US2238160A - Method of making nickel-chromium alloys - Google Patents
Method of making nickel-chromium alloys Download PDFInfo
- Publication number
- US2238160A US2238160A US253733A US25373339A US2238160A US 2238160 A US2238160 A US 2238160A US 253733 A US253733 A US 253733A US 25373339 A US25373339 A US 25373339A US 2238160 A US2238160 A US 2238160A
- Authority
- US
- United States
- Prior art keywords
- nickel
- chromium
- alloys
- chromium alloys
- making 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.)
- Expired - Lifetime
Links
- 239000000788 chromium alloy Substances 0.000 title description 6
- 238000004519 manufacturing process Methods 0.000 title description 6
- 229910000623 nickel–chromium alloy Inorganic materials 0.000 title description 6
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 36
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 19
- 229910052759 nickel Inorganic materials 0.000 description 18
- 239000011651 chromium Substances 0.000 description 17
- 229910052804 chromium Inorganic materials 0.000 description 15
- 229910045601 alloy Inorganic materials 0.000 description 6
- 239000000956 alloy Substances 0.000 description 6
- 238000005275 alloying Methods 0.000 description 4
- 229910052782 aluminium Inorganic materials 0.000 description 4
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 4
- 238000002844 melting Methods 0.000 description 4
- 230000008018 melting Effects 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 229910000990 Ni alloy Inorganic materials 0.000 description 3
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 3
- 238000003723 Smelting Methods 0.000 description 3
- 238000010438 heat treatment Methods 0.000 description 3
- 230000003647 oxidation Effects 0.000 description 3
- 238000007254 oxidation reaction Methods 0.000 description 3
- 229910052710 silicon Inorganic materials 0.000 description 3
- 239000010703 silicon Substances 0.000 description 3
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- 229910000599 Cr alloy Inorganic materials 0.000 description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 description 1
- 241000393496 Electra Species 0.000 description 1
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 1
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 1
- 229910052791 calcium Inorganic materials 0.000 description 1
- 239000011575 calcium Substances 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- VNNRSPGTAMTISX-UHFFFAOYSA-N chromium nickel Chemical compound [Cr].[Ni] VNNRSPGTAMTISX-UHFFFAOYSA-N 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000006866 deterioration Effects 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 229910052748 manganese Inorganic materials 0.000 description 1
- 239000011572 manganese Substances 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 229910000480 nickel oxide Inorganic materials 0.000 description 1
- GNRSAWUEBMWBQH-UHFFFAOYSA-N oxonickel Chemical class [Ni]=O GNRSAWUEBMWBQH-UHFFFAOYSA-N 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 238000010079 rubber tapping Methods 0.000 description 1
- 239000002893 slag Substances 0.000 description 1
- 229910052726 zirconium Inorganic materials 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/02—Making non-ferrous alloys by melting
- C22C1/023—Alloys based on nickel
Definitions
- the present invention relates to a process of 1 Claim.
- Such nickel-chromium alloys usually contain at least 60% nickel and or more chromium, and are employed extensively in articles intended to resist corrosion and oxidation. They are especially valuable as heating elements in electrical appliances because of their high electrical resistivity and excellent resistance to oxidation and deterioration at high temperatures.
- the present practice in manufacturing nickelchromium alloys is to add pieces of chromium metal to a bath of molten nickel and to superheat the bath to a degree necessary for complete solution and alloying of the chromium.
- the alloying action under these conditions is slow because of the wide difference in melting points of the nickel and chromium. Considerable time or considerable super-heating is required for satisfactory alloying, a result of which the melt may become contaminated by the inclusion of gases, carbon from electrodes, and oxidation products of the chromium. It is the usual procedure to deoxidize and to degasify the meltin order to refine it to the necessary degree of P ty.
- the present invention resides in a novel process of making alloys of nickel and chromium in which a high-chromium prealloy of chromium and nickel is added to a bath of molten nickel.
- the prealloy has a melting point of about 1650 (2., which is substantially lower than that of chromium metal. It dissolves in nickel much more readily than does chromium metal, and alloying is accomplished in much less time and at lower temperatures with consequent production of alloys of superior quality.
- This method of producing nickelchromium alloys is less expensive than the present practice because less time and heating are required and because less extensive deoxidizing and degasifying operations are needed.
- the chromium content of the prealloy may vary between about 60% and about 97% and the nickel content may accordingly vary between 40% and 3%. Part of the nickel may be replaced by iron and/or manganese. Carbon may be present in the prealloy up to about 0.5%, silicon up to about 3%. and aluminum, calcium, and/or zirconium up to 5% and preferably up to about 1%.
- the compositions of typical prealloys according to the present invention are given in the following table by way of example:
- the prealloy may be made by aluminum or silicon reduction of chromium and nickel oxides,
- the prealloy may be tapped readily from the smelting furnace which is a distinct advantage over the use of chromium because of the dlfliculty of attaining suflicient temperature and fluidity when using metallic chromium.
- Treatment of the prealloy with deoxidizers or addition agents is easily accomplished because of its high fluidity at smelting temperatures and in this manner a first-stage alloy high in aluminum or silicon can be" refined in the fluid state to the final aluminum or silcon content desired with comparative freedom from slag and oxide inclusions.
