EP1914327A1 - Superalliage à base de nickel - Google Patents
Superalliage à base de nickel Download PDFInfo
- Publication number
- EP1914327A1 EP1914327A1 EP06021724A EP06021724A EP1914327A1 EP 1914327 A1 EP1914327 A1 EP 1914327A1 EP 06021724 A EP06021724 A EP 06021724A EP 06021724 A EP06021724 A EP 06021724A EP 1914327 A1 EP1914327 A1 EP 1914327A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- superalloy
- nickel
- base superalloy
- component
- range
- 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.)
- Withdrawn
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%
Definitions
- the invention relates to nickel-base superalloys and to components containing these alloys.
- Nickel-base superalloys are used in applications where a combination of high strength and a strong resistance to chemical attacks at high temperatures is needed. They are employed for the production of components of gas turbines such as blades and vanes. These parts are arranged in the hot section of a turbine and thus have to withstand high temperatures and an aggressive atmosphere.
- Nickel-base superalloys and components of the above mentioned kind are disclosed for example in US 6,818,077 , US 6,419,763 , US 6,177,046 , EP 0 789 087 and EP 0 637 474 .
- the nickel-base superalloy of the invention comprises in wt%: Co + Fe + Mn 0 - 20 Al 4 - 6 Cr >12 - 20 Ta >7.5 - 15 Ti 0 - ⁇ 0.45 V 0 - 1 Nb 0 - ⁇ 0.28 Mo 0 - 2.5 Mo + W + Re + Rh 2 - 8 Ru + Os + Ir + Pt + Pd 0 - 4 Hf 0 - 1.5 C + B + Zr 0 - 0.5 Ca + Mg + Cu 0 - 0.5 Y + La + Sc + Ce + Actinides + Lanthanides 0 - 0.5 Si 0 - 0.5 Ni balance
- Nb and V can be added to the superalloy, but since they are detrimental to the oxidation resistance, they should at most be added in limited quantities.
- the amount of Ti should not exceed 0.45 and the amount of V should not exceed 1 wt% respectively.
- the amount of matrix strengthening elements Mo, W, Re and Rh is between 2 and 8 wt%.
- Hf, C, B, Zr, Ca, Mg, Cu, Y, La, Sc, Ce, actinites and lanthanides, and Si can be present in the superalloy in order to adapt its properties to special needs such as grain boundary strengtheners, oxide scale fortification, and compatibility with specific coating systems.
- the content of Ti can be in the range (in wt%) of 0-0.40. Preferably it can be 0-0.35, more preferably 0-0.30 and most preferably 0-0.20.
- the content of Nb (in wt%) can be in the range of 0-0.25, preferably 0-0.20, more preferably 0-0.15 and most preferably 0-0.10.
- the content of C (in wt%) can be in the range of 0-0.15, preferably 0-0.08, more preferably 0.01-0.06 and most preferably 0.02-0.04.
- the superalloy of the invention can also contain B in the range (in wt%) of 0-0.02, preferably 0-0.01, more preferably 0.001-0.008 and most preferably 0.003-0.007.
- a conventional cast component, directionally solified component and a single crystal component, which comprise the super alloy are provided.
- a conventional cast or a single crystal component consisting of a superalloy which comprises in wt%: Co + Fe + Mn 0 - 20 Al 4 - 6 Cr >12 - 20 Ta >7.5 - 15 Ti 0 - 1.5 V 0 - 1 Ti + Nb + V 0 - 2 Mo 0 - 2.5 Mo + W + Re + Rh 2 - 8 Ru + Os + Ir + Pt + Pd 0 - 4 Hf 0 - 1.5 C + B + Zr 0 - 0.5 Ca + Mg + Cu 0 - 0.5 Y + La + Sc + Ce + Actinides + Lanthanides 0 - 0.5 Si 0 - 0.5 Ni balance is provided.
- the components of the invention can especially be part of a gas turbine, for example a turbine blade or vane.
