US3203792A - Highly corrosion resistant nickel-chromium-molybdenum alloy with improved resistance o intergranular corrosion - Google Patents
Highly corrosion resistant nickel-chromium-molybdenum alloy with improved resistance o intergranular corrosion Download PDFInfo
- Publication number
- US3203792A US3203792A US393827A US39382764A US3203792A US 3203792 A US3203792 A US 3203792A US 393827 A US393827 A US 393827A US 39382764 A US39382764 A US 39382764A US 3203792 A US3203792 A US 3203792A
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- US
- United States
- Prior art keywords
- chromium
- alloy
- nickel
- silicon
- molybdenum
- 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 - Lifetime
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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
- C22C19/055—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 20% but less than 30%
Definitions
- the alloy can also contain from 3 to 4.5%
- nickel-chromium-molybdenum alloys cannot be used in many instances.
- Another object of the invention is -to provide alloys ⁇ which when used for the manufacture of apparatus need not be subjected to a heat treatment after welding.
- the present invention comprises the discovery that a greatly improved nickel-chromium-molybdenum alloy can be produced if the silicon content of the alloy is maintained at an extremely low level. In all Vother phases with a similar composition are also formed.
- Vbut silicon-free alloy nickel 58.8%, chromium 15.5%
- the silicon level should be less than 0.2%
- nickel-chromiummolybdenum alloys preferably should be from 0 to 0.1%, and more preferably from 0 to 0.012%.
- the above described nickel-chromiummolybdenum alloys have a silicon content of 0.5 to 1%. It has been suggested in the past that the presence of silicon is needed for deoxidation of the alloy and to improve the forgeability of the alloys. Silicon is also almost always incorporated in the alloy as an impurity due to the fact that silicon-containing materials are used as deoxidation agents.
- a highly corrosion and heat resistant nickel-chromium-molybdenum alloy is obtained with improved resistance to intergranular corrosion by using: a nickel content of 40 to 65%, preferably of 55 to 60%, part of the nickel, up to a maximum of 20%, if desired being replaced by cobalt; a chrome content of 14 to 26%, preferably 22 to 25%; a molybdenum content of 3 to 18%, preferably 14 to 17%; an iron content of O to 30%, preferably 0 to 7%; a tungsten content of 0 to 5%; a carbon content of not more than 0.1%; a manganese content of up to 3%; a silicon content of from 0 to less than 0.2%; as well as a phosphorus and sulfur content totaling not more than 0.1%, if these are produced from corresponding metals or master alloys which are free of silicon and by subsequent deoxidation with a silicon-free alkaline-earth metal, preferably magnesium, or a silicon-free alkaline-earth metal
- an alkaline-earth metal for instance magnesium, or a siliconfree alkaline-earth metal master alloy, is used as deoxidation agent, whereby the disadvantageous properties of the silicon in the alloy are avoided.
- Alloys deoxidized with magnesium, as an example, show much more sluggish precipitates. Moreover, these cover the grain boundaries only very slowly.
- the alloys with the following composition proved to be especially favorable: 55 to 60% nickel, 22 to 25% chromium, 14 to 17% molybdenum, iron 2%, manganese l%, silicon 0 to 0.19% and carbon 0.08%.
- the range of dangerous precipitates is in addition reduced by the increase of the chromium content as compared with alloys of normal composition Without silicon. They offer, therefore, increased safety to intergranular corrosion, especially after welding.
- the graph set out in FIG. 4 shows the dependency of the thickness of alloy sheeting on its Si-content, i.e., what thickness such sheeting must have to insure that no intercrystalline corrosion occurs when such sheeting is not heated after welding.
- the impairment is negligible with an Si-content of up to 0.1%, but becomes severe even with as low an Si-content as 0.2%.
- the graph indicates the maximum thickness up to which alloy sheeting can be welded without the Welding seam having to be heat-treated.
- the area between the curve and the ordinate pertains to sheeting which will be adequately resistant to intercrystalline corrosion without heat treatment.
