US2246886A - Manganese-base alloy and method of making and using the same - Google Patents
Manganese-base alloy and method of making and using the same Download PDFInfo
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- US2246886A US2246886A US316543A US31654340A US2246886A US 2246886 A US2246886 A US 2246886A US 316543 A US316543 A US 316543A US 31654340 A US31654340 A US 31654340A US 2246886 A US2246886 A US 2246886A
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- 229910045601 alloy Inorganic materials 0.000 title description 43
- 239000000956 alloy Substances 0.000 title description 43
- 238000004519 manufacturing process Methods 0.000 title description 5
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 35
- 229910052802 copper Inorganic materials 0.000 description 29
- 239000010949 copper Substances 0.000 description 29
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 27
- 239000011572 manganese Substances 0.000 description 18
- 229910052759 nickel Inorganic materials 0.000 description 18
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 16
- 229910052748 manganese Inorganic materials 0.000 description 16
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 10
- 238000005266 casting Methods 0.000 description 9
- 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 7
- 229910000914 Mn alloy Inorganic materials 0.000 description 6
- 229910052751 metal Inorganic materials 0.000 description 6
- 239000002184 metal Substances 0.000 description 6
- 229910000881 Cu alloy Inorganic materials 0.000 description 5
- 229910052742 iron Inorganic materials 0.000 description 5
- 238000010791 quenching Methods 0.000 description 5
- 230000000171 quenching effect Effects 0.000 description 5
- 230000009466 transformation Effects 0.000 description 5
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 4
- 238000007792 addition Methods 0.000 description 4
- HPDFFVBPXCTEDN-UHFFFAOYSA-N copper manganese Chemical compound [Mn].[Cu] HPDFFVBPXCTEDN-UHFFFAOYSA-N 0.000 description 4
- 238000010438 heat treatment Methods 0.000 description 3
- 229910052750 molybdenum Inorganic materials 0.000 description 3
- 238000005096 rolling process Methods 0.000 description 3
- 229910052710 silicon Inorganic materials 0.000 description 3
- 230000000087 stabilizing effect Effects 0.000 description 3
- 238000005482 strain hardening Methods 0.000 description 3
- 239000010936 titanium Substances 0.000 description 3
- 229910052719 titanium Inorganic materials 0.000 description 3
- 229910052725 zinc Inorganic materials 0.000 description 3
- 239000011701 zinc Substances 0.000 description 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 2
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 2
- 238000005275 alloying Methods 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 229910052790 beryllium Inorganic materials 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 229910052804 chromium Inorganic materials 0.000 description 2
- 239000011651 chromium Substances 0.000 description 2
- 239000010941 cobalt Substances 0.000 description 2
- 229910017052 cobalt Inorganic materials 0.000 description 2
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 2
- 230000002349 favourable effect Effects 0.000 description 2
- 238000005098 hot rolling Methods 0.000 description 2
- AMWRITDGCCNYAT-UHFFFAOYSA-L hydroxy(oxo)manganese;manganese Chemical compound [Mn].O[Mn]=O.O[Mn]=O AMWRITDGCCNYAT-UHFFFAOYSA-L 0.000 description 2
- 239000000155 melt Substances 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- 229910052757 nitrogen Inorganic materials 0.000 description 2
- 230000003647 oxidation Effects 0.000 description 2
- 238000007254 oxidation reaction Methods 0.000 description 2
- 230000001681 protective effect Effects 0.000 description 2
- 229910052709 silver Inorganic materials 0.000 description 2
- 229910052715 tantalum Inorganic materials 0.000 description 2
- 238000007669 thermal treatment Methods 0.000 description 2
- 229910052718 tin Inorganic materials 0.000 description 2
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 2
- 229910052721 tungsten Inorganic materials 0.000 description 2
- 239000010937 tungsten Substances 0.000 description 2
- ZSLUVFAKFWKJRC-IGMARMGPSA-N 232Th Chemical compound [232Th] ZSLUVFAKFWKJRC-IGMARMGPSA-N 0.000 description 1
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 description 1
- 229910000531 Co alloy Inorganic materials 0.000 description 1
- 229910001374 Invar Inorganic materials 0.000 description 1
- 229910001030 Iron–nickel alloy Inorganic materials 0.000 description 1
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 1
- 229910021380 Manganese Chloride Inorganic materials 0.000 description 1
- GLFNIEUTAYBVOC-UHFFFAOYSA-L Manganese chloride Chemical compound Cl[Mn]Cl GLFNIEUTAYBVOC-UHFFFAOYSA-L 0.000 description 1
