US2123840A - Alloys - Google Patents
Alloys Download PDFInfo
- Publication number
- US2123840A US2123840A US148561A US14856137A US2123840A US 2123840 A US2123840 A US 2123840A US 148561 A US148561 A US 148561A US 14856137 A US14856137 A US 14856137A US 2123840 A US2123840 A US 2123840A
- Authority
- US
- United States
- Prior art keywords
- alloy
- nickel
- iron
- copper
- amounts
- 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
- 229910045601 alloy Inorganic materials 0.000 title description 40
- 239000000956 alloy Substances 0.000 title description 40
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 26
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 26
- 229910052742 iron Inorganic materials 0.000 description 13
- 229910052759 nickel Inorganic materials 0.000 description 13
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 12
- 229910052802 copper Inorganic materials 0.000 description 12
- 239000010949 copper Substances 0.000 description 12
- 229910052785 arsenic Inorganic materials 0.000 description 10
- RQNWIZPPADIBDY-UHFFFAOYSA-N arsenic atom Chemical compound [As] RQNWIZPPADIBDY-UHFFFAOYSA-N 0.000 description 10
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 9
- 239000011701 zinc Substances 0.000 description 9
- 229910052725 zinc Inorganic materials 0.000 description 9
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 4
- 239000005864 Sulphur Substances 0.000 description 4
- 239000000155 melt Substances 0.000 description 4
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 3
- 238000005260 corrosion Methods 0.000 description 3
- 230000007797 corrosion Effects 0.000 description 3
- 230000002939 deleterious effect Effects 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 238000010438 heat treatment Methods 0.000 description 3
- 229910052748 manganese Inorganic materials 0.000 description 3
- 239000011572 manganese Substances 0.000 description 3
- 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 3
- 238000005482 strain hardening Methods 0.000 description 3
- 230000003245 working effect Effects 0.000 description 3
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 2
- 238000005299 abrasion Methods 0.000 description 2
- 239000000470 constituent Substances 0.000 description 2
- 238000005242 forging Methods 0.000 description 2
- 238000005098 hot rolling Methods 0.000 description 2
- 238000003754 machining Methods 0.000 description 2
- 229910052710 silicon Inorganic materials 0.000 description 2
- 239000010703 silicon Substances 0.000 description 2
- WWNBZGLDODTKEM-UHFFFAOYSA-N sulfanylidenenickel Chemical compound [Ni]=S WWNBZGLDODTKEM-UHFFFAOYSA-N 0.000 description 2
- 229910001369 Brass Inorganic materials 0.000 description 1
- 229910000990 Ni alloy Inorganic materials 0.000 description 1
- 229910001297 Zn alloy Inorganic materials 0.000 description 1
- HQTXVRHCLNJHCW-UHFFFAOYSA-N [As].[Zn].[Ni].[Fe].[Cu] Chemical compound [As].[Zn].[Ni].[Fe].[Cu] HQTXVRHCLNJHCW-UHFFFAOYSA-N 0.000 description 1
- 239000010951 brass Substances 0.000 description 1
- 238000005097 cold rolling Methods 0.000 description 1
- 238000013329 compounding Methods 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 239000002893 slag Substances 0.000 description 1
- 239000007779 soft material Substances 0.000 description 1
- CADICXFYUNYKGD-UHFFFAOYSA-N sulfanylidenemanganese Chemical compound [Mn]=S CADICXFYUNYKGD-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C9/00—Alloys based on copper
- C22C9/04—Alloys based on copper with zinc as the next major constituent
Definitions
- My invention relates to copper-base alloys. Applicant has found that by compounding copper, nickel, iron and arsenic in proper proportions there can be produced an alloy which has excellent resistance to abrasion, excellent strength, a high degree of toughness, good machining and wearing properties, and a reasonably good resistance to corrosion through a wide range of temperatures, and at the same time the alloy may be readily hot or cold worked and hot extruded by common mill processes, and possesses the property of being capable of being hardened by heat treatment. These properties make the alloy particularly useful for many industrial applications as, for example, piston rings, valve stems, and other applications where the material is subjected to severe stresses and wear at relatively high temperatures.
- Applicant has found, for example,,that by sub- 0 stituting 2% nickel, 1.75% iron, and 0.75% arsenic for equal amounts of zinc in Muntz metal there is ,7 produced an alloy that canbe very'easily hot worked by forging, extruding, and hot rolling to produce shapes which can be hardened and strengthened by light cold'working and be still further hardened by heat treatment.
- an extruded rod of the alloy having a hardness of B 65 Rockwell will have its hardness increased to B 79.5 upon reduction by cold rolling. If it is then annealed for about 30 minutes at 700 F. the hardness is further increased to B 87 Rockwell.
- the amount of iron ordinarily should not exceed 2% of the alloy because amounts in excess of this are not soluble within the range of zinc employed. Any iron in excess of about 2% of the alloy would be present as free iron, which would act to make articles fabricated of the alloy subject to fatigue failure and would form nuclei for the initiation of corrosion. Preferably, for these reasons, the iron should not exceed about 3% of the alloy. Ap preciable results will be secured in respect to the iron when in amount as low as about 0.1% of the alloy.