- the particle content was measured to be ⁇ 60 vol%.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Priority Applications (6)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EP06021724A EP1914327A1 (fr) | 2006-10-17 | 2006-10-17 | Superalliage à base de nickel |
| CN200780038506XA CN101528959B (zh) | 2006-10-17 | 2007-09-20 | 镍基高温合金 |
| US12/311,873 US20100296962A1 (en) | 2006-10-17 | 2007-09-20 | Nickel-base superalloys |
| JP2009532751A JP5124582B2 (ja) | 2006-10-17 | 2007-09-20 | ニッケル基超合金 |
| PCT/EP2007/059936 WO2008046708A1 (fr) | 2006-10-17 | 2007-09-20 | Superalliages à base de nickel |
| EP07803558.1A EP2076616B1 (fr) | 2006-10-17 | 2007-09-20 | Superalliages à base de nickel |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EP06021724A EP1914327A1 (fr) | 2006-10-17 | 2006-10-17 | Superalliage à base de nickel |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| EP1914327A1 true EP1914327A1 (fr) | 2008-04-23 |
Family
ID=37714689
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP06021724A Withdrawn EP1914327A1 (fr) | 2006-10-17 | 2006-10-17 | Superalliage à base de nickel |
| EP07803558.1A Active EP2076616B1 (fr) | 2006-10-17 | 2007-09-20 | Superalliages à base de nickel |
Family Applications After (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP07803558.1A Active EP2076616B1 (fr) | 2006-10-17 | 2007-09-20 | Superalliages à base de nickel |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US20100296962A1 (fr) |
| EP (2) | EP1914327A1 (fr) |
| JP (1) | JP5124582B2 (fr) |
| CN (1) | CN101528959B (fr) |
| WO (1) | WO2008046708A1 (fr) |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2371495C1 (ru) * | 2008-06-20 | 2009-10-27 | Открытое акционерное общество "Всероссийский Институт Легких сплавов" (ОАО ВИЛС) | Жаропрочный порошковый никелевый сплав |
| WO2010124923A1 (fr) * | 2009-04-27 | 2010-11-04 | Siemens Aktiengesellschaft | Superalliage γ/γ' à base de nickel comprenant de multiples éléments réactifs et utilisation dudit superalliage dans des systèmes matériaux complexes |
| EP2431489A1 (fr) | 2010-09-20 | 2012-03-21 | Siemens Aktiengesellschaft | Superalliages à base de nickel |
| CN102876953A (zh) * | 2012-09-27 | 2013-01-16 | 无锡宏昌五金制造有限公司 | 镍铬高温合金 |
| RU2652920C1 (ru) * | 2017-12-05 | 2018-05-03 | Юлия Алексеевна Щепочкина | Сплав |
| DE102019201095A1 (de) * | 2019-01-29 | 2020-07-30 | Friedrich-Alexander-Universität Erlangen-Nürnberg | Nickelbasislegierung für Hochtemperaturanwendungen und Verfahren |
| CN112575228A (zh) * | 2020-11-12 | 2021-03-30 | 中国联合重型燃气轮机技术有限公司 | 抗蠕变、长寿命镍基变形高温合金及其制备方法和应用 |
| EP4063045A1 (fr) * | 2021-03-22 | 2022-09-28 | Siemens Energy Global GmbH & Co. KG | Composition d'alliage à base de nickel pour composants présentant une fissilité réduite et des propriétés améliorées à haute température |
| RU2803779C1 (ru) * | 2022-10-28 | 2023-09-19 | Российская Федерация, От Имени Которой Выступает Министерство Промышленности И Торговли Российской Федерации | Литейный коррозионно-стойкий поликристаллический жаропрочный сплав на основе никеля |
