FR2856701A1 - Superalliage a base de nickel et pieces coulees en monocristal - Google Patents

Superalliage a base de nickel et pieces coulees en monocristal

Info

Publication number
FR2856701A1
FR2856701A1 FR0407030A FR0407030A FR2856701A1 FR 2856701 A1 FR2856701 A1 FR 2856701A1 FR 0407030 A FR0407030 A FR 0407030A FR 0407030 A FR0407030 A FR 0407030A FR 2856701 A1 FR2856701 A1 FR 2856701A1
Authority
FR
France
Prior art keywords
approximately
nickel
based superalloy
cast parts
crystal cast
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.)
Pending
Application number
FR0407030A
Other languages
English (en)
Inventor
John Corrigan
Michael G Launsbach
Russel G Vogt
John R Mihalisin
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.)
Howmet Corp
Original Assignee
Howmet Research 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 Howmet Research Corp filed Critical Howmet Research Corp
Publication of FR2856701A1 publication Critical patent/FR2856701A1/fr
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/28Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • C22C19/03Alloys based on nickel or cobalt based on nickel
    • C22C19/05Alloys based on nickel or cobalt based on nickel with chromium
    • C22C19/051Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
    • C22C19/056Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 10% but less than 20%
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • C22C19/03Alloys based on nickel or cobalt based on nickel
    • C22C19/05Alloys based on nickel or cobalt based on nickel with chromium
    • C22C19/051Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
    • C22C19/057Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being less 10%
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00Materials; Properties thereof
    • F05D2300/60Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/607Monocrystallinity

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Crystals, And After-Treatments Of Crystals (AREA)

Abstract

Ce superalliage (A ou B) comprend essentiellement, en % en poids, environ 12,5 % à environ 13,5 % de Cr, 9,0 à environ 9,9 % de Co, environ 4,7 à environ 5,1 % de Ti, environ 2,8 à environ 3,2 % de Al, environ 2,8 à environ 4,3 % de W, environ 1,4 à environ 1,6 de Mo, environ 2,85 à environ 3,1 % de Ta, environ 1,0 à environ 6,0 de Re, environ 0,08 à environ 0,11 % de C, environ 0,010 à environ 0,015 % de B, jusqu'à environ 0,15 % de Nb, jusqu'à environ 0,15 % de Hf, jusqu'à environ 0,003 % de Zr, et le reste formé de Ni et d'éventuelles impuretés.Application notamment aux aubes de turbines.
FR0407030A 2003-06-25 2004-06-25 Superalliage a base de nickel et pieces coulees en monocristal Pending FR2856701A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US48257903P 2003-06-25 2003-06-25
US10/831,978 US20050000603A1 (en) 2003-06-25 2004-04-26 Nickel base superalloy and single crystal castings

Publications (1)

Publication Number Publication Date
FR2856701A1 true FR2856701A1 (fr) 2004-12-31

Family

ID=33519539

Family Applications (2)

Application Number Title Priority Date Filing Date
FR0407030A Pending FR2856701A1 (fr) 2003-06-25 2004-06-25 Superalliage a base de nickel et pieces coulees en monocristal
FR0411661A Withdrawn FR2860804A1 (fr) 2003-06-25 2004-11-02 Superalliage a base de nickel et pieces coulees en monocristal

Family Applications After (1)

Application Number Title Priority Date Filing Date
FR0411661A Withdrawn FR2860804A1 (fr) 2003-06-25 2004-11-02 Superalliage a base de nickel et pieces coulees en monocristal

Country Status (4)

Country Link
US (1) US20050000603A1 (fr)
JP (1) JP2005139548A (fr)
DE (1) DE102004029833A1 (fr)
FR (2) FR2856701A1 (fr)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1999067435A1 (fr) * 1998-06-23 1999-12-29 Siemens Aktiengesellschaft Alliage a solidification directionnelle a resistance transversale a la rupture amelioree
US20070032848A1 (en) * 2005-08-04 2007-02-08 Cliff Bridges Elastic therapeutic wrap
US8216509B2 (en) * 2009-02-05 2012-07-10 Honeywell International Inc. Nickel-base superalloys
DE102010014832B4 (de) 2010-04-10 2018-04-26 Technische Universität Braunschweig Leicht bearbeitbare Nickelbasis-Legierung
US11130201B2 (en) * 2014-09-05 2021-09-28 Ametek, Inc. Nickel-chromium alloy and method of making the same
CN111101022B (zh) * 2018-10-29 2022-03-22 利宝地工程有限公司 高γ′镍基超级合金、其用途及制造涡轮发动机构件的方法
CN115572861B (zh) * 2022-09-23 2024-02-23 北京北冶功能材料有限公司 一种易于加工成型的镍基高温合金及其制备方法和应用

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4118223A (en) * 1971-09-13 1978-10-03 Cabot Corporation Thermally stable high-temperature nickel-base alloys
EP0637476A1 (fr) * 1993-08-06 1995-02-08 Hitachi, Ltd. Aube de turbine à gaz, procédé de fabrication et turbine à gaz utilisant cette aube
JP2000210789A (ja) * 1999-01-27 2000-08-02 Hitachi Ltd 溶接ワイヤ及び補修施工方法
US20020157738A1 (en) * 1999-07-29 2002-10-31 Ralf Burgel High-temperature-resistant component and process for producing the high-temperature-resistant component
EP1319729A1 (fr) * 2001-12-13 2003-06-18 Siemens Aktiengesellschaft Pièce résistante à des températures élevées réalisé en superalliage polycristallin ou monocristallin à base de nickel

