IL153479A0 - High strength hot corrosion and oxidation resistant, directionally solidified nickel base superalloy and articles - Google Patents

High strength hot corrosion and oxidation resistant, directionally solidified nickel base superalloy and articles

Info

Publication number
IL153479A0
IL153479A0 IL15347902A IL15347902A IL153479A0 IL 153479 A0 IL153479 A0 IL 153479A0 IL 15347902 A IL15347902 A IL 15347902A IL 15347902 A IL15347902 A IL 15347902A IL 153479 A0 IL153479 A0 IL 153479A0
Authority
IL
Israel
Prior art keywords
articles
high strength
oxidation resistant
directionally solidified
hot corrosion
Prior art date
Application number
IL15347902A
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=21815883&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=IL153479(A0) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by United Technologies Corp filed Critical United Technologies Corp
Publication of IL153479A0 publication Critical patent/IL153479A0/en

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
    • C22C19/056—Alloys 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%
    • 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

Abstract

Corrosion and oxidation resistant, high strength, directionally solidified superalloy alloys and articles are described. The articles have a nominal composition in weight percent of about 12% Cr, 9% Co, 1.9% Mo, 3.8% W, 5% Ta, 3.6% Al, 4.1% Ti, 0.015% B, 0.1 % C, up to about 0.02 Zr, balance essentially nickel, and include no intentional additions of hafnium or zirconium, and also have a small amounts of tantalum carbide. The resultant articles have good hot corrosion resistance and superior oxidation resistance and creep properties. The articles are preferably columnar grain, but may also be single crystal. <IMAGE>
IL15347902A 2001-12-18 2002-12-16 High strength hot corrosion and oxidation resistant, directionally solidified nickel base superalloy and articles IL153479A0 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/023,565 US20030111138A1 (en) 2001-12-18 2001-12-18 High strength hot corrosion and oxidation resistant, directionally solidified nickel base superalloy and articles

Publications (1)

Publication Number Publication Date
IL153479A0 true IL153479A0 (en) 2003-07-06

Family

ID=21815883

Family Applications (1)

Application Number Title Priority Date Filing Date
IL15347902A IL153479A0 (en) 2001-12-18 2002-12-16 High strength hot corrosion and oxidation resistant, directionally solidified nickel base superalloy and articles

Country Status (11)

Country Link
US (1) US20030111138A1 (en)
EP (1) EP1329527B1 (en)
JP (1) JP4413492B2 (en)
KR (1) KR100954683B1 (en)
CN (1) CN1322157C (en)
AT (1) ATE325901T1 (en)
DE (1) DE60211297T2 (en)
ES (1) ES2261604T3 (en)
IL (1) IL153479A0 (en)
RU (1) RU2295585C2 (en)
UA (1) UA73989C2 (en)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20050069450A1 (en) * 2003-09-30 2005-03-31 Liang Jiang Nickel-containing alloys, method of manufacture thereof and articles derived thereform
US20060182649A1 (en) * 2005-02-16 2006-08-17 Siemens Westinghouse Power Corp. High strength oxidation resistant superalloy with enhanced coating compatibility
US9322089B2 (en) * 2006-06-02 2016-04-26 Alstom Technology Ltd Nickel-base alloy for gas turbine applications
CN100460543C (en) * 2006-06-16 2009-02-11 中国科学院金属研究所 High strength antithermal corrosion low segregation directional high temp alloy
US20100254822A1 (en) * 2009-03-24 2010-10-07 Brian Thomas Hazel Super oxidation and cyclic damage resistant nickel-base superalloy and articles formed therefrom
US20110076179A1 (en) * 2009-03-24 2011-03-31 O'hara Kevin Swayne Super oxidation and cyclic damage resistant nickel-base superalloy and articles formed therefrom
EP2248923A1 (en) * 2009-04-27 2010-11-10 Siemens Aktiengesellschaft Nickel base y/ý superalloy with multiple reactive elements and use of said superalloy in complex material systems
US20110076181A1 (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
US20110076182A1 (en) * 2009-09-30 2011-03-31 General Electric Company Nickel-Based Superalloys and Articles
WO2011047714A1 (en) 2009-10-20 2011-04-28 Siemens Aktiengesellschaft Alloy for directional solidification and component made of stem-shaped crystals
EP2431489A1 (en) 2010-09-20 2012-03-21 Siemens Aktiengesellschaft Nickel-base superalloy
CN102011195B (en) * 2010-11-23 2012-06-06 北京科技大学 Preparation method of directional solidification high-Nb TiAl alloy single crystal
CN103314227B (en) * 2011-01-19 2016-05-18 西门子公司 For the sliding bearing and the turbine with this sliding bearing of turbine rotor
US20120282086A1 (en) * 2011-05-04 2012-11-08 General Electric Company Nickel-base alloy
CN103114225B (en) * 2011-11-16 2016-01-27 中国科学院金属研究所 A kind of High-strength hot-corrosion-resistnickel-base nickel-base monocrystal high-temperature alloy
US9404388B2 (en) 2014-02-28 2016-08-02 General Electric Company Article and method for forming an article
ITUA20161551A1 (en) * 2016-03-10 2017-09-10 Nuovo Pignone Tecnologie Srl LEAGUE HAVING HIGH RESISTANCE TO OXIDATION AND APPLICATIONS OF GAS TURBINES THAT USE IT
CN109234655B (en) * 2018-09-27 2020-09-11 北京科技大学 Method for improving relaxation stability of GH4169 high-temperature alloy
FR3094018B1 (en) * 2019-03-20 2022-02-04 Safran SUPERALLOY WITH OPTIMIZED PROPERTIES AND LIMITED DENSITY
CN117660810B (en) * 2024-01-31 2024-04-16 四川航大新材料有限公司 High-purity high-temperature master alloy for variable-cycle gas engine turbine blade and preparation method and application thereof