| WO2025098567A1 (fr) * | 2023-11-09 | 2025-05-15 | Vdm Metals International Gmbh | Procédé de fabrication d'un composant métallique |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20100034692A1 (en) * | 2008-08-06 | 2010-02-11 | General Electric Company | Nickel-base superalloy, unidirectional-solidification process therefor, and castings formed therefrom |
| RU2367698C1 (ru) * | 2008-08-15 | 2009-09-20 | Юлия Алексеевна Щепочкина | Сплав для изготовления штампового инструмента |
| RU2383642C1 (ru) * | 2008-10-29 | 2010-03-10 | Открытое акционерное общество "Научно-производственное объединение "Сатурн" (ОАО "НПО "Сатурн") | Жаропрочный литейный сплав на основе никеля |
| CN101851714A (zh) * | 2010-05-27 | 2010-10-06 | 江苏新华合金电器有限公司 | 核电站蒸汽发生器防震条端板材料及其制备方法 |
| CN102443721B (zh) * | 2010-10-13 | 2013-10-09 | 中国科学院金属研究所 | 一种组织稳定性好、易加工的镍钴基高温合金 |
| US9339398B2 (en) * | 2012-04-26 | 2016-05-17 | Medtronic Vascular, Inc. | Radiopaque enhanced nickel alloy for stents |
| CN102676881A (zh) * | 2012-06-12 | 2012-09-19 | 钢铁研究总院 | 消除原始颗粒边界的镍基粉末冶金高温合金 |
| RU2520934C1 (ru) * | 2013-03-15 | 2014-06-27 | Открытое акционерное общество "Научно-производственное объединение "Сатурн" | Жаропрочный никелевый сплав, обладающий высоким сопротивлением к сульфидной коррозии в сочетании с высокой жаропрочностью |
| CN103469011B (zh) * | 2013-08-16 | 2016-02-10 | 广东华鳌合金新材料有限公司 | 镍铬高温合金及其制备方法 |
| CN103725923B (zh) * | 2014-01-16 | 2016-08-17 | 张霞 | 一种铝强化的镍基合金及其制备方法 |
| BR112016023139B1 (pt) * | 2014-04-04 | 2021-05-18 | Special Metals Corporation | produtos de solda de ni-cr-mo-w-nb-ti de alta resistência e método de soldagem e depósito de solda usando o mesmo |
| CN103952593B (zh) * | 2014-04-21 | 2016-04-06 | 西北工业大学 | 一种k4169高温合金 |
| CN104087786B (zh) * | 2014-06-25 | 2016-06-15 | 盐城市鑫洋电热材料有限公司 | 一种镍铬电热复合材料及其制备方法 |
| US20160167172A1 (en) * | 2014-08-26 | 2016-06-16 | Liburdi Engineering Limited | Method of cladding, additive manufacturing and fusion welding of superalloys and materialf or the same |
| DE102014220179A1 (de) * | 2014-10-06 | 2016-04-07 | Siemens Aktiengesellschaft | Nickelbasierter Werkstoff mit Platin, Verwendung als Schweißzusatzwerkstoff und Bauteil |
| JP6095237B2 (ja) * | 2015-01-26 | 2017-03-15 | 日立金属Mmcスーパーアロイ株式会社 | 高温クリープ特性に優れたNi基合金およびこのNi基合金を用いたガスタービン用部材 |
| GB2539959A (en) | 2015-07-03 | 2017-01-04 | Univ Oxford Innovation Ltd | A Nickel-based alloy |
| RU2626118C2 (ru) * | 2015-09-17 | 2017-07-21 | Открытое акционерное общество "Научно-производственное объединение "Сатурн" | Литейный жаропрочный сплав на основе никеля |
| CN105349811B (zh) * | 2015-11-11 | 2017-04-05 | 江西理工大学 | 提高镍基单晶高温合金铸造过程中稀土元素收得率的方法 |
| RU2685455C2 (ru) * | 2015-12-15 | 2019-04-18 | Открытое акционерное общество "Научно-производственное объединение "Сатурн" | Литейный никелевый сплав с равноосной структурой |
| CN105400992A (zh) * | 2015-12-18 | 2016-03-16 | 常熟市意润达商业设备厂 | 新型仓储笼 |
| CN105543747B (zh) * | 2015-12-21 | 2017-11-21 | 西北工业大学 | 一种保留有Laves相的增材制造镍基高温合金的制备方法 |
