US2982646A - Manganese alloys - Google Patents
Manganese alloys Download PDFInfo
- Publication number
- US2982646A US2982646A US788269A US78826959A US2982646A US 2982646 A US2982646 A US 2982646A US 788269 A US788269 A US 788269A US 78826959 A US78826959 A US 78826959A US 2982646 A US2982646 A US 2982646A
- Authority
- US
- United States
- Prior art keywords
- resistance
- alloys
- rod
- alloy
- manganese
- 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
- 229910000914 Mn alloy Inorganic materials 0.000 title description 2
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 19
- 229910052748 manganese Inorganic materials 0.000 description 18
- 239000011572 manganese Substances 0.000 description 18
- 229910052802 copper Inorganic materials 0.000 description 16
- 239000010949 copper Substances 0.000 description 16
- 229910052759 nickel Inorganic materials 0.000 description 16
- 229910045601 alloy Inorganic materials 0.000 description 14
- 239000000956 alloy Substances 0.000 description 14
- 239000011651 chromium Substances 0.000 description 12
- 229910052804 chromium Inorganic materials 0.000 description 11
- 229910052782 aluminium Inorganic materials 0.000 description 6
- 230000007797 corrosion Effects 0.000 description 6
- 238000005260 corrosion Methods 0.000 description 6
- 239000000203 mixture Substances 0.000 description 5
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 4
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 4
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 4
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 229910052742 iron Inorganic materials 0.000 description 2
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 description 2
- 239000012266 salt solution Substances 0.000 description 2
- 150000003839 salts Chemical class 0.000 description 2
- 238000012360 testing method Methods 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 230000004580 weight loss Effects 0.000 description 2
- 230000006698 induction Effects 0.000 description 1
- ZLNQQNXFFQJAID-UHFFFAOYSA-L magnesium carbonate Chemical compound [Mg+2].[O-]C([O-])=O ZLNQQNXFFQJAID-UHFFFAOYSA-L 0.000 description 1
- 229910000021 magnesium carbonate Inorganic materials 0.000 description 1
- 235000014380 magnesium carbonate Nutrition 0.000 description 1
- 239000001095 magnesium carbonate Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C22/00—Alloys based on manganese
Definitions
- This invention relates to corrosion resistant alloys having high coefficient of expansion and high electrical resistance. It relates particularly to alloys containing a major proportion of manganese and lesser amounts of nickel, and one or more of the metals chromium and copper.
- Alloys of the nominal composition 72% Mn, 18% Cu, 10% Ni are widely used in the art because of their high expansion and high resistance. These alloys, however, are not fully corrosion resistant and their high resistance is accompanied by a moderately high temperature coefiicient of resistance. It is the aim of the present invention to provide alloys of equally high expansion and resistance, but with lower temperature coeflicient of resistance and improved corrosion resistance. I have found that alloys of 72% Mn, 1-14% nickel, 418% copper, up to 9% chromium and up to 3% aluminum have improved properties in this respect. Preferred compositions within the composition range of my invention are:
- Example I melt electrolytic manganese with electrolytic nickel, chromium and copper in a magnesite crucible in an induction furnace in the approximate proportions of 72% Mn, 14% Ni, 9% Cr and 5% Cu.
- I cast the alloy in a chill mold and hot roll at 900-950 C. to A1" rod.
- I then reduce this rod by drawing through dies with frequent anneals to 10 mil wire.
- the wire was then found to be ductile and have a specific resistance of 192 microhm Cm and a temperature coefiicient of resistance from 20-150" C. of 0.000008 per C.
- the wire by actual analysis showed 71.86% Mn, 13.13% Ni, 10.93% Cr and 4.08% Cu.
- Example 11 In this example, I proceed as in Example I except that instead of electrolytic manganese, I use aluminothermic manganese containing 1.8% A1.
- the wire produced had a specific resistance of 198 microhm Cm and a temperature coefiicient of resistance from 20-150 C. of 0.00002.
- the loss in weight on shaking in 10% salt solution for 96 hours was 0.28 mg. as compared with 0.56 mg. for
- Example III I prepare an alloy as in Example I except that the nominal composition is 72% Mn, 17% Cu, 10% Ni and 1% Al. This alloy is reduced to 4: inch rod and an.
- the coefiicient of linear expansion is found to be 30 10- C. at 20 C. as compared to a commercial 72-18-10 rod which had a coefiicient of 27.2 lO-
- the specific electrical resistance of this rod was 178 microhm Cm and the temperature coefiicient of electrical resistance was 0.00015 per C.