- Nickel will produce appreciable effects when present in amount as low as 0.1%.
- the maximum efiects of the nickel are obtained at about 2.5%, and therefore, for reasons of economy, this amount ordinarily should not be exceeded.
- amounts of nickel up to 4% are not particularly objectionable in respect to deleteriously affecting the valuable properties of the alloy.
- arsenic acts to toughen the alloy, and is particularly valuable in that it hardens it without detracting from its cold working properties. Still further, arsenic is of value in case the '5 alloy is exposed to high temperatures in that it will prevent dezinciflcation which otherwise would occur in an alloy of this composition in the absence of arsenic. Appreciable results are secured with as little as 0.05% arsenic, and it may be employed in amounts up to 1% of the alloy.
- the copper may range from about 54 to 69%, but preferably does not exceed 64% as with higher' amounts of copper the alloy becomes increasingly diificult to work.
- balance zinc is meant that the balance is zinc in the sense just defined.
- other elements is manganese, small amounts of which may be added to the melt to insure against the deleterious effects of any sulphur that may be present in the alloy.
- the sulphur if present, will unite with the manganese to form manganese-sulphide which in small amounts has little or no effect on the properties of the alloy, but in the absence. of manganese the sulphur would unite with the nickel to form nickel-sulphide which, even in small amounts, has a deleterious eiiect on the cold working properties of the alloy.
- the manganese which also will desulphurize any small amounts of nickel-sulphide commonly present in the nickel or nickel alloy added to the melt, preferably should not exceed 1% ofthe final alloy.
- the manganese added to the melt commonly, but not necessarily, will burn off or will go off in the slag, it maybe present in the final alloy from about 0.05 to 1%.
- Another of such elements is lead, which may be added in small amounts if the alloy is to be machined or if in use the alloy is to present a bearing surface, Lead from 0.1 to 2.5% will have appreciable effects in the respects mentioned without particularly modifying any of the properties of the basic alloy, except, for the reason that it constitutes a soft material entered into an other- 55 wise hard alloy and is dispersed instead of dissolved in that alloy, it acts to improve its machining, wearing, and bearing properties.
- silicon which may be present in amounts from 0.1 to 1%, silicon acting as a deoxidizer in the melt and also within this range acting materially to increase the tensile strength and markedly increase the corrosion resistant properties of the alloy.
- the preferred alloy contains 54 to 64% copper, 0.25 to 2.5% nickel, 0.25 to 2% iron,and 0.05 to 1% arsenic. To insure against the deleterious effects of sulphur, it also, not necessarily but preferably, contains 0.05 to 1% manganese, and, if it is to be employed in situations where it is desired to machine it, 0.2 to 2.5% lead. Alloys containing the lesser amounts of copper and the gerater amounts of the other constituents within the ranges of elements specified have the best hot working properties and require only a minimum of cold working to develop maximums of strength,
- alloys having the greater amounts of copper and the lesser amounts of the other constituents are not so easily hot worked. Nevertheless the alloys having the greater amounts of copper have sufiicient plasticity within a temperature range of 1200 F. to 1500 F. to enable them to be fabricated into shapes by hot rolling, or hot forging, or hot extruding, but not with the same ease as the alloys containing the lesser amounts of copper.
- An alloy having a high degree of toughness and capable of being hot and cold worked, hot extruded and hardened by heat treatment containing 54 to 69% copper, 0.1 to 4% nickel, 0.1 to 3% iron, 0.05 to 1% arsenic, balance zinc.
- Alloys according to claim 1 containing 0.25 to 2.5% nickel, and 0.25 to 2% iron.
- Alloys according to claim 1 containing, approximately, 57% copper, 2.5% nickel, 1.75% iron, 0.75% arsenic, balance zinc.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Forging (AREA)
Description
Patented July 12, 1938 UNITED STATES ALLOYS Edward S. Bunn, Rome, N. Y., assignor to Revere Copper and Brass Incorporated, Rome, N. Y., a corporation of Maryland No Drawing.
Application June 16, 1937,
Serial No, 148,561
3 Claims.
My invention relates to copper-base alloys. Applicant has found that by compounding copper, nickel, iron and arsenic in proper proportions there can be produced an alloy which has excellent resistance to abrasion, excellent strength, a high degree of toughness, good machining and wearing properties, and a reasonably good resistance to corrosion through a wide range of temperatures, and at the same time the alloy may be readily hot or cold worked and hot extruded by common mill processes, and possesses the property of being capable of being hardened by heat treatment. These properties make the alloy particularly useful for many industrial applications as, for example, piston rings, valve stems, and other applications where the material is subjected to severe stresses and wear at relatively high temperatures.
