EP1914327A1 - Nickel-Basis-Superlegierung - Google Patents

Nickel-Basis-Superlegierung Download PDF

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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Withdrawn
Application number
EP06021724A
Other languages
English (en)
French (fr)
Inventor
Magnus Hasselqvist
Gordon Mccolvin
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.)
Siemens AG
Original Assignee
Siemens AG
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 Siemens AG filed Critical Siemens AG
Priority to EP06021724A priority Critical patent/EP1914327A1/de
Priority to CN200780038506XA priority patent/CN101528959B/zh
Priority to PCT/EP2007/059936 priority patent/WO2008046708A1/en
Priority to JP2009532751A priority patent/JP5124582B2/ja
Priority to EP07803558.1A priority patent/EP2076616B1/de
Priority to US12/311,873 priority patent/US20100296962A1/en
Publication of EP1914327A1 publication Critical patent/EP1914327A1/de
Withdrawn legal-status Critical Current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
    • C22C19/056—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)
EP06021724A 2006-10-17 2006-10-17 Nickel-Basis-Superlegierung Withdrawn EP1914327A1 (de)

Priority Applications (6)

Application Number Priority Date Filing Date Title
EP06021724A EP1914327A1 (de) 2006-10-17 2006-10-17 Nickel-Basis-Superlegierung
CN200780038506XA CN101528959B (zh) 2006-10-17 2007-09-20 镍基高温合金
PCT/EP2007/059936 WO2008046708A1 (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
EP07803558.1A EP2076616B1 (de) 2006-10-17 2007-09-20 Nickelbasis-superlegierungen
US12/311,873 US20100296962A1 (en) 2006-10-17 2007-09-20 Nickel-base superalloys

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP06021724A EP1914327A1 (de) 2006-10-17 2006-10-17 Nickel-Basis-Superlegierung

Publications (1)

Publication Number Publication Date
EP1914327A1 true EP1914327A1 (de) 2008-04-23

Family

ID=37714689

Family Applications (2)

Application Number Title Priority Date Filing Date
EP06021724A Withdrawn EP1914327A1 (de) 2006-10-17 2006-10-17 Nickel-Basis-Superlegierung
EP07803558.1A Active EP2076616B1 (de) 2006-10-17 2007-09-20 Nickelbasis-superlegierungen

Family Applications After (1)

Application Number Title Priority Date Filing Date
EP07803558.1A Active EP2076616B1 (de) 2006-10-17 2007-09-20 Nickelbasis-superlegierungen

Country Status (5)

Country Link
US (1) US20100296962A1 (de)
EP (2) EP1914327A1 (de)
JP (1) JP5124582B2 (de)
CN (1) CN101528959B (de)
WO (1) WO2008046708A1 (de)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2010124923A1 (en) * 2009-04-27 2010-11-04 Siemens Aktiengesellschaft NICKEL BASE γ/ γ' SUPERALLOY WITH MULTIPLE REACTIVE ELEMENTS AND USE OF SAID SUPERALLOY IN COMPLEX MATERIAL SYSTEMS
EP2431489A1 (de) 2010-09-20 2012-03-21 Siemens Aktiengesellschaft Superlegierung auf Nickelbasis
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 (de) * 2021-03-22 2022-09-28 Siemens Energy Global GmbH & Co. KG Nickelbasis-legierungszusammensetzung für bauteile mit reduzierter rissneigung und optimierten hochtemperatureigenschaften
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

