EP0386730A1 - Alliage de nickel-chrome-fer - Google Patents
Alliage de nickel-chrome-fer Download PDFInfo
- Publication number
- EP0386730A1 EP0386730A1 EP90104349A EP90104349A EP0386730A1 EP 0386730 A1 EP0386730 A1 EP 0386730A1 EP 90104349 A EP90104349 A EP 90104349A EP 90104349 A EP90104349 A EP 90104349A EP 0386730 A1 EP0386730 A1 EP 0386730A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- alloy
- less
- nicr
- chromium
- nickel
- 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
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Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
-
- 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
- C22C19/058—Alloys based on nickel or cobalt based on nickel with chromium without Mo and W
Definitions
- the invention relates to a thermoformable, austenitic Ni-Cr-Fe alloy with very good oxidation resistance and heat resistance.
- Alloys of this type are used for the production of wires and strips for heating conductor resistors, for the production of support systems in furnaces and for other furnace components and increasingly also for nuclear reactors.
- an alloy of the following composition has become known from DE-PS 30 37 209: 8 to 25% Cr 2.5 to 8% Al 0.005 to 0.04% Y up to 15% of one or more of the elements Mo, Rh, Hf, W, Ta and Nb up to 0.5% of one or more of the elements C, B, Mg, Zr and Ca. up to 1% Si, up to 2% Mn, up to 20% Co, up to 5% Ti, up to 30% Fe, balance Ni.
- the main issue was a well-adhering aluminum oxide layer, which is expediently produced by preoxidation in an oxygen-containing atmosphere at above 1093 ° C.
- an aluminum content of 2.5 to 8% has a strong effect on this alloy ⁇ '-excretion preferably in the temperature range of 600 to 800 ° C. This is associated with a sharp decrease in the ductility of the material, which can lead to material damage, particularly in furnaces that often pass through this temperature range during heating and cooling.
- aluminum contents of 2.5 to 8% and chromium contents of 8 to 25% are not sufficient to only form aluminum oxide in NiCrAl alloys. Rather, the formation of aluminum oxide, chromium oxide, mixed oxides and internal oxidation occurs, a process that leads to a poorer protective effect than the pure chromium oxide, especially in the case of thermal-cyclical stress.
- the alloy can also contain Ti, Al and Y.
- zirconium on the resistance to oxidation is neutralized if zirconium is present as a stable carbide to improve the hot formability.
- the positive influence of zirconium on the hot processing properties can be reversed if coarsely dispersed zirconium carbides are formed due to the non-coordinated addition of zirconium and carbon.
- an alloy from DIN 17 742 (material no. 2.4867) is included Max. 0.15% C Max. 0.3% Al 14 to 19% Cr Max. 0.5% Cu 19 to 25% Fe Max. 2.0% Mn 0.5 to 2.0% Si and at least 59% Ni (including 1% Co) known in the form of wires and tapes for the production of heating conductors and electrical resistors is suitable and is generally manufactured and offered with the following composition: up to 0.08% C 0.1 to 0.2% Al 14.0 to 16.0% Cr up to 0.5% Cu 19.0 to 23.0% Fe 0.1 to 0.8% Mn 1.1 to 1.6% Si 0.001 to 0.04% approx up to 0.05% N up to 0.01% S up to 0.015% P 0.01 to 0.04% lanthanide as cerium mixed metal Rest of nickel.
- This heating conductor alloy is known under the short name NiCr 60 15. Under thermal cycling (according to FIG. 1b, see below) it has service life values that lie between those of the pure Ni-Cr alloy NiCr 80 20 on the one hand and those of the iron-based material NiCr 30 20 on the other hand (see FIG. 2). In addition, despite the higher melting point, the NiCr 60 15 alloy has a lower maximum operating temperature than the pure Ni-Cr alloy and does not have sufficient heat resistance for certain applications.
- the maximum operating temperature which is usually limited to approx. 1200 ° C., can be increased by approx. 50 ° C. if the alloy elements are used there according to the prior art Form of mixed metal added lanthanides replaced by yttrium.
- FIG. 1a shows, in a highly simplified manner, a device for checking the service life of a horizontally arranged, helically wound heating conductor (1) which is clamped at the end in a holder (2) and connected to a voltage source (3).
- the heating conductor consisted of a 50 mm long coil with 12 turns and an inner diameter of 3 mm. The wire diameter was 0.4 mm.
- the heating conductor was switched on and off in alternation of two minutes, whereby the maximum temperature reached during the heating phase was measured without contact using a radiation pyrometer and regulated to a constant value by changing the applied voltage.
- Fig. 1b shows - also greatly simplified - a device for testing the life of a vertically hanging heating conductor wire (4) of one meter in length, which is clamped at its upper end in a holder (5), loaded with a variable weight (6) and with a voltage source (7) is connected.
