WO2002070764A8 - Superalloy for single crystal turbine vanes - Google Patents

Superalloy for single crystal turbine vanes

Info

Publication number
WO2002070764A8
WO2002070764A8 PCT/US2001/017956 US0117956W WO02070764A8 WO 2002070764 A8 WO2002070764 A8 WO 2002070764A8 US 0117956 W US0117956 W US 0117956W WO 02070764 A8 WO02070764 A8 WO 02070764A8
Authority
WO
WIPO (PCT)
Prior art keywords
single crystal
superalloy
turbine vanes
nickel
crystal turbine
Prior art date
Application number
PCT/US2001/017956
Other languages
French (fr)
Other versions
WO2002070764A1 (en
Inventor
Kenneth Harris
Jacqueline B Wahl
Original Assignee
Cannon Muskegon 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 Cannon Muskegon Corp filed Critical Cannon Muskegon Corp
Priority to IL15682601A priority Critical patent/IL156826A0/en
Priority to AU2001275175A priority patent/AU2001275175A1/en
Publication of WO2002070764A1 publication Critical patent/WO2002070764A1/en
Priority to IL156826A priority patent/IL156826A/en
Publication of WO2002070764A8 publication Critical patent/WO2002070764A8/en

Links

Classifications

    • 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%

Abstract

A nickel-base superalloy that is useful for making single crystal castings exhibiting outstanding stress-rupture properties, creep-rupture properties, and an increased tolerance for grain defects contains, in percentages by weight, from about 4.3 % to about 5.3 % chromium, (Cr), from about 9 % to about 10 % cobalt (Co), from about 0.6 % to about 0.8 % molybdenum (Mo), from about 8.4 % to about 8.8 % tungsten (W), from about 4.3 % to about 4.8 % tantalum (Ta), from about 0.6 % to about 0.8 % titanium (Ti), from about 5.6 % to about 5.8 % aluminium (Al), from about 2,8 % to about 3.1 % rhenium (Re), from about 0.9 % to about 1.5 % hafnium (Hf), from about 0.06 % to about 0.08 % carbon (C), from about 0.012 % to about 0.020 % boron (B), from about 0.010 % zirconium (Zr), the balance being nickel and incidental impurities.
PCT/US2001/017956 2001-03-01 2001-06-04 Superalloy for single crystal turbine vanes WO2002070764A1 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
IL15682601A IL156826A0 (en) 2001-03-01 2001-06-04 Superalloy for single crystal turbine vanes
AU2001275175A AU2001275175A1 (en) 2001-03-01 2001-06-04 Superalloy for single crystal turbine vanes
IL156826A IL156826A (en) 2001-03-01 2003-07-08 Superalloy for single crystal turbine vanes

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/797,326 2001-03-01
US09/797,326 US20020164263A1 (en) 2001-03-01 2001-03-01 Superalloy for single crystal turbine vanes

Publications (2)

Publication Number Publication Date
WO2002070764A1 WO2002070764A1 (en) 2002-09-12
WO2002070764A8 true WO2002070764A8 (en) 2003-11-13

Family

ID=25170525

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2001/017956 WO2002070764A1 (en) 2001-03-01 2001-06-04 Superalloy for single crystal turbine vanes

Country Status (5)

Country Link
US (1) US20020164263A1 (en)
AU (1) AU2001275175A1 (en)
IL (1) IL156826A (en)
TW (1) TW576887B (en)
WO (1) WO2002070764A1 (en)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6632299B1 (en) * 2000-09-15 2003-10-14 Cannon-Muskegon Corporation Nickel-base superalloy for high temperature, high strain application
US7011721B2 (en) * 2001-03-01 2006-03-14 Cannon-Muskegon Corporation Superalloy for single crystal turbine vanes
JP4449337B2 (en) * 2003-05-09 2010-04-14 株式会社日立製作所 High oxidation resistance Ni-base superalloy castings and gas turbine parts
US6969431B2 (en) 2003-08-29 2005-11-29 Honeywell International, Inc. High temperature powder metallurgy superalloy with enhanced fatigue and creep resistance
SE528807C2 (en) * 2004-12-23 2007-02-20 Siemens Ag Component of a superalloy containing palladium for use in a high temperature environment and use of palladium for resistance to hydrogen embrittlement
US8495461B2 (en) * 2007-09-17 2013-07-23 Lg Electronics Inc. Data modulation method, modulator, recording method, and recording apparatus
US20110076181A1 (en) * 2009-09-30 2011-03-31 General Electric Company Nickel-Based Superalloys and Articles
US20110076182A1 (en) * 2009-09-30 2011-03-31 General Electric Company Nickel-Based Superalloys and Articles
US20110076180A1 (en) * 2009-09-30 2011-03-31 General Electric Company Nickel-Based Superalloys and Articles
GB2536940A (en) 2015-04-01 2016-10-05 Isis Innovation A nickel-based alloy
GB2539959A (en) 2015-07-03 2017-01-04 Univ Oxford Innovation Ltd A Nickel-based alloy
FR3057880B1 (en) * 2016-10-25 2018-11-23 Safran SUPERALLIAGE BASED ON NICKEL, MONOCRYSTALLINE AUBE AND TURBOMACHINE
GB201818180D0 (en) * 2018-11-08 2018-12-26 Rolls Royce Plc A nickel-base superalloy
FR3092340B1 (en) 2019-01-31 2021-02-12 Safran Nickel-based superalloy with high mechanical and environmental resistance at high temperature and low density

