JP2011514431A5 - - Google Patents
Download PDFInfo
- Publication number
- JP2011514431A5 JP2011514431A5 JP2010523068A JP2010523068A JP2011514431A5 JP 2011514431 A5 JP2011514431 A5 JP 2011514431A5 JP 2010523068 A JP2010523068 A JP 2010523068A JP 2010523068 A JP2010523068 A JP 2010523068A JP 2011514431 A5 JP2011514431 A5 JP 2011514431A5
- Authority
- JP
- Japan
- Prior art keywords
- nickel
- superalloy composition
- base superalloy
- balance
- composition according
- 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.)
- Granted
Links
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims 22
- 229910000601 superalloy Inorganic materials 0.000 claims 19
- 229910052759 nickel Inorganic materials 0.000 claims 11
- 239000012535 impurity Substances 0.000 claims 7
- 230000003647 oxidation Effects 0.000 claims 2
- 238000007254 oxidation reaction Methods 0.000 claims 2
- 230000002459 sustained Effects 0.000 claims 2
- 229910052684 Cerium Inorganic materials 0.000 claims 1
- WUAPFZMCVAUBPE-UHFFFAOYSA-N Rhenium Chemical compound [Re] WUAPFZMCVAUBPE-UHFFFAOYSA-N 0.000 claims 1
- 125000004122 cyclic group Chemical group 0.000 claims 1
- 229910052746 lanthanum Inorganic materials 0.000 claims 1
- 229910052761 rare earth metal Inorganic materials 0.000 claims 1
- 229910052702 rhenium Inorganic materials 0.000 claims 1
- 229910052727 yttrium Inorganic materials 0.000 claims 1
Claims (17)
The gas turbine engine component according to any one of claims 14 to 16, wherein the gas turbine engine component is at least one member of a group consisting of a nozzle, a shroud, and a splash plate.
Applications Claiming Priority (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US96936007P | 2007-08-31 | 2007-08-31 | |
US60/969,360 | 2007-08-31 | ||
US11/964,668 | 2007-12-26 | ||
US11/964,668 US20130230405A1 (en) | 2007-08-31 | 2007-12-26 | Nickel base superalloy compositions being substantially free of rhenium and superalloy articles |
PCT/US2008/074171 WO2009032579A1 (en) | 2007-08-31 | 2008-08-25 | Nickel base superalloy compositions being substantially free of rhenium and superalloy articles |
Publications (3)
Publication Number | Publication Date |
---|---|
JP2011514431A JP2011514431A (en) | 2011-05-06 |
JP2011514431A5 true JP2011514431A5 (en) | 2011-10-13 |
JP5595917B2 JP5595917B2 (en) | 2014-09-24 |
Family
ID=40092097
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2010523068A Expired - Fee Related JP5595917B2 (en) | 2007-08-31 | 2008-08-25 | Nickel-based superalloy composition and superalloy article substantially free of rhenium |
Country Status (6)
Country | Link |
---|---|
US (1) | US20130230405A1 (en) |
EP (1) | EP2188401A1 (en) |
JP (1) | JP5595917B2 (en) |
CN (2) | CN101790593A (en) |
CA (1) | CA2696939A1 (en) |
WO (1) | WO2009032579A1 (en) |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2009085420A1 (en) * | 2007-12-26 | 2009-07-09 | General Electric Company | Nickel base superalloy compositions, superalloy articles, and methods for stabilizing superalloy compositions |
US20100254822A1 (en) * | 2009-03-24 | 2010-10-07 | Brian Thomas Hazel | Super oxidation and cyclic damage resistant nickel-base superalloy and articles formed therefrom |
US20100329921A1 (en) * | 2009-06-30 | 2010-12-30 | Joshua Leigh Miller | Nickel base superalloy compositions and superalloy articles |
US20110076180A1 (en) * | 2009-09-30 | 2011-03-31 | General Electric Company | Nickel-Based Superalloys and Articles |
US20110076181A1 (en) * | 2009-09-30 | 2011-03-31 | General Electric Company | Nickel-Based Superalloys and Articles |
ES2670877T3 (en) | 2011-12-07 | 2018-06-01 | Mtu Aero Engines Gmbh | Nickel-free super alloy with rhenium or reduced rhenium content |
EP2725110B1 (en) | 2012-10-26 | 2017-05-03 | MTU Aero Engines GmbH | Creep resistant rhenium-free nickel based superalloy |
ES2682362T3 (en) | 2015-05-05 | 2018-09-20 | MTU Aero Engines AG | Super-alloy of rhenium-free nickel with low density |
US10378087B2 (en) * | 2015-12-09 | 2019-08-13 | General Electric Company | Nickel base super alloys and methods of making the same |
US10253396B2 (en) * | 2016-09-02 | 2019-04-09 | General Electric Company | Modified articles, coated articles, and modified alloys |
FR3072717B1 (en) * | 2017-10-20 | 2019-10-11 | Safran | SUPERALLIATION TURBINE PIECE COMPRISING RHENIUM AND METHOD OF MANUFACTURING THE SAME |
CN108256192B (en) * | 2018-01-10 | 2021-06-01 | 中国科学院金属研究所 | Low-cycle fatigue-based thermomechanical fatigue life prediction method for metal material |
US10577679B1 (en) | 2018-12-04 | 2020-03-03 | General Electric Company | Gamma prime strengthened nickel superalloy for additive manufacturing |