- Method of making nickel-chromium alloys con-- taining at least 60% nickel and over 10% chromium without prolonged superheating of the principal part of the nickel which comprises reducing oxides of nickel'and chromium in prw portions to yield an alloy containing between 10% and 24% nickel and the reminder chromim'and tapping such alloy and add-int it to a bath of nickel held at a temperature between about 1650 C. and the melting point 01 the nickel.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Manufacture And Refinement Of Metals (AREA)
Description
"Patented Apr. 15, 1941 METHOD OF MAKING NICKEL-CHROMIUM ALLOYS Ernest Floyd Doom, New Rochelle, N. Y., assignor to Electra Metallurgical Company, a corporation of West Virginia No Drawing. Application January 31, 1939, Serial No. 253,733
The present invention relates to a process of 1 Claim.
making alloys of nickel and chromium in which the nickel content is in excess of the chromium content. Such nickel-chromium alloys usually contain at least 60% nickel and or more chromium, and are employed extensively in articles intended to resist corrosion and oxidation. They are especially valuable as heating elements in electrical appliances because of their high electrical resistivity and excellent resistance to oxidation and deterioration at high temperatures.
The present practice in manufacturing nickelchromium alloys is to add pieces of chromium metal to a bath of molten nickel and to superheat the bath to a degree necessary for complete solution and alloying of the chromium. The alloying action under these conditions is slow because of the wide difference in melting points of the nickel and chromium. Considerable time or considerable super-heating is required for satisfactory alloying, a result of which the melt may become contaminated by the inclusion of gases, carbon from electrodes, and oxidation products of the chromium. It is the usual procedure to deoxidize and to degasify the meltin order to refine it to the necessary degree of P ty.
In its general aspect, the present invention resides in a novel process of making alloys of nickel and chromium in which a high-chromium prealloy of chromium and nickel is added to a bath of molten nickel. The prealloy has a melting point of about 1650 (2., which is substantially lower than that of chromium metal. It dissolves in nickel much more readily than does chromium metal, and alloying is accomplished in much less time and at lower temperatures with consequent production of alloys of superior quality. This method of producing nickelchromium alloys is less expensive than the present practice because less time and heating are required and because less extensive deoxidizing and degasifying operations are needed.
The chromium content of the prealloy may vary between about 60% and about 97% and the nickel content may accordingly vary between 40% and 3%. Part of the nickel may be replaced by iron and/or manganese. Carbon may be present in the prealloy up to about 0.5%, silicon up to about 3%. and aluminum, calcium, and/or zirconium up to 5% and preferably up to about 1%. The compositions of typical prealloys according to the present invention are given in the following table by way of example:
Pct. Pct. Pct. Pct. Pct. Pct. Pet. 24. 06 12. 83 11.13 14. 62 14. 22 14.40 12.97 74. 02 84. 48 84. 79 84. 82. 30 82. 70 83. 67 0. 89 0. 61 0. 84 0. 61 0. 69 0. 64 0. 64 0.07 l. 21 l. 48 0. 21 2. l. 69 2. 27 0. l4 0. 16 0. 13 0. 06 0. 073 0. 08 0. 08 None 0. 08 1. None 0. 04 0. 04 0. 04
It has been found that a chromium-nickel alloy containing from 10% to 20% nickel is somewhat more brittle and hence more readily crushed than alloys of higher nickel content. Ready crushability is advantageous in facilitating the production of small pieces suitable for addition to the furnace.
The prealloy may be made by aluminum or silicon reduction of chromium and nickel oxides,
with chromium or nickel possibly also present in the smelting batch in metal or alloy form. Because of its lower melting point as compared with chromium, the prealloy may be tapped readily from the smelting furnace which is a distinct advantage over the use of chromium because of the dlfliculty of attaining suflicient temperature and fluidity when using metallic chromium. Treatment of the prealloy with deoxidizers or addition agents is easily accomplished because of its high fluidity at smelting temperatures and in this manner a first-stage alloy high in aluminum or silicon can be" refined in the fluid state to the final aluminum or silcon content desired with comparative freedom from slag and oxide inclusions.
I claim:
Method of making nickel-chromium alloys con-- taining at least 60% nickel and over 10% chromium without prolonged superheating of the principal part of the nickel, which comprises reducing oxides of nickel'and chromium in prw portions to yield an alloy containing between 10% and 24% nickel and the reminder chromim'and tapping such alloy and add-int it to a bath of nickel held at a temperature between about 1650 C. and the melting point 01 the nickel.
ERNEST I". DOOM.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US253733A US2238160A (en) | 1939-01-31 | 1939-01-31 | Method of making nickel-chromium alloys |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US253733A US2238160A (en) | 1939-01-31 | 1939-01-31 | Method of making nickel-chromium alloys |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2238160A true US2238160A (en) | 1941-04-15 |
Family
ID=22961497
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US253733A Expired - Lifetime US2238160A (en) | 1939-01-31 | 1939-01-31 | Method of making nickel-chromium alloys |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2238160A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2607170A (en) * | 1950-06-15 | 1952-08-19 | Owens Corning Fiberglass Corp | Apparatus for contacting molten glass |
| US2809139A (en) * | 1952-10-24 | 1957-10-08 | Research Corp | Method for heat treating chromium base alloy |
| US3640777A (en) * | 1968-02-08 | 1972-02-08 | Int Nickel Co | Heat treatment of high-chromium alloys to improve ductility |
| US6632299B1 (en) | 2000-09-15 | 2003-10-14 | Cannon-Muskegon Corporation | Nickel-base superalloy for high temperature, high strain application |
-
1939
- 1939-01-31 US US253733A patent/US2238160A/en not_active Expired - Lifetime
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2607170A (en) * | 1950-06-15 | 1952-08-19 | Owens Corning Fiberglass Corp | Apparatus for contacting molten glass |
| US2809139A (en) * | 1952-10-24 | 1957-10-08 | Research Corp | Method for heat treating chromium base alloy |
| US3640777A (en) * | 1968-02-08 | 1972-02-08 | Int Nickel Co | Heat treatment of high-chromium alloys to improve ductility |
| US6632299B1 (en) | 2000-09-15 | 2003-10-14 | Cannon-Muskegon Corporation | Nickel-base superalloy for high temperature, high strain application |
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