Family Cites Families (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USRE29920E (en) * 1975-07-29 1979-02-27 High temperature alloys
US4169742A (en) * 1976-12-16 1979-10-02 General Electric Company Cast nickel-base alloy article
US5154884A (en) * 1981-10-02 1992-10-13 General Electric Company Single crystal nickel-base superalloy article and method for making
US4765850A (en) * 1984-01-10 1988-08-23 Allied-Signal Inc. Single crystal nickel-base super alloy
US4719080A (en) * 1985-06-10 1988-01-12 United Technologies Corporation Advanced high strength single crystal superalloy compositions
US5100484A (en) * 1985-10-15 1992-03-31 General Electric Company Heat treatment for nickel-base superalloys
US6074602A (en) * 1985-10-15 2000-06-13 General Electric Company Property-balanced nickel-base superalloys for producing single crystal articles
US4908183A (en) * 1985-11-01 1990-03-13 United Technologies Corporation High strength single crystal superalloys
US5068084A (en) * 1986-01-02 1991-11-26 United Technologies Corporation Columnar grain superalloy articles
CA1315572C (en) * 1986-05-13 1993-04-06 Xuan Nguyen-Dinh Phase stable single crystal materials
US4781772A (en) * 1988-02-22 1988-11-01 Inco Alloys International, Inc. ODS alloy having intermediate high temperature strength
US5173255A (en) * 1988-10-03 1992-12-22 General Electric Company Cast columnar grain hollow nickel base alloy articles and alloy and heat treatment for making
US4983233A (en) * 1989-01-03 1991-01-08 General Electric Company Fatigue crack resistant nickel base superalloys and product formed
US5069873A (en) * 1989-08-14 1991-12-03 Cannon-Muskegon Corporation Low carbon directional solidification alloy
EP0560296B1 (en) * 1992-03-09 1998-01-14 Hitachi Metals, Ltd. Highly hot corrosion resistant and high-strength superalloy, highly hot corrosion resistant and high-strength casting having single crystal structure, gas turbine and combined cycle power generation system
US5470371A (en) * 1992-03-12 1995-11-28 General Electric Company Dispersion strengthened alloy containing in-situ-formed dispersoids and articles and methods of manufacture
US5366695A (en) * 1992-06-29 1994-11-22 Cannon-Muskegon Corporation Single crystal nickel-based superalloy
US5820700A (en) * 1993-06-10 1998-10-13 United Technologies Corporation Nickel base superalloy columnar grain and equiaxed materials with improved performance in hydrogen and air
DE69423061T2 (en) * 1993-08-06 2000-10-12 Hitachi Ltd Gas turbine blade, method for producing the same and gas turbine with this blade
EP0789087B1 (en) * 1996-02-09 2000-05-10 Hitachi, Ltd. High strength Ni-base superalloy for directionally solidified castings
DE19624056A1 (en) * 1996-06-17 1997-12-18 Abb Research Ltd Nickel-based super alloy
US5925198A (en) * 1997-03-07 1999-07-20 The Chief Controller, Research And Developement Organization Ministry Of Defence, Technical Coordination Nickel-based superalloy
JP2905473B1 (en) * 1998-03-02 1999-06-14 科学技術庁金属材料技術研究所長 Method for producing Ni-based directionally solidified alloy
US20020007877A1 (en) * 1999-03-26 2002-01-24 John R. Mihalisin Casting of single crystal superalloy articles with reduced eutectic scale and grain recrystallization

Also Published As

Publication number Publication date
TW576887B (en) 2004-02-21
AU2001275175A1 (en) 2002-09-19
US20020164263A1 (en) 2002-11-07
WO2002070764A1 (en) 2002-09-12
IL156826A (en) 2006-04-10

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