| CN105543568B (zh) * | 2015-12-21 | 2017-10-13 | 谷月恒 | 一种含铂无铼镍基单晶高温合金及其制备方法和应用 |
| RU2633679C1 (ru) * | 2016-12-20 | 2017-10-16 | Федеральное государственное унитарное предприятие "Всероссийский научно-исследовательский институт авиационных материалов" (ФГУП "ВИАМ") | Литейный жаропрочный сплав на никелевой основе и изделие, выполненное из него |
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| WO2020179082A1 (fr) | 2019-03-07 | 2020-09-10 | 三菱日立パワーシステムズ株式会社 | Poudre d'alliage à base de cobalt, corps fritté en alliage à base de cobalt et procédé de production d'un corps fritté en alliage à base de cobalt |
| SG11202012572PA (en) | 2019-03-07 | 2021-09-29 | Mitsubishi Power Ltd | Cobalt based alloy product, method for manufacturing same, and cobalt based alloy article |
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| CN112004951B (zh) | 2019-03-07 | 2022-02-18 | 三菱动力株式会社 | 钴基合金制造物及其制造方法 |
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| EP4241906A1 (fr) * | 2022-03-11 | 2023-09-13 | Siemens Aktiengesellschaft | Alliage à base de nickel, composant, poudre et procédé |
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| CN115572850A (zh) * | 2022-10-27 | 2023-01-06 | 惠州市惠阳协力精密铸造有限公司 | 一种高温合金铸件及其制备方法 |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0560296A1 (fr) * | 1992-03-09 | 1993-09-15 | Hitachi Metals, Ltd. | Superalliage à haute résistance mécanique présentant une bonne résistance à la corrosion à haute température, monocristal à haute résistance mécanique présentant une bonne résistance à la corrosion à haute température pour turbine à gaz et centrale thermique à cycle combiné |
| JPH10317080A (ja) * | 1997-05-22 | 1998-12-02 | Toshiba Corp | Ni基耐熱超合金、Ni基耐熱超合金の製造方法及びNi基耐熱超合金部品 |
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-
2006
- 2006-10-17 EP EP06021724A patent/EP1914327A1/fr not_active Withdrawn
-
2007
- 2007-09-20 JP JP2009532751A patent/JP5124582B2/ja not_active Expired - Fee Related
- 2007-09-20 CN CN200780038506XA patent/CN101528959B/zh active Active
- 2007-09-20 EP EP07803558.1A patent/EP2076616B1/fr active Active
- 2007-09-20 WO PCT/EP2007/059936 patent/WO2008046708A1/fr not_active Ceased
- 2007-09-20 US US12/311,873 patent/US20100296962A1/en not_active Abandoned
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| EP0560296A1 (fr) * | 1992-03-09 | 1993-09-15 | Hitachi Metals, Ltd. | Superalliage à haute résistance mécanique présentant une bonne résistance à la corrosion à haute température, monocristal à haute résistance mécanique présentant une bonne résistance à la corrosion à haute température pour turbine à gaz et centrale thermique à cycle combiné |
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| RU2371495C1 (ru) * | 2008-06-20 | 2009-10-27 | Открытое акционерное общество "Всероссийский Институт Легких сплавов" (ОАО ВИЛС) | Жаропрочный порошковый никелевый сплав |
| CN102414331A (zh) * | 2009-04-27 | 2012-04-11 | 西门子公司 | 具有多活性元素的镍基γ/γ'超合金和所述超合金在复杂材料体系中的用途 |