- FIG. 3 the service life of the material according to the invention determined with a device according to FIG. 1a at a maximum temperature set at 1150 ° C. is below the same conditions measured lifetime of the unmodified material "NiCr 60 15 old" compared.
- the service life was increased from 2900 cycles to 4100 cycles, which means an improvement of over 40%.
- modified alloy at 1200 or 1250 ° C still has 65 or 34% of the life of the base alloy at 1150 ° C is important for practice, which represents a considerable safety reserve, especially with regard to short-term exceeding of the operating temperatures is very desirable in most fields of application.
- a high level of heat resistance is generally required for heating conductor windings, and thus for free-hanging The sagging of the windings can be avoided.
- the heat resistance is based above all on solid-solution strengthening of the basic nickel structure by Cr and Fe and hardening by carbides.
- Ti and Zr and N were alloyed, so that the modified alloy contains nitrides and carbonitrides in addition to the carbides.
- the modified material showed a significantly longer service life.
- Two complete heating elements such as those used for tumble dryers, were charged with 227 volts in 30-second cycles, with which a maximum temperature of 1150 ° C is achieved with a new heating element.
- the comparative alloy "NiCr 60 15 old" only withstood around 130,000 cycles
- the alloy “NiCr 60 15 new” according to the invention has so far endured more than 380,000 cycles in the test which has not yet ended. This almost triples the service life, which speaks for the considerable economic importance of the alloy according to the invention.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Resistance Heating (AREA)
- Contacts (AREA)
- Heat Treatment Of Steel (AREA)
- Dental Preparations (AREA)
- Soft Magnetic Materials (AREA)
- Materials For Medical Uses (AREA)
- Conductive Materials (AREA)
- Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
- Laminated Bodies (AREA)
- Powder Metallurgy (AREA)
- High-Tension Arc-Extinguishing Switches Without Spraying Means (AREA)
- Heat Treatment Of Sheet Steel (AREA)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| AT90104349T ATE89872T1 (de) | 1989-03-09 | 1990-03-07 | Nickel-chrom-eisen-legierung. |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE3907564A DE3907564A1 (de) | 1989-03-09 | 1989-03-09 | Nickel-chrom-eisen-legierung |
| DE3907564 | 1989-03-09 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP0386730A1 true EP0386730A1 (fr) | 1990-09-12 |
| EP0386730B1 EP0386730B1 (fr) | 1993-05-26 |
Family
ID=6375882
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP90104349A Expired - Lifetime EP0386730B1 (fr) | 1989-03-09 | 1990-03-07 | Alliage de nickel-chrome-fer |
Country Status (14)
| Country | Link |
|---|---|
| US (1) | US4997623A (fr) |
| EP (1) | EP0386730B1 (fr) |
| JP (1) | JPH0689427B2 (fr) |
| KR (1) | KR900014619A (fr) |
| AT (1) | ATE89872T1 (fr) |
| AU (1) | AU617242B2 (fr) |
| BR (1) | BR9001105A (fr) |
| CA (1) | CA2011152A1 (fr) |
| DD (1) | DD292479A5 (fr) |
| DE (2) | DE3907564A1 (fr) |
| ES (1) | ES2042102T3 (fr) |
| IE (1) | IE62547B1 (fr) |
| MX (1) | MX172020B (fr) |
| ZA (1) | ZA901579B (fr) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0492517A1 (fr) * | 1990-12-21 | 1992-07-01 | Nippon Steel Corporation | Alliage et tube composite en acier présentant une excellente résistance à la corrosion pour utilisation dans une atmosphère combustible contenant vanadium, sodium, soufre ou chlore |
| EP0690140A1 (fr) * | 1994-06-28 | 1996-01-03 | Krupp VDM GmbH | Alliage réfractaire et forgeable |
| US5851318A (en) * | 1995-06-09 | 1998-12-22 | Krupp Vdm Gmbh | High temperature forgeable alloy |
| WO2005031018A1 (fr) * | 2003-10-02 | 2005-04-07 | Sandvik Intellectual Property Ab | Alliage austenitique fe-cr-ni pour usage haute temperature |