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 1
- 229910000990 Ni alloy Inorganic materials 0.000 description 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- 229910052776 Thorium Inorganic materials 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- KGWWEXORQXHJJQ-UHFFFAOYSA-N [Fe].[Co].[Ni] Chemical compound [Fe].[Co].[Ni] KGWWEXORQXHJJQ-UHFFFAOYSA-N 0.000 description 1
- 229910001615 alkaline earth metal halide Inorganic materials 0.000 description 1
- 238000000137 annealing Methods 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 229910002056 binary alloy Inorganic materials 0.000 description 1
- 229910052791 calcium Inorganic materials 0.000 description 1
- 239000011575 calcium Substances 0.000 description 1
- 239000004927 clay Substances 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- UTICYDQJEHVLJZ-UHFFFAOYSA-N copper manganese nickel Chemical compound [Mn].[Ni].[Cu] UTICYDQJEHVLJZ-UHFFFAOYSA-N 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000004821 distillation Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000004907 flux Effects 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 239000001307 helium Substances 0.000 description 1
- 229910052734 helium Inorganic materials 0.000 description 1
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 125000004435 hydrogen atom Chemical class [H]* 0.000 description 1
- 230000000266 injurious effect Effects 0.000 description 1
- DALUDRGQOYMVLD-UHFFFAOYSA-N iron manganese Chemical compound [Mn].[Fe] DALUDRGQOYMVLD-UHFFFAOYSA-N 0.000 description 1
- 229910000833 kovar Inorganic materials 0.000 description 1
- 229910052744 lithium Inorganic materials 0.000 description 1
- 239000011565 manganese chloride Substances 0.000 description 1
- 229940099607 manganese chloride Drugs 0.000 description 1
- 235000002867 manganese chloride Nutrition 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 238000003303 reheating Methods 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 239000002893 slag Substances 0.000 description 1
- 229910000679 solder Inorganic materials 0.000 description 1
- 238000005476 soldering Methods 0.000 description 1
- 239000006104 solid solution Substances 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D21/00—Casting non-ferrous metals or metallic compounds so far as their metallurgical properties are of importance for the casting procedure; Selection of compositions therefor
- B22D21/002—Castings of light metals
- B22D21/007—Castings of light metals with low melting point, e.g. Al 659 degrees C, Mg 650 degrees C
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C28/00—Alloys based on a metal not provided for in groups C22C5/00 - C22C27/00
Definitions
- the invention relates to alloys containing a large proportion of manganese, and has for one of its principal objects the provision of manganese alloys which may be cold-worked. Another object is to provide a method of making and treating such alloys to improve their amenability to cold-working.
- the present invention is based on the discovery that the above-described conversion of ductile manganese to the brittle form may be to a great extent prevented by means of certain alloying additions which act to inhibit such conversion, and that when suitable thermal treat ment is employed, the resulting alloys may be kept in a ductile condition at room temperature.
- the alloying addition producing the most favorable results is copper in a proportion of about 1% to 60%, preferably between 10% and 35%, of the alloy.
- the cast ingots still hot, are hot rolledin the gamma-beta regions until the grain has been broken down.
- the l5 thinner cross sections may then be rapidly cooled,
- ingots .50 mm. of a manganese alloy containing 15% or more copper are rolled at 950 G. into sheets 2 mm. thick which may then be air cooled.
- Cold working may be done within wide limits. intermediate anneals being effected by rapid heating to within the beta or gamma field, followed by quenching.
- manganese-copper alloys are relatively stable, they nevertheless tend to become brittle when heated to certain moderately.
- the nese alloy becomes brittle in the same time at 500 C.
- the iron, 65% manganese alloy can stand up to 450 C.
- Clay crucibles may be used in preparing the alloy.
- the hot rolling of the alloys of the invention must be conducted entirely aboife the beta-alpha transformation temperature, and preferably is commenced while the alloy is in the gamma form. Otherwise, the metal tends to be redshort or cold-short.
- the beta-alpha point is causing embrittlement requires a certain time at the critical temperature, therefore no brittleness appears when the alloy passes rapidly through the critical temperature range, and it is possible so to control the embrittlement as to exploit it for the purpose of increasing the hardness and strength of the alloy.