- the values for Si-content and thickness fall outside this area, this means that the sheeting must be subjected to a heat treatment after welding.
- the specimens used for the impact tests described in Table 2 were pieces 4 by 3 by 27 mm.
- a nickel-chromiurrr-molybdenum alloy having high corrosion and heat resistance properties said alloy consisting essentially of from 40 to 65 nickel; up to 20% cobalt, the total amount of nickel and cobalt being from 40 to 65%; from 14 to 26% chromium; from 3 to 18% molybdenum; up to 30% iron; up to 5% tungsten; up to 0.1% carbon; up to 3% manganese; and a combined phosphorus and sulfur content of up to 0.1%, said alloy containing less than 0.2% silicon.
- a nickel-chromium-molybdenum alloy having high corrosion and heat resistance properties consisting essentially of from 55 to 60% nickel; up to 20% cobalt, the total amount of nickel and cobalt being from 55 to 60%; from 22 to 25% chromium; from 14 to 17% molybdenum; up to 7% iron; up to 5% tungsten; up to 0.1% carbon; up to 3% manganese; a combined phos- 65 Q3 phorus and sulfur content of up to 0.1%; and up to 0.1% molybdenum, about 1% iron, about 1% manganese, a silicon. maximum of 0.03% carbon, a maximum of 0.04% silicon,
- a nickel-chromium-molybdenum alloy having high balll nickel 3.
- said alloy consisting essentially of from 55 to 60% nickel; from 22 to 25% 5 Referegs Cmd by the Examner chromium; from 14 to 17% molybdenum; up to 2% iron; UNITED STATES PATENTS up to 0.08% Carbon; up t0 1% manganese; and up t0 2,840,469 6/58 Gresham etal 75-171 0.012% silicon. 2,959,480 11/60 Flint 75-171 4.
- a nickel-chromium-molybdenum ailoy having high corrosion and heat resistance properties said alloy con- 10 DAVID L RECK, PIWUY Examinersisting essentially of about 24% chromium, about 14% HYLAND BZQT, Examiner.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Arc Welding In General (AREA)
- Powder Metallurgy (AREA)
- Manufacture And Refinement Of Metals (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DEB61993A DE1210566B (de) | 1961-04-01 | 1961-04-01 | Verfahren zum Herstellen einer hoch-korrosionsbestaendigen und warmfesten Nickel-Chrom-Molybdaen-Legierung mit erhoehter Bestaendigkeit gegen interkristalline Korrosion |
Publications (1)
Publication Number | Publication Date |
---|---|
US3203792A true US3203792A (en) | 1965-08-31 |
Family
ID=6973416
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US393827A Expired - Lifetime US3203792A (en) | 1961-04-01 | 1964-08-31 | Highly corrosion resistant nickel-chromium-molybdenum alloy with improved resistance o intergranular corrosion |
Country Status (4)
Country | Link |
---|---|
US (1) | US3203792A (ja) |
JP (1) | JPS495812B1 (ja) |
DE (1) | DE1210566B (ja) |
GB (1) | GB956166A (ja) |
Cited By (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3473922A (en) * | 1967-07-21 | 1969-10-21 | Carondelet Foundry Co | Corrosion-resistant alloys |
US3510294A (en) * | 1966-07-25 | 1970-05-05 | Int Nickel Co | Corrosion resistant nickel-base alloy |
US3850624A (en) * | 1973-03-06 | 1974-11-26 | Howmet Corp | Method of making superalloys |
US3918964A (en) * | 1973-12-21 | 1975-11-11 | Sorcery Metals Inc | Nickel-base alloys having a low coefficient of thermal expansion |