| DE102007005605A1 (de) | 2007-01-31 | 2008-08-07 | Thyssenkrupp Vdm Gmbh | Eisen-Nickel-Chrom-Silizium-Legierung |
| WO2009000230A1 (fr) * | 2007-06-26 | 2008-12-31 | Thyssenkrupp Vdm Gmbh | Alliage fer-nickel-chrome-silicium |
| US8926769B2 (en) | 2005-07-01 | 2015-01-06 | Sandvik Intellectual Property Ab | Ni—Cr—Fe alloy for high-temperature use |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5330590A (en) * | 1993-05-26 | 1994-07-19 | The United States Of America, As Represented By The Administrator Of The National Aeronautics & Space Administration | High temperature creep and oxidation resistant chromium silicide matrix alloy containing molybdenum |
| DK172987B1 (da) * | 1994-12-13 | 1999-11-01 | Man B & W Diesel As | Cylinderelement, nikkelbaseret pålægningslegering og anvendelse af legeringen |
| RU2425901C1 (ru) * | 2009-12-24 | 2011-08-10 | Федеральное Государственное Унитарное Предприятие "Центральный Научно-Исследовательский Институт Конструкционных Материалов "Прометей" (Фгуп "Цнии Км Прометей") | Жаропрочный сплав на никелевой основе |
| CN103153102B (zh) | 2010-09-29 | 2015-04-08 | 霍丁斯瑞典有限公司 | 适于保护头部的安全气囊 |
| DK177487B1 (en) * | 2012-07-06 | 2013-07-15 | Man Diesel & Turbo Deutschland | An exhaust valve spindle for an exhaust valve in an internal combustion engine |
| CN111411265B (zh) * | 2020-03-21 | 2021-11-26 | 交大材料科技(江苏)研究院有限公司 | 一种镍基合金超薄板材 |
| CN112080749B (zh) * | 2020-09-09 | 2022-01-11 | 北京首钢吉泰安新材料有限公司 | 一种镍铬合金丝的表面处理方法和装置 |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2581420A (en) * | 1949-09-23 | 1952-01-08 | Driver Harris Co | Alloys |
| US3865581A (en) * | 1972-01-27 | 1975-02-11 | Nippon Steel Corp | Heat resistant alloy having excellent hot workabilities |
| EP0178785A2 (fr) * | 1984-09-20 | 1986-04-23 | Nippon Yakin Kogyo Kabushiki Kaisha | Alliage à base de nickel, à résistance élevée contre la corrosion intercristalline et la fissuration par corrosion sous tension et à haute usinabilité à chaud |
| EP0183536A2 (fr) * | 1984-11-30 | 1986-06-04 | Nippon Steel Corporation | Acier magnétique à haute résistance à la corrosion et à haute résistance mécanique pour masse-tige de forage et masse-type fabriquée avec cet acier |
| EP0235075A2 (fr) * | 1986-01-20 | 1987-09-02 | Mitsubishi Jukogyo Kabushiki Kaisha | Alliage à base de nickel et procédé pour sa fabrication |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5111013A (en) * | 1974-07-19 | 1976-01-28 | Nippon Steel Corp | Tainetsunitsukerugokinno seizoho |
| US4400211A (en) * | 1981-06-10 | 1983-08-23 | Sumitomo Metal Industries, Ltd. | Alloy for making high strength deep well casing and tubing having improved resistance to stress-corrosion cracking |
| US4400210A (en) * | 1981-06-10 | 1983-08-23 | Sumitomo Metal Industries, Ltd. | Alloy for making high strength deep well casing and tubing having improved resistance to stress-corrosion cracking |
| US4421571A (en) * | 1981-07-03 | 1983-12-20 | Sumitomo Metal Industries, Ltd. | Process for making high strength deep well casing and tubing having improved resistance to stress-corrosion cracking |
| JPS6179742A (ja) * | 1984-09-26 | 1986-04-23 | Mitsubishi Heavy Ind Ltd | 耐熱合金 |
-
1989
- 1989-03-09 DE DE3907564A patent/DE3907564A1/de not_active Withdrawn
-
1990
- 1990-02-28 CA CA002011152A patent/CA2011152A1/fr not_active Abandoned
- 1990-03-01 ZA ZA901579A patent/ZA901579B/xx unknown
- 1990-03-07 EP EP90104349A patent/EP0386730B1/fr not_active Expired - Lifetime
- 1990-03-07 ES ES199090104349T patent/ES2042102T3/es not_active Expired - Lifetime
- 1990-03-07 DE DE9090104349T patent/DE59001527D1/de not_active Expired - Fee Related
- 1990-03-07 MX MX019797A patent/MX172020B/es unknown
- 1990-03-07 AT AT90104349T patent/ATE89872T1/de not_active IP Right Cessation
- 1990-03-08 BR BR909001105A patent/BR9001105A/pt not_active Application Discontinuation
- 1990-03-08 JP JP2055164A patent/JPH0689427B2/ja not_active Expired - Lifetime