- a binary manganese-copper alloy containing 15% copper was rolled at 900 C. and quenched.
- the suitable proportions of nickel and copper preferably within the range of 0.5% to 10% nickel and 5% to 40% copper, the tendency to become embrittled at moderately elevated temperatures within the alpha field is suppressed and may be substantially eliminated.
- an alloy containing 6.9% Ni, 5.1% Cu, rest Mn is substantially entirely stable, and after working and quenching from 950 C. has a tensile strength of 39.9 ken/mm. with 20% elongation and a Brinell hardness of 105.
- the alloys containing the higher percentages of copper tolerate the higher nickel additions.
- Aluminum may be added to the alloys in an amount suitably between 0.1% and (the higher percentages preferably being used with the higher copper percentages) to deoxidize them, thereby improving their workability. Furthermore, aluminum protects the alloy against oxidation at high temperatures, and during melting and casting it forms a superficial film of oxide which hinders oxidation and nitrogen pick-up. It promotes the existence of a surface favorable for rolling.
- the aluminum-5 containing alloys may advantageously be made from manganese produced by alumino-thermic reduction.
- Zinc may also be added in a proportion up to 20%, the copper preferably being correspondingly reduced.
- a more narrowly circumscribed limit for such alloys is between 5% and 35% copper and 1% to 8% zinc.
- an alloy containing 10% Cu, 5% Zn, rest Mn, after rolling and quenching from 1050 C. and subsequent cold working had a tensile strength of 47.7 kg./mm. with 13.1% elongation and a Brinell hardness of 131.
- Other metals may be present, as one or more of iron, cobalt, tungsten, or chromium, in 'a total percentage up to 5% but preferably not over about 2%.
- the elements Si, Sn, Ti, Ta, Mo, Ag, Ce, Mg, and Be appear to be injurious and should ordinarily not exceed 0.5% Si, 1% Sn, 2% Ti, 5% Ta, 2% Mo, 2% Ag, 2% Ce, Mg, or 0.5% Be.
- Calcium, lithium, or thorium may be used in a proportion of 1% or more as a deoxidizer.
- the alloys containing the higher percentages of copper or of copperand nickel will tolerate the higher amounts of such other metals. It is preferred that the silicon content be less than 0.15%.
- Iron in a proportion between 30% and 50% may be used as the stabilizing metal instead of the copper; but the stabilizing effects oi iron are not, in general, as strong as those produced by copper.
- the beta-alpha point is about 600 to 742 C. in the case of the iron-manganese alloys.
- the alloys of the invention preferably contain less than 0.2% carbon and should usually contain less than 0.05% of this element, although somewhat higher carbon contents will on occasion be permissible. It is also preferred that the manganese content be at least 50%, although on occasion it may be as low as 40%.
- the alloys containing over 30% copper may easily be soldered with'. either soft or hard solder.
- the alloys of the invention have a particularly high electrical resistivity, generally between about 1.2 and 2 ohm/m./mm.
- the binary manganese-copper alloy containing 40% copper has a resistivity slightly more than 2 ohm/m./mm.*
- the binary alloys age-harden, with a decrease in electrical resistivity.
- the stable manganese-copper nickel alloys are particularly useful as resistance alloys. For example. an alloy containing about 37% copper, 8% nickel, rest manganese, has an electrical resistivity of about 1.8 ohmlmlmmfi, three times that of commercial resistance-wires of copperbase alloys. while an alloy containing 5% copper,
- the highest resistivities are obtained in the range of 30% to copper, and the addition of 6% to 8% nickel is suiiicient to stabilize the alloy. If the alloy is to be used at temperatures below 100 C., the nickel content may be as low as 0.5% or be eliminated entirely. If de sired, the nickel content may be raised as high as 20%. Nickel only slightly aifects the resistivity, the latter being determined chiefly by the solid solution of manganese and copper.
- Nickel does not have any. pronounced effect on the temperature coeflicient of electrical resistivity.
- the alloys of the invention also have an unusually high coeflicient of expansion, and are accordingly useful as thermoregulatorelements. If such elements are to be used at elevated temperatures, the stable ternary. manganese-copper,- nickel alloys containing about 4% to 20%, preferably 5% to 12%, nickel are most suitable.
- the temperature-expansion curve is almost straight, is without breaks, and is reproducible as often as desired.