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US20100034692A1 (en) * 2008-08-06 2010-02-11 General Electric Company Nickel-base superalloy, unidirectional-solidification process therefor, and castings formed therefrom
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
US9815147B2 (en) * 2014-04-04 2017-11-14 Special Metals Corporation High strength Ni—Cr—Mo—W—Nb—Ti welding product and method of welding and weld deposit using the same
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
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
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
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
CN106498308B (zh) * 2016-12-29 2019-01-22 沈阳大陆激光工程技术有限公司 一种用于小型型材轧辊激光合金化的耐磨抗热合金材料
CN106636760B (zh) * 2017-01-16 2019-01-08 宁国市华成金研科技有限公司 一种镍基高温合金及其制造方法
CN106636848B (zh) * 2017-01-18 2018-06-15 东南大学 一种耐磨抗蚀镍基合金丝材的制备方法
GB2565063B (en) 2017-07-28 2020-05-27 Oxmet Tech Limited A nickel-based alloy
CN107619957B (zh) * 2017-08-31 2018-12-21 江西理工大学 一种稳定镍基单晶合金中稀土元素成分的方法
JP6509290B2 (ja) * 2017-09-08 2019-05-08 三菱日立パワーシステムズ株式会社 コバルト基合金積層造形体、コバルト基合金製造物、およびそれらの製造方法
EP3489376A1 (de) * 2017-11-24 2019-05-29 Siemens Aktiengesellschaft Legierung für gasturbinenanwendungen mit hoher oxidationsbeständigkeit
RU2674274C1 (ru) * 2018-03-22 2018-12-06 Федеральное государственное унитарное предприятие "Всероссийский научно-исследовательский институт авиационных материалов" (ФГУП "ВИАМ") Жаропрочный литейный сплав на основе никеля и изделие, выполненное из него
CN108467972B (zh) * 2018-04-16 2020-06-09 中国航发北京航空材料研究院 一种高承温能力的镍基变形高温合金及其制备方法
RU2691790C1 (ru) * 2019-02-20 2019-06-18 Общество с ограниченной ответственностью "НТЦ "Современные технологии металлургии" (ООО "НТЦ "СТМ") Литейный никелевый сплав
WO2020179081A1 (ja) 2019-03-07 2020-09-10 三菱日立パワーシステムズ株式会社 コバルト基合金製造物
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CN110157953A (zh) * 2019-06-04 2019-08-23 沈阳中科煜宸科技有限公司 一种激光增材制造用高温合金粉末及其制备方法
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CN112853154B (zh) * 2021-01-04 2022-02-22 广东省科学院中乌焊接研究所 镍基中间层合金材料及其制备方法、焊件及焊接方法以及应用
CN113265563B (zh) * 2021-05-06 2022-04-29 中国联合重型燃气轮机技术有限公司 一种抗热腐蚀性好的Ni高温合金及其制备方法
CN113930642B (zh) * 2021-09-30 2022-04-22 中南大学 一种高强韧多组分精密高电阻合金及其制备方法
EP4241906A1 (de) * 2022-03-11 2023-09-13 Siemens Aktiengesellschaft Nickelbasislegierung, bauteil, pulver und verfahren
CN115044805B (zh) * 2022-05-30 2023-04-11 北京科技大学 一种多性能平衡的镍基单晶高温合金及制备方法
CN115418598A (zh) * 2022-09-20 2022-12-02 国网福建省电力有限公司 一种镧掺杂的高锰硅含量镍铜基电弧喷涂涂层的制备方法
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
GB2626730A (en) * 2023-01-27 2024-08-07 Siemens Energy Global Gmbh & Co Kg Oxidation resistant Nickel (Ni) base superalloy, powder, components and methods

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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
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 (en) * 2009-04-27 2010-11-04 Siemens Aktiengesellschaft NICKEL BASE γ/ γ' SUPERALLOY WITH MULTIPLE REACTIVE ELEMENTS AND USE OF SAID SUPERALLOY IN COMPLEX MATERIAL SYSTEMS
EP2248923A1 (de) * 2009-04-27 2010-11-10 Siemens Aktiengesellschaft y/ý-Superlegierung auf Nickelbasis mit mehreren reaktiven Elementen und Verwendung besagter Superlegierung in komplexen Materialsystemen
EP2431489A1 (de) 2010-09-20 2012-03-21 Siemens Aktiengesellschaft Superlegierung auf Nickelbasis
WO2012038166A3 (en) * 2010-09-20 2012-09-07 Siemens Aktiengesellschaft Nickel-base superalloy
CN103119183A (zh) * 2010-09-20 2013-05-22 西门子公司 镍基超级合金
CN103119183B (zh) * 2010-09-20 2015-05-06 西门子公司 镍基超级合金
RU2567759C2 (ru) * 2010-09-20 2015-11-10 Сименс Акциенгезелльшафт Суперсплав на основе никеля
WO2012038166A2 (en) 2010-09-20 2012-03-29 Siemens Aktiengesellschaft Nickel-base superalloy
US9593583B2 (en) 2010-09-20 2017-03-14 Siemens Aktiengesellschaft Nickel-base superalloy
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 (de) * 2021-03-22 2022-09-28 Siemens Energy Global GmbH & Co. KG Nickelbasis-legierungszusammensetzung für bauteile mit reduzierter rissneigung und optimierten hochtemperatureigenschaften
WO2022200175A1 (de) * 2021-03-22 2022-09-29 Siemens Energy Global GmbH & Co. KG Nickelbasis-legierungszusammensetzung für bauteile mit reduzierter rissneigung und optimierten hochtemperatureigenschaften
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

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EP2076616A1 (de) 2009-07-08
WO2008046708A1 (en) 2008-04-24
CN101528959A (zh) 2009-09-09
CN101528959B (zh) 2012-10-10
JP5124582B2 (ja) 2013-01-23
JP2010507016A (ja) 2010-03-04

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