| WO2010124923A1 (fr) * | 2009-04-27 | 2010-11-04 | Siemens Aktiengesellschaft | Superalliage γ/γ' à base de nickel comprenant de multiples éléments réactifs et utilisation dudit superalliage dans des systèmes matériaux complexes |
| EP2248923A1 (fr) * | 2009-04-27 | 2010-11-10 | Siemens Aktiengesellschaft | Superalliage de y/ý à base de nickel avec plusieurs éléments réactifs et utilisation de cet alliage dans des systèmes de matériau complexes |
| CN102414331B (zh) * | 2009-04-27 | 2014-07-16 | 西门子公司 | 具有多活性元素的镍基γ/γ’超合金和所述超合金在复杂材料体系中的用途 |
| CN103119183B (zh) * | 2010-09-20 | 2015-05-06 | 西门子公司 | 镍基超级合金 |
| US9593583B2 (en) | 2010-09-20 | 2017-03-14 | Siemens Aktiengesellschaft | Nickel-base superalloy |
| WO2012038166A3 (fr) * | 2010-09-20 | 2012-09-07 | Siemens Aktiengesellschaft | Superalliage à base de nickel |
| CN103119183A (zh) * | 2010-09-20 | 2013-05-22 | 西门子公司 | 镍基超级合金 |
| WO2012038166A2 (fr) | 2010-09-20 | 2012-03-29 | Siemens Aktiengesellschaft | Superalliage à base de nickel |
| EP2431489A1 (fr) | 2010-09-20 | 2012-03-21 | Siemens Aktiengesellschaft | Superalliages à base de nickel |
| RU2567759C2 (ru) * | 2010-09-20 | 2015-11-10 | Сименс Акциенгезелльшафт | Суперсплав на основе никеля |
| CN102876953A (zh) * | 2012-09-27 | 2013-01-16 | 无锡宏昌五金制造有限公司 | 镍铬高温合金 |
| RU2652920C1 (ru) * | 2017-12-05 | 2018-05-03 | Юлия Алексеевна Щепочкина | Сплав |
| DE102019201095A1 (de) * | 2019-01-29 | 2020-07-30 | Friedrich-Alexander-Universität Erlangen-Nürnberg | Nickelbasislegierung für Hochtemperaturanwendungen und Verfahren |
| US12221674B2 (en) | 2019-01-29 | 2025-02-11 | Siemens Energy Global GmbH & Co. KG | Nickel-based alloy for high-temperature applications, and method |
| CN112575228A (zh) * | 2020-11-12 | 2021-03-30 | 中国联合重型燃气轮机技术有限公司 | 抗蠕变、长寿命镍基变形高温合金及其制备方法和应用 |
| EP4063045A1 (fr) * | 2021-03-22 | 2022-09-28 | Siemens Energy Global GmbH & Co. KG | Composition d'alliage à base de nickel pour composants présentant une fissilité réduite et des propriétés améliorées à haute température |
| WO2022200175A1 (fr) * | 2021-03-22 | 2022-09-29 | Siemens Energy Global GmbH & Co. KG | Composition d'alliage à base de nickel pour composants avec une tendance réduite à la fissuration et des propriétés optimisées à haute température |
| RU2803779C1 (ru) * | 2022-10-28 | 2023-09-19 | Российская Федерация, От Имени Которой Выступает Министерство Промышленности И Торговли Российской Федерации | Литейный коррозионно-стойкий поликристаллический жаропрочный сплав на основе никеля |
| WO2025098567A1 (fr) * | 2023-11-09 | 2025-05-15 | Vdm Metals International Gmbh | Procédé de fabrication d'un composant métallique |
Also Published As
| Publication number | Publication date |
|---|---|
| US20100296962A1 (en) | 2010-11-25 |
| CN101528959A (zh) | 2009-09-09 |
| JP2010507016A (ja) | 2010-03-04 |
| JP5124582B2 (ja) | 2013-01-23 |
| EP2076616B1 (fr) | 2015-10-28 |
| WO2008046708A1 (fr) | 2008-04-24 |
| CN101528959B (zh) | 2012-10-10 |
| EP2076616A1 (fr) | 2009-07-08 |
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