- Bimetallic elements may be formed by fastening a strip of metal having a low thermal expansion, e. g. an iron-nickel alloy of the Invar type, or an iron-nickel-cobalt alloy of the Kovar" type, of the alloy of the invention, as by casting, soldering, or welding.
- a strip of metal having a low thermal expansion e. g. an iron-nickel alloy of the Invar type, or an iron-nickel-cobalt alloy of the Kovar" type, of the alloy of the invention, as by casting, soldering, or welding.
- compositions described herein are examples illustrative of the invention, and that the invention is not limited to or by such examples.
- Method of making a wrought article of a manganese-ba e valloy containing upwards of 40% manganese which comprises forming a melt from substantially pure manganese and a-minor percentage at least 1% of copper which acts to stabilize the gamma phase of manganese, such melt being substantially free from embrittling elements; casting and solidifying the alloy melt; and, before the casting has cooled below the transformation temperature at about 740 0., hot deforming the casting to break down the grain.
- Method of making a wrought article of a manganese-base alloy which comprises forming a melt from substantially pure manganese and an effective percentage above 0.5% of an element having the property of stabilizing the gamma phase of manganese and selected from the group consisting of copper, nickel, and iron, such melt being substantially free from embrittling elements and containing upwards of 40% manganese; casting and solidifying the alloy melt; before the casting has cooled below the transformation temperature at about 740 C., hot rolling the casting; and thereafter quenching the casting.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Conductive Materials (AREA)
Description
Patented June 24, 1941 MAN GANESE-BASE ALLOY AND METHOD OF MAKING AND USING THE SAME William Kroll, Luxemburg, Luxcmburg -No Drawing. Original application January 17,
1940, Serial No. 314,229.
ary 4, 1939.
In Luxemburg, J anu- Divided and this application Jannary 31, 1940, Serial No. 316,543
3 Claims.
The invention relates to alloys containing a large proportion of manganese, and has for one of its principal objects the provision of manganese alloys which may be cold-worked. Another object is to provide a method of making and treating such alloys to improve their amenability to cold-working.
It is known that electrolytically refined gamma manganese remains in that state for several weeks, and that during such time it may be coldworked. But in time the gamma manganese alters to the brittle alpha form, and it has heretofore been impossible to obtain by thermal treatment forms of manganese or high-manganese alloys that are stably ductile at room temperatures.
I have observed that pure manganese obtained by distillation may be hot rolled at temperatures above the alpha-betatransformation point, the best results being obtained in the neighborhood of the gamma transformation point; but when quenched it-pass'es over immediately to the brittle alpha state.
The present invention is based on the discovery that the above-described conversion of ductile manganese to the brittle form may be to a great extent prevented by means of certain alloying additions which act to inhibit such conversion, and that when suitable thermal treat ment is employed, the resulting alloys may be kept in a ductile condition at room temperature.
The alloying addition producing the most favorable results is copper in a proportion of about 1% to 60%, preferably between 10% and 35%, of the alloy.
In order to obtain the maximum freedom from brittleness, it is important when making the alloys to protect the molten metal from the nitrogen and oxygen of the air. This may be done by the use of protective fluxes, e. g. slags containing manganese chloride, manganese oxide .structure is still present, cooling to room temperatureand reheating to rolling temperature will cause cracks and red-shortness.
According to the invention, the cast ingots, still hot, are hot rolledin the gamma-beta regions until the grain has been broken down. The l5 thinner cross sections may then be rapidly cooled,
thereby avoiding embrittlement. Thus, for example, ingots .50 mm. of a manganese alloy containing 15% or more copper are rolled at 950 G. into sheets 2 mm. thick which may then be air cooled.
Cold working may be done within wide limits. intermediate anneals being effected by rapid heating to within the beta or gamma field, followed by quenching.
Although the manganese-copper alloys are relatively stable, they nevertheless tend to become brittle when heated to certain moderately.
nese alloy becomes brittle in the same time at 500 C. The iron, 65% manganese alloy can stand up to 450 C. The transformation and alkaline earth metal halides; or by the use of a protective atmosphere, for instance hydrogen, methane, and the rare permanent gases such as argon or helium; or by the use of a partial vacuum, if it be not carried to such a point as to vaporize manganese too rapidly; or by a combination of two or three of these measures. Clay crucibles may be used in preparing the alloy.
