publication date
JP7305662B2 (ja) 2023-07-10
BR112020009492A2 (pt) 2020-10-13
EP3710611A1 (fr) 2020-09-23
JP2021503045A (ja) 2021-02-04
EP3710611B1 (fr) 2024-01-10
WO2019097163A1 (fr) 2019-05-23
FR3073526A1 (fr) 2019-05-17
CA3081885A1 (fr) 2019-05-23
RU2020119484A (ru) 2021-12-15
US11268170B2 (en) 2022-03-08
US20200299808A1 (en) 2020-09-24
BR112020009492B1 (pt) 2023-04-11
CN111655881A (zh) 2020-09-11
RU2020119484A3 (fr) 2021-12-15

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