AU2001265422A1 - Nickel-base superalloy for high temperature, high strain application - Google Patents

Nickel-base superalloy for high temperature, high strain application

Info

Publication number
AU2001265422A1
AU2001265422A1 AU2001265422A AU6542201A AU2001265422A1 AU 2001265422 A1 AU2001265422 A1 AU 2001265422A1 AU 2001265422 A AU2001265422 A AU 2001265422A AU 6542201 A AU6542201 A AU 6542201A AU 2001265422 A1 AU2001265422 A1 AU 2001265422A1
Authority
AU
Australia
Prior art keywords
nickel
high temperature
life
base superalloy
useful
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.)
Abandoned
Application number
AU2001265422A
Inventor
Kenneth Harris
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.)
Cannon Muskegon Corp
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
Publication of AU2001265422A1 publication Critical patent/AU2001265422A1/en
Abandoned legal-status Critical Current

Links

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%

Abstract

A nickel-base superalloy that exhibits outstanding mechanical properties under high temperature and high strain conditions when cast in an equiaxed and/or directionally solidified, columnar grain structure, and which exhibits increased grain boundary strength and ductility while maintaining microstructural stability includes, in percentages by weight, 5-6 chromium, 9-9.5 cobalt, 0.3-0.7 molybdenum, 8-9 tungsten, 5.9-6.3 tantalum, 0.05-0.25 titanium, 5.6-6.0 aluminum, 2.8-3.1 rhenium, 1.1-1.8 hafnium, 0.10-0.12 carbon, 0.010-0.024 boron, 0.011-0.020 zirconium, with the balance being nickel and incidental impurities. The superalloys of this invention are useful for casting gas turbine engine components exhibiting significantly improved low cycle fatigue life, improved airfoil high temperature stress rupture life, significantly reduced life cycle cost, and longer useful life.</PTEXT>
AU2001265422A 2000-09-15 2001-06-04 Nickel-base superalloy for high temperature, high strain application Abandoned AU2001265422A1 (en)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
US23282200P 2000-09-15 2000-09-15
US60232822 2000-09-15
US09/692,750 US6632299B1 (en) 2000-09-15 2000-10-19 Nickel-base superalloy for high temperature, high strain application
US09692750 2000-10-19
PCT/US2001/040842 WO2002022901A1 (en) 2000-09-15 2001-06-04 Nickel-base superalloy for high temperature, high strain application

Publications (1)

Publication Number Publication Date
AU2001265422A1 true AU2001265422A1 (en) 2002-03-26

Family

ID=26926359

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2001265422A Abandoned AU2001265422A1 (en) 2000-09-15 2001-06-04 Nickel-base superalloy for high temperature, high strain application

Country Status (10)

Country Link
US (1) US6632299B1 (en)
EP (1) EP1334215B1 (en)
AT (1) ATE347623T1 (en)
AU (1) AU2001265422A1 (en)
CA (1) CA2421039C (en)
DE (1) DE60125059T2 (en)
ES (1) ES2275686T3 (en)
IL (2) IL154889A0 (en)
TW (1) TWI248975B (en)
WO (1) WO2002022901A1 (en)

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US7608560B2 (en) * 2003-06-06 2009-10-27 Symyx Technologies, Inc. Platinum-titanium-tungsten fuel cell catalyst
JP4676958B2 (en) * 2003-08-18 2011-04-27 サイミックス ソリューションズ， インコーポレイテッド Platinum-copper fuel cell catalyst
US20050284547A1 (en) * 2004-06-24 2005-12-29 Strattan Scott C Cast flapper with hot isostatic pressing treatment
CN101061289A (en) * 2004-06-24 2007-10-24 贝克休斯公司 Cast flapper with hot isostatic pressing treatment
US7422994B2 (en) * 2005-01-05 2008-09-09 Symyx Technologies, Inc. Platinum-copper-tungsten fuel cell catalyst
US20080044719A1 (en) * 2005-02-02 2008-02-21 Symyx Technologies, Inc. Platinum-copper-titanium fuel cell catalyst
US20070215586A1 (en) * 2006-03-16 2007-09-20 Clifford Graillat Nickel alloy welding wire
US7922969B2 (en) * 2007-06-28 2011-04-12 King Fahd University Of Petroleum And Minerals Corrosion-resistant nickel-base alloy
US8206117B2 (en) * 2007-12-19 2012-06-26 Honeywell International Inc. Turbine components and methods of manufacturing turbine components
US8216509B2 (en) * 2009-02-05 2012-07-10 Honeywell International Inc. Nickel-base superalloys
US20140030545A1 (en) * 2012-07-27 2014-01-30 United Technologies Corporation Article With Grouped Grain Patterns
US20160214350A1 (en) 2012-08-20 2016-07-28 Pratt & Whitney Canada Corp. Oxidation-Resistant Coated Superalloy
FR3057880B1 (en) * 2016-10-25 2018-11-23 Safran SUPERALLIAGE BASED ON NICKEL, MONOCRYSTALLINE AUBE AND TURBOMACHINE
RU2017134765A (en) 2016-11-29 2019-04-05 Зульцер Мэнэджмент Аг NICKEL-BASED CASTING ALLOY, CASTING AND METHOD FOR MANUFACTURING A ROTOR VANE VEHICLE
FR3084671B1 (en) * 2018-07-31 2020-10-16 Safran NICKEL-BASED SUPERALLY FOR MANUFACTURING A PART BY POWDER SHAPING
GB2579580B (en) 2018-12-04 2022-07-13 Alloyed Ltd A nickel-based alloy
FR3092340B1 (en) * 2019-01-31 2021-02-12 Safran Nickel-based superalloy with high mechanical and environmental resistance at high temperature and low density

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Also Published As

Publication number Publication date
ATE347623T1 (en) 2006-12-15
DE60125059D1 (en) 2007-01-18
EP1334215B1 (en) 2006-12-06
EP1334215A4 (en) 2005-12-14
CA2421039A1 (en) 2002-03-21
IL154889A0 (en) 2003-10-31
US6632299B1 (en) 2003-10-14
TWI248975B (en) 2006-02-11
IL154889A (en) 2006-08-20
EP1334215A1 (en) 2003-08-13
ES2275686T3 (en) 2007-06-16
CA2421039C (en) 2008-08-26
WO2002022901A1 (en) 2002-03-21
DE60125059T2 (en) 2007-06-21

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