The hot rolling of the alloys of the invention must be conducted entirely aboife the beta-alpha transformation temperature, and preferably is commenced while the alloy is in the gamma form. Otherwise, the metal tends to be redshort or cold-short. The beta-alpha point is causing embrittlement requires a certain time at the critical temperature, therefore no brittleness appears when the alloy passes rapidly through the critical temperature range, and it is possible so to control the embrittlement as to exploit it for the purpose of increasing the hardness and strength of the alloy. Thus, a binary manganese-copper alloy containing 15% copper was rolled at 900 C. and quenched. The tensile strength of the rolled and quenched sheets, 0.75 mm. thick, was 40.3 kg./mm. with an elongation of'34.5% and a Brinell hardness of 111. By re- .heating the sheets at 500 C, for five minutes the suitable proportions of nickel and copper, preferably within the range of 0.5% to 10% nickel and 5% to 40% copper, the tendency to become embrittled at moderately elevated temperatures within the alpha field is suppressed and may be substantially eliminated. For example, an alloy containing 6.9% Ni, 5.1% Cu, rest Mn, is substantially entirely stable, and after working and quenching from 950 C. has a tensile strength of 39.9 ken/mm. with 20% elongation and a Brinell hardness of 105. In general, the alloys containing the higher percentages of copper tolerate the higher nickel additions.
Aluminum may be added to the alloys in an amount suitably between 0.1% and (the higher percentages preferably being used with the higher copper percentages) to deoxidize them, thereby improving their workability. Furthermore, aluminum protects the alloy against oxidation at high temperatures, and during melting and casting it forms a superficial film of oxide which hinders oxidation and nitrogen pick-up. It promotes the existence of a surface favorable for rolling. The aluminum-5 containing alloys may advantageously be made from manganese produced by alumino-thermic reduction.
Zinc may also be added in a proportion up to 20%, the copper preferably being correspondingly reduced. A more narrowly circumscribed limit for such alloys is between 5% and 35% copper and 1% to 8% zinc. For instance, an alloy containing 10% Cu, 5% Zn, rest Mn, after rolling and quenching from 1050 C. and subsequent cold working, had a tensile strength of 47.7 kg./mm. with 13.1% elongation and a Brinell hardness of 131.
Other metals may be present, as one or more of iron, cobalt, tungsten, or chromium, in 'a total percentage up to 5% but preferably not over about 2%. In general, the elements Si, Sn, Ti, Ta, Mo, Ag, Ce, Mg, and Be appear to be injurious and should ordinarily not exceed 0.5% Si, 1% Sn, 2% Ti, 5% Ta, 2% Mo, 2% Ag, 2% Ce, Mg, or 0.5% Be. Calcium, lithium, or thorium may be used in a proportion of 1% or more as a deoxidizer. The alloys containing the higher percentages of copper or of copperand nickel will tolerate the higher amounts of such other metals. It is preferred that the silicon content be less than 0.15%.
Iron in a proportion between 30% and 50% (up to 5% of. which may be replaced by one or more of the elements nickel, cobalt, tungsten, molybdenum, titanium, and chromium) may be used as the stabilizing metal instead of the copper; but the stabilizing effects oi iron are not, in general, as strong as those produced by copper. The beta-alpha point is about 600 to 742 C. in the case of the iron-manganese alloys.
The alloys of the invention preferably contain less than 0.2% carbon and should usually contain less than 0.05% of this element, although somewhat higher carbon contents will on occasion be permissible. It is also preferred that the manganese content be at least 50%, although on occasion it may be as low as 40%.
The resistance of the alloys of the invention to corrosion =by moist air is about the same as thatof pure copper. Scaling accompanied by peeling is noticeable only above 600 C. in the case of the lower copper alloys and only above 700' C. in the case of the higher copper alloys. 1
The alloys containing over 30% copper may easily be soldered with'. either soft or hard solder.
Those with less than 30% copper are soldered with some difllculty.
The alloys of the invention have a particularly high electrical resistivity, generally between about 1.2 and 2 ohm/m./mm. For instance, the binary manganese-copper alloy containing 40% copper has a resistivity slightly more than 2 ohm/m./mm.* The binary alloys age-harden, with a decrease in electrical resistivity. The stable manganese-copper nickel alloys, are particularly useful as resistance alloys. For example. an alloy containing about 37% copper, 8% nickel, rest manganese, has an electrical resistivity of about 1.8 ohmlmlmmfi, three times that of commercial resistance-wires of copperbase alloys. while an alloy containing 5% copper,
8% nickel, rest manganese, has a resistivity of 1.35 ohm/m./mm.
