JP5024797B2 - コバルトフリーのNi基超合金 - Google Patents
コバルトフリーのNi基超合金 Download PDFInfo
- Publication number
- JP5024797B2 JP5024797B2 JP2007510462A JP2007510462A JP5024797B2 JP 5024797 B2 JP5024797 B2 JP 5024797B2 JP 2007510462 A JP2007510462 A JP 2007510462A JP 2007510462 A JP2007510462 A JP 2007510462A JP 5024797 B2 JP5024797 B2 JP 5024797B2
- Authority
- JP
- Japan
- Prior art keywords
- base superalloy
- less
- hours
- turbine
- cobalt
- 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.)
- Expired - Fee Related
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D27/00—Treating the metal in the mould while it is molten or ductile ; Pressure or vacuum casting
- B22D27/04—Influencing the temperature of the metal, e.g. by heating or cooling the mould
- B22D27/045—Directionally solidified castings
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- 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
- C22C19/007—Alloys based on nickel or cobalt with a light metal (alkali metal Li, Na, K, Rb, Cs; earth alkali metal Be, Mg, Ca, Sr, Ba, Al Ga, Ge, Ti) or B, Si, Zr, Hf, Sc, Y, lanthanides, actinides, as the next major constituent
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- 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%
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C30/00—Alloys containing less than 50% by weight of each constituent
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/10—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of nickel or cobalt or alloys based thereon
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/10—Metals, alloys or intermetallic compounds
- F05D2300/12—Light metals
- F05D2300/121—Aluminium
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/10—Metals, alloys or intermetallic compounds
- F05D2300/13—Refractory metals, i.e. Ti, V, Cr, Zr, Nb, Mo, Hf, Ta, W
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/10—Metals, alloys or intermetallic compounds
- F05D2300/13—Refractory metals, i.e. Ti, V, Cr, Zr, Nb, Mo, Hf, Ta, W
- F05D2300/131—Molybdenum
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/10—Metals, alloys or intermetallic compounds
- F05D2300/13—Refractory metals, i.e. Ti, V, Cr, Zr, Nb, Mo, Hf, Ta, W
- F05D2300/132—Chromium
Description
上記第3〜第8のタービンブレードやタービンベーンの発明によれば、請求の範囲1または2で製造されるコバルトフリーのNi基超合金を普通凝固法、単結晶凝固法および一方向凝固法を用いて成形することにより、長時間にわたり組織安定性が高く、高温におけるクリープ特性が優れたタービンブレードまたはタービンベーン部品を製造することが可能となる。
Claims (6)
- Cr:1.0〜10.0wt%、Mo:0.1〜3.5wt%、W:7.5〜10.0wt%、Al:4.0〜8.0wt%、TaおよびNbの少なくとも1種:12.0wt%以下、Hf:0〜2.0wt%、Re:0.1〜5.0wt%、残部がNiと不可避的不純物からなる組成を有することを特徴とするNi基超合金。
- Cr:4.0〜6.0wt%、Mo:1.0〜3.0wt%、W:7.6〜8.5wt%、Al:4.5〜6.0wt%、TaおよびNbの少なくとも1種:4.0〜10.0wt%以下、Hf:0.1〜1.6wt%、Re:1.5〜3.5wt%を含有し、残部がNiと不可避的不純物からなる組成を有することを特徴とする請求項1のNi基超合金。
- 請求項1または2のNi基超合金において、その組成に、さらに、Si:0.3wt%以下およびTi:0.5wt%以下の少なくとも1種以上を含有することを特徴とするNi基超合金。
- 請求項1から3のいずれかのNi基超合金を、普通鋳造法、一方向凝固法、あるいは単結晶凝固法により鋳造することを特徴とするNi基超合金の製造方法。