- the actual analysis of this rod was 71.96% Mn, 17.96% Cu, 9.96% Ni and 1.2% A1.
- a corrosion test of this rod in 1% salt solution showed a weight loss of /2 that of standard 72-18-10 under the same conditions.
- Example IV prepare the alloy of Example IV except that instead of electrolytic manganese, I use aluminothennic manganese with 1.87% A1.
- a rod prepared from this alloy had a coefiicient of linear expansion of 30.2 10 C. Weight loss on corrosion testing in salt water was less than 1% of standard 72-18-10.
- the actual analysis of the alloy was 71.92% Mn, 14.65% Cu, 10.75% Ni, 2.05% I Cr, 1.3% A1 and a trace of iron.
- An alloy consisting of about 16.518% Cu, 9.5- 10.5% Ni. 0.54% Al, and about 72% Mn having a coefiicient of linear expansion at 20 C. of about 30 10- C.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Investigating And Analyzing Materials By Characteristic Methods (AREA)
Description
United States atent O MANGANESE ALLOYS Reginald S. Dean, Hyattsville, Md., assignor to Chicago Development Corporation, Riverdale, Md, a corporation of Delaware N Drawing. Filed Jan. 22, 1959, Ser. No. 788,269
2 Claims. (Cl. 75134) This invention relates to corrosion resistant alloys having high coefficient of expansion and high electrical resistance. It relates particularly to alloys containing a major proportion of manganese and lesser amounts of nickel, and one or more of the metals chromium and copper.
Alloys of the nominal composition 72% Mn, 18% Cu, 10% Ni are widely used in the art because of their high expansion and high resistance. These alloys, however, are not fully corrosion resistant and their high resistance is accompanied by a moderately high temperature coefiicient of resistance. It is the aim of the present invention to provide alloys of equally high expansion and resistance, but with lower temperature coeflicient of resistance and improved corrosion resistance. I have found that alloys of 72% Mn, 1-14% nickel, 418% copper, up to 9% chromium and up to 3% aluminum have improved properties in this respect. Preferred compositions within the composition range of my invention are:
(1) 72% Mn, 10% Ni, 17% Cu, 1% Al (2) 72% Mn, 10% Ni, 16% Cu, 1% Al, 1% Cr (3) 72% Mn, 14% Ni, 9% Cr, Cu
(4) 72% Mn, 13% Ni, 9% Cr, 5% Cu, 1% A1 listed may be varied within the limits of the composition of my invention when it is desired to improve certain properties at the expense of others. In general, increasing aluminum increases the coefficient of expansion, while increasing chromium increases corrosion resistance.
Having now described my invention in its general terms, I will now illustrate my invention by specific examples.
Example I In this example, I melt electrolytic manganese with electrolytic nickel, chromium and copper in a magnesite crucible in an induction furnace in the approximate proportions of 72% Mn, 14% Ni, 9% Cr and 5% Cu. I cast the alloy in a chill mold and hot roll at 900-950 C. to A1" rod. I then reduce this rod by drawing through dies with frequent anneals to 10 mil wire. I beat this wire for 4 hours in an inert atmosphere of N2 at 750 C. The wire was then found to be ductile and have a specific resistance of 192 microhm Cm and a temperature coefiicient of resistance from 20-150" C. of 0.000008 per C. The wire by actual analysis showed 71.86% Mn, 13.13% Ni, 10.93% Cr and 4.08% Cu.
2 Example 11 In this example, I proceed as in Example I except that instead of electrolytic manganese, I use aluminothermic manganese containing 1.8% A1. The wire produced had a specific resistance of 198 microhm Cm and a temperature coefiicient of resistance from 20-150 C. of 0.00002. The loss in weight on shaking in 10% salt solution for 96 hours was 0.28 mg. as compared with 0.56 mg. for
for the product of Example I. Both samples remained bright and were not embrittled by the salt water treatment. The analysis of this wire was 71.90% Mn, 13.05% Ni, 10.95% Cr, 4.10% Cu and a trace of iron.
Example III I prepare an alloy as in Example I except that the nominal composition is 72% Mn, 17% Cu, 10% Ni and 1% Al. This alloy is reduced to 4: inch rod and an.
nealed at 1600" F. The coefiicient of linear expansion is found to be 30 10- C. at 20 C. as compared to a commercial 72-18-10 rod which had a coefiicient of 27.2 lO- The specific electrical resistance of this rod was 178 microhm Cm and the temperature coefiicient of electrical resistance was 0.00015 per C. The actual analysis of this rod was 71.96% Mn, 17.96% Cu, 9.96% Ni and 1.2% A1. A corrosion test of this rod in 1% salt solution showed a weight loss of /2 that of standard 72-18-10 under the same conditions.