US4043810A (en) * | 1971-09-13 | 1977-08-23 | Cabot Corporation | Cast thermally stable high temperature nickel-base alloys and casting made therefrom |
US4080201A (en) * | 1973-02-06 | 1978-03-21 | Cabot Corporation | Nickel-base alloys |
US4118223A (en) * | 1971-09-13 | 1978-10-03 | Cabot Corporation | Thermally stable high-temperature nickel-base alloys |
DE2901976A1 (de) * | 1978-02-09 | 1979-08-16 | Cabot Corp | Gegen korrosion und spannungsrisskorrosion bestaendige legierung und ihre verwendung |
DE2904161A1 (de) * | 1978-02-21 | 1979-08-30 | Cabot Corp | Gegen rissbildung unter dem einfluss von wasserstoff und spannungsrissbildung unter dem einfluss von sulfiden und chloriden bestaendige legierung und ihre verwendung |
US4374721A (en) * | 1980-09-29 | 1983-02-22 | Mitsubishi Steel Mfg. Co., Ltd. | Roll having low volume resistivity for electroplating |
DE3312109A1 (de) * | 1982-04-02 | 1983-10-06 | Cabot Corp | Korrosionsbestaendige nickel-eisen-legierung |
US4533414A (en) * | 1980-07-10 | 1985-08-06 | Cabot Corporation | Corrosion-resistance nickel alloy |
US4729799A (en) * | 1986-06-30 | 1988-03-08 | United Technologies Corporation | Stress relief of single crystal superalloy articles |
US5019184A (en) * | 1989-04-14 | 1991-05-28 | Inco Alloys International, Inc. | Corrosion-resistant nickel-chromium-molybdenum alloys |
US5120614A (en) * | 1988-10-21 | 1992-06-09 | Inco Alloys International, Inc. | Corrosion resistant nickel-base alloy |
EP0693565A2 (en) | 1994-07-22 | 1996-01-24 | Haynes International, Inc. | Copper containing Ni-Cr-Mo Alloys |
US5529642A (en) * | 1993-09-20 | 1996-06-25 | Mitsubishi Materials Corporation | Nickel-based alloy with chromium, molybdenum and tantalum |
US20040101433A1 (en) * | 2000-10-20 | 2004-05-27 | Ulrich Brill | Austenitic nickel/chrome/cobalt/molybdenum/tungsten alloy and use thereof |
US6860948B1 (en) | 2003-09-05 | 2005-03-01 | Haynes International, Inc. | Age-hardenable, corrosion resistant Ni—Cr—Mo alloys |
US20050227781A1 (en) * | 2003-09-30 | 2005-10-13 | Fu Sheng Industrial Co., Ltd. | Weight member for a golf club head |
US20060093509A1 (en) * | 2004-11-03 | 2006-05-04 | Paul Crook | Ni-Cr-Mo alloy having improved corrosion resistance |
US20080001115A1 (en) * | 2006-06-29 | 2008-01-03 | Cong Yue Qiao | Nickel-rich wear resistant alloy and method of making and use thereof |
WO2008005030A1 (en) * | 2005-08-30 | 2008-01-10 | Aerogen, Inc. | Aerosol generators with enhanced corrosion resistance |
US20080038148A1 (en) * | 2006-08-09 | 2008-02-14 | Paul Crook | Hybrid corrosion-resistant nickel alloys |
EP1918392A1 (en) * | 2005-08-25 | 2008-05-07 | Solvothermal Crystal Growth Technology Research Al | Nickel-base corrosion-resistant alloy and corrosion-resistant members made of the alloy for the apparatus for reaction with supercritical ammonia |
EP3115472A1 (en) | 2015-07-08 | 2017-01-11 | Haynes International, Inc. | Method for producing two-phase ni-cr-mo alloys |
US11186898B2 (en) | 2020-03-09 | 2021-11-30 | Ati Properties Llc | Corrosion resistant nickel-based alloys |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4129464A (en) * | 1977-08-24 | 1978-12-12 | Cabot Corporation | High yield strength Ni-Cr-Mo alloys and methods of producing the same |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2840469A (en) * | 1954-06-18 | 1958-06-24 | Rolls Royce | Nickel-chromium-molybdenum alloy |