The highest resistivities are obtained in the range of 30% to copper, and the addition of 6% to 8% nickel is suiiicient to stabilize the alloy. If the alloy is to be used at temperatures below 100 C., the nickel content may be as low as 0.5% or be eliminated entirely. If de sired, the nickel content may be raised as high as 20%. Nickel only slightly aifects the resistivity, the latter being determined chiefly by the solid solution of manganese and copper.
Within the range of 25% to 55% copper, 0% to 15% nickel, rest manganese, the temperature coefficient of electrical resistivity is low, e. g. alpha=0.0003 for an alloy containing 50% manganese and 50% copper. The higher-manganese alloys have a relatively high temperature coefficient, for instance, -alpha=0.03 for an alloy containing manganese and 5% copper. Nickel does not have any. pronounced effect on the temperature coeflicient of electrical resistivity.
The alloys of the invention also have an unusually high coeflicient of expansion, and are accordingly useful as thermoregulatorelements. If such elements are to be used at elevated temperatures, the stable ternary. manganese-copper,- nickel alloys containing about 4% to 20%, preferably 5% to 12%, nickel are most suitable.
An alloy containing 5% copper and 8% nickel, rest manganese, has an average coeflicient of expansion of alpha=390 10", an electrical resistance of about 1.3 ohm/mJmmF, a Brinellhardness of about 150, and a melting point at about, 1100" C. The temperature-expansion curve is almost straight, is without breaks, and is reproducible as often as desired.
An alloy containing 37% copper and 8% nickel, rest manganese has a coefllcient of expansion of alpha-=290X 10- and an electrical resistance of more than 1.8 ohm/mJmn'i.
Bimetallic elements may be formed by fastening a strip of metal having a low thermal expansion, e. g. an iron-nickel alloy of the Invar type, or an iron-nickel-cobalt alloy of the Kovar" type, of the alloy of the invention, as by casting, soldering, or welding.
It is to be understood that the several specific compositions described herein are examples illustrative of the invention, and that the invention is not limited to or by such examples.
This application is a division of my application Serial Number 314,229, filed January 17, 1940.
I claim:
1. Method of making a wrought article of a manganese-ba e valloy containing upwards of 40% manganese, which comprises forming a melt from substantially pure manganese and a-minor percentage at least 1% of copper which acts to stabilize the gamma phase of manganese, such melt being substantially free from embrittling elements; casting and solidifying the alloy melt; and, before the casting has cooled below the transformation temperature at about 740 0., hot deforming the casting to break down the grain.
2. Method as claimed in claim 1, wherein the hot deformed alloy is thereafter cold rolled in a plurality of stages and annealed between such stages, said annealing being effected by heating the alloy to, and quenching it from, a temperature above the alpha-beta point (about 740 C.).
3. Method of making a wrought article of a manganese-base alloy which comprises forming a melt from substantially pure manganese and an effective percentage above 0.5% of an element having the property of stabilizing the gamma phase of manganese and selected from the group consisting of copper, nickel, and iron, such melt being substantially free from embrittling elements and containing upwards of 40% manganese; casting and solidifying the alloy melt; before the casting has cooled below the transformation temperature at about 740 C., hot rolling the casting; and thereafter quenching the casting.
' WILLIAM KROLL.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US316543A US2246886A (en) | 1940-01-17 | 1940-01-31 | Manganese-base alloy and method of making and using the same |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US31422940A | 1940-01-17 | 1940-01-17 | |
| US316543A US2246886A (en) | 1940-01-17 | 1940-01-31 | Manganese-base alloy and method of making and using the same |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2246886A true US2246886A (en) | 1941-06-24 |
Family
ID=26979269
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US316543A Expired - Lifetime US2246886A (en) | 1940-01-17 | 1940-01-31 | Manganese-base alloy and method of making and using the same |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2246886A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3349472A (en) * | 1962-02-27 | 1967-10-31 | Schlegel Werner | Process for pressure-forming metallic bodies |
-
1940
- 1940-01-31 US US316543A patent/US2246886A/en not_active Expired - Lifetime
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3349472A (en) * | 1962-02-27 | 1967-10-31 | Schlegel Werner | Process for pressure-forming metallic bodies |
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