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US292920A (en) * 1884-02-05 Assigxob to himself akd
US3619182A (en) * 1968-05-31 1971-11-09 Int Nickel Co Cast nickel-base alloy
US6416596B1 (en) * 1974-07-17 2002-07-09 The General Electric Company Cast nickel-base alloy
US4116723A (en) * 1976-11-17 1978-09-26 United Technologies Corporation Heat treated superalloy single crystal article and process
US4222794A (en) * 1979-07-02 1980-09-16 United Technologies Corporation Single crystal nickel superalloy
US5399313A (en) * 1981-10-02 1995-03-21 General Electric Company Nickel-based superalloys for producing single crystal articles having improved tolerance to low angle grain boundaries
US5154884A (en) * 1981-10-02 1992-10-13 General Electric Company Single crystal nickel-base superalloy article and method for making
US6054096A (en) * 1982-12-27 2000-04-25 United Technologies Corporation Stable heat treatable nickel superalloy single crystal articles and compositions
US4643782A (en) * 1984-03-19 1987-02-17 Cannon Muskegon Corporation Single crystal alloy technology
US5100484A (en) * 1985-10-15 1992-03-31 General Electric Company Heat treatment for nickel-base superalloys
US4731404A (en) * 1986-08-25 1988-03-15 Allied Corporation Polyester composition containing ester of polyfunctional high molecular weight alcohol
US4716080A (en) * 1987-04-09 1987-12-29 Owens-Corning Fiberglass Corporation Size composition
US5240518A (en) * 1990-09-05 1993-08-31 General Electric Company Single crystal, environmentally-resistant gas turbine shroud
US5395584A (en) * 1992-06-17 1995-03-07 Avco Corporation Nickel-base superalloy compositions
DE19624056A1 (de) * 1996-06-17 1997-12-18 Abb Research Ltd Nickel-Basis-Superlegierung
CN1278200A (zh) * 1997-10-27 2000-12-27 西门子西屋动力公司 铸造超级合金的接合方法
JP3184882B2 (ja) * 1997-10-31 2001-07-09 科学技術庁金属材料技術研究所長 Ni基単結晶合金とその製造方法
US6217286B1 (en) * 1998-06-26 2001-04-17 General Electric Company Unidirectionally solidified cast article and method of making
JP4392870B2 (ja) * 1998-06-29 2010-01-06 ダウ コ−ニング コ−ポレ−ション ヒドロシリル化反応による芳香族クロロシラン化合物の製造方法

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4118223A (en) * 1971-09-13 1978-10-03 Cabot Corporation Thermally stable high-temperature nickel-base alloys
EP0637476A1 (fr) * 1993-08-06 1995-02-08 Hitachi, Ltd. Aube de turbine à gaz, procédé de fabrication et turbine à gaz utilisant cette aube
JP2000210789A (ja) * 1999-01-27 2000-08-02 Hitachi Ltd 溶接ワイヤ及び補修施工方法
US20020157738A1 (en) * 1999-07-29 2002-10-31 Ralf Burgel High-temperature-resistant component and process for producing the high-temperature-resistant component
EP1319729A1 (fr) * 2001-12-13 2003-06-18 Siemens Aktiengesellschaft Pièce résistante à des températures élevées réalisé en superalliage polycristallin ou monocristallin à base de nickel

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
PATENT ABSTRACTS OF JAPAN vol. 2000, no. 11 3 January 2001 (2001-01-03) *

Also Published As

Publication number Publication date
US20050000603A1 (en) 2005-01-06
FR2860804A1 (fr) 2005-04-15
DE102004029833A1 (de) 2005-01-20
JP2005139548A (ja) 2005-06-02

Similar Documents

Publication Publication Date Title
WO2012038166A3 (fr) Superalliage à base de nickel
EP2128283A3 (fr) Superalliage à moulage à base de nickel et composant de moulage pour turbine à vapeur l'utilisant en tant
CA2276154A1 (fr) Superalliage monocristallin a base de nickel et a .gamma.' solvus eleve
HK1133047A1 (en) Nickel-rich wear resistant alloy and method of making and use thereof
CA2603681A1 (fr) Acier inoxydable austenitique
JP2011514430A5 (fr)
WO2008111585A1 (fr) SUPERALLIAGE MONOCRISTALLIN À BASE DE Ni ET AUBE DE TURBINE L'UTILISANT
GB0127237D0 (en) coating composition for high temperature protection
WO2008015643A3 (fr) Alliage pour brasage à base de nickel et procédé de brasage
WO2019018038A3 (fr) Superalliage à base de cobalt-nickel à durcissement par précipitation et article fabriqué à partir de celui-ci
EP1426457A3 (fr) Composition de superalliage à base de nickel et son utilisation dans les articles monocrystaline
JP2011514431A5 (fr)
RU2009110199A (ru) Мартенситная нержавеющая сталь
UA100460C2 (uk) Сплав на основі нікелю, здатний утворювати оксид алюмінію
RU2009111603A (ru) Мартенситная нержавеющая сталь для сварных структур
FR2856701A1 (fr) Superalliage a base de nickel et pieces coulees en monocristal
PL2099946T3 (pl) Stop żelazo-nikiel o dużej ciągliwości i małym współczynniku rozszerzalności
JP3944582B2 (ja) Ni基超合金
DE60125059D1 (de) Nickelbasis-superlegierung zur anwendung im hochtemperatur- und hochbeanspruchungsbereich
DE50301388D1 (de) Nickel-Basis-Superlegierung
JP2004218086A5 (fr)
ATE296901T1 (de) Superlegierung auf nickelbasis
EP2206795A3 (fr) Alliage à base de Ni pour une pièce de moulage d'une turbine à vapeur avec une excellente résistance à haute température, coulabilité et soudabilité
ATE325902T1 (de) Reparaturmaterial für bauteile
ATE217652T1 (de) Nickelbasislegierung und verfahren