US20230357897A1 (en) * | 2022-05-05 | 2023-11-09 | General Electric Company | Nickel-based superalloys and articles |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3655458A (en) * | 1970-07-10 | 1972-04-11 | Federal Mogul Corp | Process for making nickel-based superalloys |
GR80048B (en) * | 1983-12-27 | 1984-11-30 | Gen Electric | Yttrium and yttrium-silicon bearing nickel-based superalloys especially useful as comptible coatings for advanced superalloys |
GR80049B (en) * | 1983-12-27 | 1984-12-30 | Gen Electric | Nickel-based superalloys especially useful as compatible protective environmental coatings for advanced superalloys |
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 |
US5011353A (en) * | 1988-12-06 | 1991-04-30 | Allied-Signal Inc. | High temperature turbine engine structure |
US5435861A (en) * | 1992-02-05 | 1995-07-25 | Office National D'etudes Et De Recherches Aerospatiales | Nickel-based monocrystalline superalloy with improved oxidation resistance and method of production |
JPH09157777A (en) * | 1995-12-12 | 1997-06-17 | Mitsubishi Materials Corp | Nickel base alloy excellent in thermal fatigue resistance, high temperature creep resistance and high temperature corrosion resistance |
US5630700A (en) * | 1996-04-26 | 1997-05-20 | General Electric Company | Floating vane turbine nozzle |
JPH10168534A (en) * | 1996-12-10 | 1998-06-23 | Toshiba Corp | Turbine blade and its production |
US6096141A (en) * | 1998-08-03 | 2000-08-01 | General Electric Co. | Nickel-based superalloys exhibiting minimal grain defects |
US20020007877A1 (en) * | 1999-03-26 | 2002-01-24 | John R. Mihalisin | Casting of single crystal superalloy articles with reduced eutectic scale and grain recrystallization |
DE60108212T2 (en) * | 2000-08-30 | 2005-12-08 | Kabushiki Kaisha Toshiba | Monocrystalline nickel-based alloys and methods of making and high temperature components of a gas turbine engineered therefrom |
JP2002167636A (en) * | 2000-10-30 | 2002-06-11 | United Technol Corp <Utc> | Low density oxidation resistant superalloy material capable of thermal barrier coating retention without bond coat |
JP4521610B2 (en) * | 2002-03-27 | 2010-08-11 | 独立行政法人物質・材料研究機構 | Ni-based unidirectionally solidified superalloy and Ni-based single crystal superalloy |
US6706241B1 (en) * | 2002-11-12 | 2004-03-16 | Alstom Technology Ltd | Nickel-base superalloy |
-
2007
- 2007-12-26 US US11/964,668 patent/US20130230405A1/en not_active Abandoned
-
2008
- 2008-08-25 CA CA2696939A patent/CA2696939A1/en not_active Abandoned
- 2008-08-25 JP JP2010523068A patent/JP5595917B2/en not_active Expired - Fee Related
- 2008-08-25 CN CN200880105530.5A patent/CN101790593A/en active Pending
- 2008-08-25 EP EP08798597A patent/EP2188401A1/en not_active Withdrawn
- 2008-08-25 WO PCT/US2008/074171 patent/WO2009032579A1/en active Application Filing
- 2008-08-25 CN CN201410525776.5A patent/CN104313397A/en active Pending
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JP2011514431A5 (en) | ||
JP2011514430A5 (en) | ||
JP6248117B2 (en) | Nickel-based superalloys and articles | |
JP2011080146A5 (en) | ||
JP2011052323A5 (en) | ||
CA2479774A1 (en) | Ni-base directionally solidified and single-crystal superalloy | |
JP6016016B2 (en) | Ni-based single crystal superalloy | |
JP2011074493A (en) | Nickel-based superalloy and article | |
CA2680650A1 (en) | Ni-based single crystal superalloy and turbine blade incorporating the same | |
WO2009023090A3 (en) | Corrosion resistant nickel alloy compositions with enhanced castability and mechanical properties | |
ATE543920T1 (en) | NICKEL-BASED SUPER ALLOY AND PRODUCTION PROCESS THEREOF | |
RU2011153366A (en) | SINGLE-CRYSTAL SUPER ALLOY ON THE BASIS OF Ni AND TURBINE SHOVEL | |
JP2011514431A (en) | Nickel-based superalloy composition and superalloy article substantially free of rhenium | |
JP2011514430A (en) | Low rhenium nickel-base superalloy composition and superalloy article | |
EP2612935A3 (en) | Low rhenium single crystal superalloy for turbine blades and vane applications | |
JP2011074491A (en) | Nickel-based superalloy and article | |
CA2537225A1 (en) | High temperature powder metallurgy superalloy with enhanced fatigue & creep resistance | |
JP5715782B2 (en) | Processes and alloys for turbine blades and blades formed therefrom | |
JP2004332116A (en) | Nickel-base alloy | |
JP2010126813A (en) | Highly heat-resistant and oxidation-resistant material | |
EP2449140B1 (en) | Nickel base superalloy compositions and articles thereof | |
EP2304066B1 (en) | Nickel base gamma prime strengthened superalloy | |
WO2005064027A1 (en) | Nickel-based super-heat-resistant alloy and gas turbine component using same | |
CN104404309A (en) | High-temperature resistant nickel alloy | |
Koizumi et al. | Effects of Alloying Additions on the Creep Strength of a Fourth Generation Single-Crystal Superalloy. |