US2959480A (en) * | 1956-11-19 | 1960-11-08 | Int Nickel Co | Corrosion resistant nickel-molybdenum alloys |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE526469C (de) * | 1931-06-08 | Heraeus Vacuumschmelze Akt Ges | Legierung mit hoher Korrosionsbestaendigkeit und insbesondere gleichmaessiger Bestaendigkeit gegen Schwefelsaeure, Salzsaeure und Salpetersaeure | |
CH129646A (fr) * | 1926-09-10 | 1929-01-02 | Daniel Kelly Thomas | Alliage malléable et procédé pour le fabriquer. |
DE597547C (de) * | 1932-11-11 | 1934-05-26 | Heraeus Vacuumschmelze Akt Ges | Verwendung von Chrom-Nickel-Legierungen fuer Gegenstaende mit erhoehten Arbeitstemperaturen |
AT210155B (de) * | 1956-09-24 | 1960-07-25 | Junker Fa O | Korrosionsbeständige Nickel-Molybdän- und Nickel-Molybdän-Chrom-Legierungen |
-
1961
- 1961-04-01 DE DEB61993A patent/DE1210566B/de active Pending
-
1962
- 1962-01-18 GB GB1849/62A patent/GB956166A/en not_active Expired
- 1962-02-13 JP JP37009218A patent/JPS495812B1/ja active Pending
-
1964
- 1964-08-31 US US393827A patent/US3203792A/en not_active Expired - Lifetime
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2840469A (en) * | 1954-06-18 | 1958-06-24 | Rolls Royce | Nickel-chromium-molybdenum alloy |
US2959480A (en) * | 1956-11-19 | 1960-11-08 | Int Nickel Co | Corrosion resistant nickel-molybdenum alloys |
Cited By (37)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3510294A (en) * | 1966-07-25 | 1970-05-05 | Int Nickel Co | Corrosion resistant nickel-base alloy |
US3473922A (en) * | 1967-07-21 | 1969-10-21 | Carondelet Foundry Co | Corrosion-resistant alloys |
US4043810A (en) * | 1971-09-13 | 1977-08-23 | Cabot Corporation | Cast thermally stable high temperature nickel-base alloys and casting made therefrom |
US4118223A (en) * | 1971-09-13 | 1978-10-03 | Cabot Corporation | Thermally stable high-temperature nickel-base alloys |
US4080201A (en) * | 1973-02-06 | 1978-03-21 | Cabot Corporation | Nickel-base alloys |
US3850624A (en) * | 1973-03-06 | 1974-11-26 | Howmet Corp | Method of making superalloys |
US3918964A (en) * | 1973-12-21 | 1975-11-11 | Sorcery Metals Inc | Nickel-base alloys having a low coefficient of thermal expansion |
US4168188A (en) * | 1978-02-09 | 1979-09-18 | Cabot Corporation | Alloys resistant to localized corrosion, hydrogen sulfide stress cracking and stress corrosion cracking |
DE2901976A1 (de) * | 1978-02-09 | 1979-08-16 | Cabot Corp | Gegen korrosion und spannungsrisskorrosion bestaendige legierung und ihre verwendung |
DE2904161A1 (de) * | 1978-02-21 | 1979-08-30 | Cabot Corp | Gegen rissbildung unter dem einfluss von wasserstoff und spannungsrissbildung unter dem einfluss von sulfiden und chloriden bestaendige legierung und ihre verwendung |
US4171217A (en) * | 1978-02-21 | 1979-10-16 | Cabot Corporation | Corrosion-resistant nickel alloy |
US4533414A (en) * | 1980-07-10 | 1985-08-06 | Cabot Corporation | Corrosion-resistance nickel alloy |
US4374721A (en) * | 1980-09-29 | 1983-02-22 | Mitsubishi Steel Mfg. Co., Ltd. | Roll having low volume resistivity for electroplating |
DE3312109A1 (de) * | 1982-04-02 | 1983-10-06 | Cabot Corp | Korrosionsbestaendige nickel-eisen-legierung |