- 鋳造後に、1260〜1300℃で20分〜2時間の予備熱処理を施し、1300〜1350℃での3〜10時間の溶体化処理、1050〜1150℃での2〜8時間の1次時効処理並びに800〜900℃での10〜24時間の2次時効処理を施すことを特徴とする請求項4のNi基超合金の製造方法。
- 請求項1から3のいずれかのNi基超合金を少くともその構成の一部としていることを特徴とするタービンブレードあるいはタービンベーン部品。
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2007510462A JP5024797B2 (ja) | 2005-03-28 | 2006-03-24 | コバルトフリーのNi基超合金 |
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2005090451 | 2005-03-28 | ||
JP2005090451 | 2005-03-28 | ||
PCT/JP2006/306022 WO2006104059A1 (ja) | 2005-03-28 | 2006-03-24 | コバルトフリーのNi基超合金 |
JP2007510462A JP5024797B2 (ja) | 2005-03-28 | 2006-03-24 | コバルトフリーのNi基超合金 |
Publications (2)
Publication Number | Publication Date |
---|---|
JPWO2006104059A1 JPWO2006104059A1 (ja) | 2008-09-04 |
JP5024797B2 true JP5024797B2 (ja) | 2012-09-12 |
Family
ID=37053317
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2007510462A Expired - Fee Related JP5024797B2 (ja) | 2005-03-28 | 2006-03-24 | コバルトフリーのNi基超合金 |
Country Status (4)
Country | Link |
---|---|
US (1) | US20080240926A1 (ja) |
JP (1) | JP5024797B2 (ja) |
GB (1) | GB2439071B (ja) |
WO (1) | WO2006104059A1 (ja) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP5636639B2 (ja) * | 2009-06-18 | 2014-12-10 | 独立行政法人物質・材料研究機構 | Ni基超合金 |
IT1394975B1 (it) * | 2009-07-29 | 2012-08-07 | Nuovo Pignone Spa | Superlega a base di nichel, componente meccanico realizzato con detta superlega, turbomacchina comprendente tale componente e metodi relativi |
JP6016016B2 (ja) * | 2012-08-09 | 2016-10-26 | 国立研究開発法人物質・材料研究機構 | Ni基単結晶超合金 |
US20160214350A1 (en) | 2012-08-20 | 2016-07-28 | Pratt & Whitney Canada Corp. | Oxidation-Resistant Coated Superalloy |
JP6048805B2 (ja) * | 2012-09-28 | 2016-12-21 | 国立研究開発法人物質・材料研究機構 | Ni基単結晶超合金部品の直接リサイクル法 |
JP6803573B2 (ja) * | 2016-03-07 | 2020-12-23 | 国立研究開発法人物質・材料研究機構 | Ni基一方向凝固合金 |
FR3057880B1 (fr) * | 2016-10-25 | 2018-11-23 | Safran | Superalliage a base de nickel, aube monocristalline et turbomachine |
FR3097879B1 (fr) * | 2019-06-28 | 2021-05-28 | Safran Aircraft Engines | Procede de fabrication d’une piece en superalliage monocristallin |
CN110396624B (zh) * | 2019-08-13 | 2021-04-09 | 上海大学 | 核屏蔽用富硼镍钨基合金材料及其制备方法 |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS6230037A (ja) * | 1985-05-09 | 1987-02-09 | ユナイテツド・テクノロジ−ズ・コ−ポレイシヨン | 耐酸化性を有する物品 |
JPH07145703A (ja) * | 1993-08-06 | 1995-06-06 | Hitachi Ltd | ガスタービン用動翼及びその製造法とそれを用いたガスタービン |
JPH09111382A (ja) * | 1995-10-02 | 1997-04-28 | United Technol Corp <Utc> | 耐クラック伸長性の改善されたニッケル基超合金、それを含んでなる物体及びそれらの製造方法 |
JPH09272933A (ja) * | 1996-02-09 | 1997-10-21 | Hitachi Ltd | 方向性凝固用高強度Ni基超合金 |
JP2000034531A (ja) * | 1998-07-07 | 2000-02-02 | Office Natl Etud Rech Aerospat <Onera> | γ′ソルバスの高い、ニッケル系単結晶超合金 |
JP2000063969A (ja) * | 1998-08-13 | 2000-02-29 | Toshiba Corp | Ni基超合金、その製造方法およびガスタービン部品 |
JP2002146460A (ja) * | 2000-08-30 | 2002-05-22 | National Institute For Materials Science | ニッケル基単結晶超合金、その製造方法およびガスタービン高温部品 |