Example IV Example V I prepare the alloy of Example IV except that instead of electrolytic manganese, I use aluminothennic manganese with 1.87% A1. A rod prepared from this alloy had a coefiicient of linear expansion of 30.2 10 C. Weight loss on corrosion testing in salt water was less than 1% of standard 72-18-10. The actual analysis of the alloy was 71.92% Mn, 14.65% Cu, 10.75% Ni, 2.05% I Cr, 1.3% A1 and a trace of iron.
What is claimed is:
1. An alloy consisting of about 72% Mn, 14% Ni, 9% Cr, 5% Cu, heated at 750 C. for several hours whereby to reduce the temperature coeflicient of resistance to.
about 0.00002 in the range 20150 C.
2. An alloy consisting of about 16.518% Cu, 9.5- 10.5% Ni. 0.54% Al, and about 72% Mn having a coefiicient of linear expansion at 20 C. of about 30 10- C.
References Cited in the file of this patent UNITED'STATES PATENTS 2,250,470 Dean July 29, 1941 2,287,888 Kroll June 30, 1942 FOREIGN PATENTS 537,333 GreatBritain ..-"u...- June 18, 1941
Claims (1)
- 2. AN ALLOY CONSISTING OF ABOUT 16.5-18% CU, 9.510.5% NI. 0.5-3% AL, AND ABOUT 72% MN HAVING A COEFFICIENT OF LINEAR EXPANSION AT 20*C. OF ABOUT 30X10-6/*C.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US788269A US2982646A (en) | 1959-01-22 | 1959-01-22 | Manganese alloys |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US788269A US2982646A (en) | 1959-01-22 | 1959-01-22 | Manganese alloys |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2982646A true US2982646A (en) | 1961-05-02 |
Family
ID=25143965
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US788269A Expired - Lifetime US2982646A (en) | 1959-01-22 | 1959-01-22 | Manganese alloys |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2982646A (en) |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB537333A (en) * | 1939-09-08 | 1941-06-18 | Cons Mining & Smelting Co | Improvements in or relating to manganese alloys |
| US2250470A (en) * | 1940-09-23 | 1941-07-29 | Chicago Dev Co | Manganese alloy |
| US2287888A (en) * | 1940-01-17 | 1942-06-30 | Electro Metallurg Co | Manganese-base alloys |
-
1959
- 1959-01-22 US US788269A patent/US2982646A/en not_active Expired - Lifetime
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB537333A (en) * | 1939-09-08 | 1941-06-18 | Cons Mining & Smelting Co | Improvements in or relating to manganese alloys |
| US2287888A (en) * | 1940-01-17 | 1942-06-30 | Electro Metallurg Co | Manganese-base alloys |
| US2250470A (en) * | 1940-09-23 | 1941-07-29 | Chicago Dev Co | Manganese alloy |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US4073667A (en) | Processing for improved stress relaxation resistance in copper alloys exhibiting spinodal decomposition | |
| US1620082A (en) | Aluminum alloy containing lithium | |
| US1945297A (en) | Aluminum alloy | |
| JPS60121249A (en) | Stress corrosion resistant aluminum base alloy | |
| US1254987A (en) | Alloy. | |
| US2494736A (en) | Copper base alloy | |
| US4173469A (en) | Magnesium alloys | |
| US2445868A (en) | Copper base alloys | |
| US3993479A (en) | Copper base alloy | |
| US2798806A (en) | Titanium alloy | |
| JPS5918457B2 (en) | Magnesium-based alloy with high mechanical strength and low corrosion tendency | |
| US3941620A (en) | Method of processing copper base alloys | |
| US3392015A (en) | Aluminum-base alloy for use at elevated temperatures | |
| JPS6158541B2 (en) | ||
| US3403997A (en) | Treatment of age-hardenable coppernickel-zinc alloys and product resulting therefrom | |
| US2982646A (en) | Manganese alloys | |
| US3772094A (en) | Copper base alloys | |
| US3985589A (en) | Processing copper base alloys | |
| JP3407054B2 (en) | Copper alloy with excellent heat resistance, strength and conductivity | |
| US3201234A (en) | Alloy and method of producing the same | |
| US4071359A (en) | Copper base alloys | |
| JPS6241302B2 (en) | ||
| US3772095A (en) | Copper base alloys | |
| US1261987A (en) | Method of making aluminum-alloy articles. | |
| US2720459A (en) | Highly wear-resistant zinc base alloy |