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 PDF

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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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chromium
alloy
nickel
silicon
molybdenum
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Scheil Margarete
Class Immanuel
Graefen Hubert
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BASF SE
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BASF SE
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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • C22C19/03Alloys based on nickel or cobalt based on nickel
    • C22C19/05Alloys based on nickel or cobalt based on nickel with chromium
    • C22C19/051Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
    • C22C19/055Alloys 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)
US393827A 1961-04-01 1964-08-31 Highly corrosion resistant nickel-chromium-molybdenum alloy with improved resistance o intergranular corrosion Expired - Lifetime US3203792A (en)

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

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US (1) US3203792A (ja)
JP (1) JPS495812B1 (ja)
DE (1) DE1210566B (ja)
GB (1) GB956166A (ja)

Cited By (27)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Patent Citations (2)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

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Publication number Publication date
GB956166A (en) 1964-04-22
DE1210566B (de) 1966-02-10
JPS495812B1 (ja) 1974-02-09

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