JP2002167636A (ja) * | 2000-10-30 | 2002-06-11 | United Technol Corp <Utc> | 接合被覆なしに断熱被覆を保持できる低密度耐酸化性超合金材料 |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4116723A (en) * | 1976-11-17 | 1978-09-26 | United Technologies Corporation | Heat treated superalloy single crystal article and process |
US4719080A (en) * | 1985-06-10 | 1988-01-12 | United Technologies Corporation | Advanced high strength single crystal superalloy compositions |
DE69423061T2 (de) * | 1993-08-06 | 2000-10-12 | Hitachi Ltd | Gasturbinenschaufel, Verfahren zur Herstellung derselben sowie Gasturbine mit dieser Schaufel |
DE69701900T2 (de) * | 1996-02-09 | 2000-12-07 | Hitachi Ltd | Hochfeste Superlegierung auf Nickelbasis für gerichtet erstarrte Giesteilen |
GB9718972D0 (en) * | 1996-09-25 | 1997-11-12 | Zeneca Ltd | Chemical compounds |
JP3820430B2 (ja) * | 1998-03-04 | 2006-09-13 | 独立行政法人物質・材料研究機構 | Ni基単結晶超合金、その製造方法およびガスタービン部品 |
EP1184473B1 (en) * | 2000-08-30 | 2005-01-05 | Kabushiki Kaisha Toshiba | Nickel-base single-crystal superalloys, method of manufacturing same and gas turbine high temperature parts made thereof |
US6966956B2 (en) * | 2001-05-30 | 2005-11-22 | National Institute For Materials Science | Ni-based single crystal super alloy |
JP4521610B2 (ja) * | 2002-03-27 | 2010-08-11 | 独立行政法人物質・材料研究機構 | Ni基一方向凝固超合金およびNi基単結晶超合金 |
-
2006
- 2006-03-24 US US11/887,221 patent/US20080240926A1/en not_active Abandoned
- 2006-03-24 WO PCT/JP2006/306022 patent/WO2006104059A1/ja active Application Filing
- 2006-03-24 JP JP2007510462A patent/JP5024797B2/ja not_active Expired - Fee Related
-
2007
- 2007-10-23 GB GB0720743A patent/GB2439071B/en not_active Expired - Fee Related
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS6230037A (ja) * | 1985-05-09 | 1987-02-09 | ユナイテツド・テクノロジ−ズ・コ−ポレイシヨン | 耐酸化性を有する物品 |
JPH07145703A (ja) * | 1993-08-06 | 1995-06-06 | Hitachi Ltd | ガスタービン用動翼及びその製造法とそれを用いたガスタービン |
JPH09111382A (ja) * | 1995-10-02 | 1997-04-28 | United Technol Corp <Utc> | 耐クラック伸長性の改善されたニッケル基超合金、それを含んでなる物体及びそれらの製造方法 |
JPH09272933A (ja) * | 1996-02-09 | 1997-10-21 | Hitachi Ltd | 方向性凝固用高強度Ni基超合金 |
JP2000034531A (ja) * | 1998-07-07 | 2000-02-02 | Office Natl Etud Rech Aerospat <Onera> | γ′ソルバスの高い、ニッケル系単結晶超合金 |
JP2000063969A (ja) * | 1998-08-13 | 2000-02-29 | Toshiba Corp | Ni基超合金、その製造方法およびガスタービン部品 |
JP2002146460A (ja) * | 2000-08-30 | 2002-05-22 | National Institute For Materials Science | ニッケル基単結晶超合金、その製造方法およびガスタービン高温部品 |
JP2002167636A (ja) * | 2000-10-30 | 2002-06-11 | United Technol Corp <Utc> | 接合被覆なしに断熱被覆を保持できる低密度耐酸化性超合金材料 |
Also Published As
Publication number | Publication date |
---|---|
GB2439071B (en) | 2010-09-22 |
GB0720743D0 (en) | 2007-12-05 |
US20080240926A1 (en) | 2008-10-02 |
GB2439071A (en) | 2007-12-19 |
WO2006104059A1 (ja) | 2006-10-05 |
JPWO2006104059A1 (ja) | 2008-09-04 |
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