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3619182A (en) * 1968-05-31 1971-11-09 Int Nickel Co Cast nickel-base alloy
US3615376A (en) * 1968-11-01 1971-10-26 Gen Electric Cast nickel base alloy
GB1409628A (en) * 1973-06-26 1975-10-08 Avco Corp Nickel base alloy containing hafnium
GB1511562A (en) * 1974-07-17 1978-05-24 Gen Electric Nickel-base alloys
GB2033925B (en) * 1978-09-25 1983-07-20 Johnson Matthey Co Ltd Nickel based superalloys
US4597809A (en) * 1984-02-10 1986-07-01 United Technologies Corporation High strength hot corrosion resistant single crystals containing tantalum carbide
DE4323486C2 (en) * 1992-07-23 2001-09-27 Abb Research Ltd Precipitation-hardenable nickel-based superalloy and use of the alloy as a material in the production of a directional solidified component, such as in particular a gas turbine blade
US6355117B1 (en) * 1992-10-30 2002-03-12 United Technologies Corporation Nickel base superalloy single crystal articles with improved performance in air and hydrogen
EP0637476B1 (en) * 1993-08-06 2000-02-23 Hitachi, Ltd. Blade for gas turbine, manufacturing method of the same, and gas turbine including the blade
EP0855449B1 (en) * 1997-01-23 2000-08-23 Mitsubishi Materials Corporation Columnar crystalline Ni-base heat-resistant alloy having high resistance to intergranular corrosion at high temperature, method of producing the alloy, large-size article, and method of producing large-size article from the alloy
WO1999067435A1 (en) * 1998-06-23 1999-12-29 Siemens Aktiengesellschaft Directionally solidified casting with improved transverse stress rupture strength
JP2003529677A (en) * 1999-07-29 2003-10-07 シーメンス アクチエンゲゼルシヤフト Heat resistant structural member and method of manufacturing the same

Also Published As

Publication number Publication date
ES2261604T3 (en) 2006-11-16
UA73989C2 (en) 2005-10-17
RU2295585C2 (en) 2007-03-20
EP1329527A3 (en) 2003-10-22
DE60211297T2 (en) 2007-04-26
KR100954683B1 (en) 2010-04-27
ATE325901T1 (en) 2006-06-15
EP1329527B1 (en) 2006-05-10
DE60211297D1 (en) 2006-06-14
CN1322157C (en) 2007-06-20
EP1329527A2 (en) 2003-07-23
JP2003231933A (en) 2003-08-19
CN1432659A (en) 2003-07-30
KR20030051386A (en) 2003-06-25
JP4413492B2 (en) 2010-02-10
US20030111138A1 (en) 2003-06-19

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