US4729799A (en) * | 1986-06-30 | 1988-03-08 | United Technologies Corporation | Stress relief of single crystal superalloy articles |
US5120614A (en) * | 1988-10-21 | 1992-06-09 | Inco Alloys International, Inc. | Corrosion resistant nickel-base alloy |
US5019184A (en) * | 1989-04-14 | 1991-05-28 | Inco Alloys International, Inc. | Corrosion-resistant nickel-chromium-molybdenum alloys |
US5529642A (en) * | 1993-09-20 | 1996-06-25 | Mitsubishi Materials Corporation | Nickel-based alloy with chromium, molybdenum and tantalum |
US6280540B1 (en) | 1994-07-22 | 2001-08-28 | Haynes International, Inc. | Copper-containing Ni-Cr-Mo alloys |
EP0693565A2 (en) | 1994-07-22 | 1996-01-24 | Haynes International, Inc. | Copper containing Ni-Cr-Mo Alloys |
US20040101433A1 (en) * | 2000-10-20 | 2004-05-27 | Ulrich Brill | Austenitic nickel/chrome/cobalt/molybdenum/tungsten alloy and use thereof |
US6860948B1 (en) | 2003-09-05 | 2005-03-01 | Haynes International, Inc. | Age-hardenable, corrosion resistant Ni—Cr—Mo alloys |
GB2405643A (en) * | 2003-09-05 | 2005-03-09 | Haynes Internat Inc | A nickel-chromium-molybdenum alloy |
US20050053513A1 (en) * | 2003-09-05 | 2005-03-10 | Pike Lee M. | Age-hardenable, corrosion resistant ni-cr-mo alloys |
US20050227781A1 (en) * | 2003-09-30 | 2005-10-13 | Fu Sheng Industrial Co., Ltd. | Weight member for a golf club head |
US20060093509A1 (en) * | 2004-11-03 | 2006-05-04 | Paul Crook | Ni-Cr-Mo alloy having improved corrosion resistance |
EP1918392A1 (en) * | 2005-08-25 | 2008-05-07 | Solvothermal Crystal Growth Technology Research Al | Nickel-base corrosion-resistant alloy and corrosion-resistant members made of the alloy for the apparatus for reaction with supercritical ammonia |
EP1918392A4 (en) * | 2005-08-25 | 2013-09-25 | Furuya Metal Co Ltd | NICKEL-BASED CORROSION RESISTANT ALLOY AND CORROSION-RESISTANT ELEMENTS MADE THEREFROM FOR REACTION APPARATUS USING SUPERCRITICAL AMMONIA |
WO2008005030A1 (en) * | 2005-08-30 | 2008-01-10 | Aerogen, Inc. | Aerosol generators with enhanced corrosion resistance |
US20080001115A1 (en) * | 2006-06-29 | 2008-01-03 | Cong Yue Qiao | Nickel-rich wear resistant alloy and method of making and use thereof |
US8613886B2 (en) | 2006-06-29 | 2013-12-24 | L. E. Jones Company | Nickel-rich wear resistant alloy and method of making and use thereof |
US7785532B2 (en) | 2006-08-09 | 2010-08-31 | Haynes International, Inc. | Hybrid corrosion-resistant nickel alloys |
US20080038148A1 (en) * | 2006-08-09 | 2008-02-14 | Paul Crook | Hybrid corrosion-resistant nickel alloys |
EP3115472A1 (en) | 2015-07-08 | 2017-01-11 | Haynes International, Inc. | Method for producing two-phase ni-cr-mo alloys |
US9970091B2 (en) | 2015-07-08 | 2018-05-15 | Haynes International, Inc. | Method for producing two-phase Ni—Cr—Mo alloys |
US11186898B2 (en) | 2020-03-09 | 2021-11-30 | Ati Properties Llc | Corrosion resistant nickel-based alloys |
US12000023B2 (en) | 2020-03-09 | 2024-06-04 | Ati Properties Llc | Methods of making corrosion resistant nickel-based alloys |
Also Published As
Publication number | Publication date |
---|---|
GB956166A (en) | 1964-04-22 |
DE1210566B (de) | 1966-02-10 |
JPS495812B1 (ja) | 1974-02-09 |
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