- 1990-03-08 IE IE83590A patent/IE62547B1/en not_active IP Right Cessation
- 1990-03-08 DD DD90338513A patent/DD292479A5/de not_active IP Right Cessation
- 1990-03-08 KR KR1019900003077A patent/KR900014619A/ko not_active Ceased
- 1990-03-08 AU AU51173/90A patent/AU617242B2/en not_active Ceased
- 1990-03-09 US US07/491,182 patent/US4997623A/en not_active Expired - Fee Related
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2581420A (en) * | 1949-09-23 | 1952-01-08 | Driver Harris Co | Alloys |
| US3865581A (en) * | 1972-01-27 | 1975-02-11 | Nippon Steel Corp | Heat resistant alloy having excellent hot workabilities |
| EP0178785A2 (fr) * | 1984-09-20 | 1986-04-23 | Nippon Yakin Kogyo Kabushiki Kaisha | Alliage à base de nickel, à résistance élevée contre la corrosion intercristalline et la fissuration par corrosion sous tension et à haute usinabilité à chaud |
| EP0183536A2 (fr) * | 1984-11-30 | 1986-06-04 | Nippon Steel Corporation | Acier magnétique à haute résistance à la corrosion et à haute résistance mécanique pour masse-tige de forage et masse-type fabriquée avec cet acier |
| EP0235075A2 (fr) * | 1986-01-20 | 1987-09-02 | Mitsubishi Jukogyo Kabushiki Kaisha | Alliage à base de nickel et procédé pour sa fabrication |
Non-Patent Citations (1)
| Title |
|---|
| DIN 17742, Februar 1983, Seiten 1-3, Deutsches Institut für Normung e.V., Berlin, DE * |
Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0492517A1 (fr) * | 1990-12-21 | 1992-07-01 | Nippon Steel Corporation | Alliage et tube composite en acier présentant une excellente résistance à la corrosion pour utilisation dans une atmosphère combustible contenant vanadium, sodium, soufre ou chlore |
| EP0690140A1 (fr) * | 1994-06-28 | 1996-01-03 | Krupp VDM GmbH | Alliage réfractaire et forgeable |
| US5851318A (en) * | 1995-06-09 | 1998-12-22 | Krupp Vdm Gmbh | High temperature forgeable alloy |
| WO2005031018A1 (fr) * | 2003-10-02 | 2005-04-07 | Sandvik Intellectual Property Ab | Alliage austenitique fe-cr-ni pour usage haute temperature |
| US10683569B2 (en) | 2003-10-02 | 2020-06-16 | Sandvik Intellectual Property Ab | Austenitic Fe—Cr—Ni alloy for high temperature |
| EP2426226A2 (fr) | 2003-10-02 | 2012-03-07 | Sandvik Intellectual Property AB | Alliage à base de fer et nickel pour utilisation à hautes températures |
| EP2426226A3 (fr) * | 2003-10-02 | 2014-02-26 | Sandvik Intellectual Property AB | Alliage à base de fer et nickel pour utilisation à hautes températures |
| US9260770B2 (en) | 2003-10-02 | 2016-02-16 | Sandvik Intellectual Property Ab | Austenitic FE-CR-NI alloy for high temperature use |
| US8926769B2 (en) | 2005-07-01 | 2015-01-06 | Sandvik Intellectual Property Ab | Ni—Cr—Fe alloy for high-temperature use |
| DE102007005605A1 (de) | 2007-01-31 | 2008-08-07 | Thyssenkrupp Vdm Gmbh | Eisen-Nickel-Chrom-Silizium-Legierung |
| DE102007029400A1 (de) | 2007-06-26 | 2009-01-02 | Thyssenkrupp Vdm Gmbh | Eisen-Nickel-Chrom-Silizium-Legierung |
| DE102007029400B4 (de) * | 2007-06-26 | 2014-05-15 | Outokumpu Vdm Gmbh | Eisen-Nickel-Chrom-Silizium-Legierung |
| WO2009000230A1 (fr) * | 2007-06-26 | 2008-12-31 | Thyssenkrupp Vdm Gmbh | Alliage fer-nickel-chrome-silicium |
Also Published As
| Publication number | Publication date |
|---|---|
| EP0386730B1 (fr) | 1993-05-26 |
| DE59001527D1 (de) | 1993-07-01 |
| KR900014619A (ko) | 1990-10-24 |
| DD292479A5 (de) | 1991-08-01 |
| IE62547B1 (en) | 1995-02-08 |
| IE900835L (en) | 1990-09-09 |
| BR9001105A (pt) | 1991-03-05 |
| CA2011152A1 (fr) | 1990-09-09 |
| DE3907564A1 (de) | 1990-09-13 |
| US4997623A (en) | 1991-03-05 |
| ZA901579B (en) | 1991-01-30 |
| JPH0689427B2 (ja) | 1994-11-09 |
| ES2042102T3 (es) | 1993-12-01 |
| MX172020B (es) | 1993-11-29 |
| JPH0320433A (ja) | 1991-01-29 |
| ATE89872T1 (de) | 1993-06-15 |
| AU5117390A (en) | 1990-09-20 |
| AU617242B2 (en) | 1991-11-21 |
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