Applicant has found, for example,,that by sub- 0 stituting 2% nickel, 1.75% iron, and 0.75% arsenic for equal amounts of zinc in Muntz metal there is ,7 produced an alloy that canbe very'easily hot worked by forging, extruding, and hot rolling to produce shapes which can be hardened and strengthened by light cold'working and be still further hardened by heat treatment. For example, it has been found that an extruded rod of the alloy having a hardness of B 65 Rockwell will have its hardness increased to B 79.5 upon reduction by cold rolling. If it is then annealed for about 30 minutes at 700 F. the hardness is further increased to B 87 Rockwell.
The combination of nickel and iron it has been found imparts hardness, toughness, and resist- 35 ance to abrasion and wear. The amount of iron ordinarily should not exceed 2% of the alloy because amounts in excess of this are not soluble within the range of zinc employed. Any iron in excess of about 2% of the alloy would be present as free iron, which would act to make articles fabricated of the alloy subject to fatigue failure and would form nuclei for the initiation of corrosion. Preferably, for these reasons, the iron should not exceed about 3% of the alloy. Ap preciable results will be secured in respect to the iron when in amount as low as about 0.1% of the alloy.
Nickel will produce appreciable effects when present in amount as low as 0.1%. The maximum efiects of the nickel are obtained at about 2.5%, and therefore, for reasons of economy, this amount ordinarily should not be exceeded. However, amounts of nickel up to 4% are not particularly objectionable in respect to deleteriously affecting the valuable properties of the alloy.
The arsenic, it has been found, in combination with the other elements acts to toughen the alloy, and is particularly valuable in that it hardens it without detracting from its cold working properties. Still further, arsenic is of value in case the '5 alloy is exposed to high temperatures in that it will prevent dezinciflcation which otherwise would occur in an alloy of this composition in the absence of arsenic. Appreciable results are secured with as little as 0.05% arsenic, and it may be employed in amounts up to 1% of the alloy.
The copper may range from about 54 to 69%, but preferably does not exceed 64% as with higher' amounts of copper the alloy becomes increasingly diificult to work.
The balance of the alloy, in respect to copper, nickel, iron and arsenic and neglecting impurities, is zinc in the sense that such balance is all zinc or all zinc except for small amounts of other elements added for imparting special properties to the alloy without eliminating the characteristic properties of the basic copper-nickel-iron-arsenic-zinc alloy or for insuring the existence of or for modifying such characteristic properties. It will therefore be understood that in the appended claims by the words balance zinc is meant that the balance is zinc in the sense just defined. Among such other elements is manganese, small amounts of which may be added to the melt to insure against the deleterious effects of any sulphur that may be present in the alloy. The sulphur, if present, will unite with the manganese to form manganese-sulphide which in small amounts has little or no effect on the properties of the alloy, but in the absence. of manganese the sulphur would unite with the nickel to form nickel-sulphide which, even in small amounts, has a deleterious eiiect on the cold working properties of the alloy. The manganese, which also will desulphurize any small amounts of nickel-sulphide commonly present in the nickel or nickel alloy added to the melt, preferably should not exceed 1% ofthe final alloy. As a large proportion of the manganese added to the melt commonly, but not necessarily, will burn off or will go off in the slag, it maybe present in the final alloy from about 0.05 to 1%. Another of such elements is lead, which may be added in small amounts if the alloy is to be machined or if in use the alloy is to present a bearing surface, Lead from 0.1 to 2.5% will have appreciable effects in the respects mentioned without particularly modifying any of the properties of the basic alloy, except, for the reason that it constitutes a soft material entered into an other- 55 wise hard alloy and is dispersed instead of dissolved in that alloy, it acts to improve its machining, wearing, and bearing properties. Still another of such elements which may be added is silicon, which may be present in amounts from 0.1 to 1%, silicon acting as a deoxidizer in the melt and also within this range acting materially to increase the tensile strength and markedly increase the corrosion resistant properties of the alloy.
It will be understood from the foregoing that the preferred alloy contains 54 to 64% copper, 0.25 to 2.5% nickel, 0.25 to 2% iron,and 0.05 to 1% arsenic. To insure against the deleterious effects of sulphur, it also, not necessarily but preferably, contains 0.05 to 1% manganese, and, if it is to be employed in situations where it is desired to machine it, 0.2 to 2.5% lead. Alloys containing the lesser amounts of copper and the gerater amounts of the other constituents within the ranges of elements specified have the best hot working properties and require only a minimum of cold working to develop maximums of strength,
whereas alloys having the greater amounts of copper and the lesser amounts of the other constituents are not so easily hot worked. Nevertheless the alloys having the greater amounts of copper have sufiicient plasticity within a temperature range of 1200 F. to 1500 F. to enable them to be fabricated into shapes by hot rolling, or hot forging, or hot extruding, but not with the same ease as the alloys containing the lesser amounts of copper.
I claim:
1. An alloy having a high degree of toughness and capable of being hot and cold worked, hot extruded and hardened by heat treatment containing 54 to 69% copper, 0.1 to 4% nickel, 0.1 to 3% iron, 0.05 to 1% arsenic, balance zinc.
2. Alloys according to claim 1 containing 0.25 to 2.5% nickel, and 0.25 to 2% iron.
3. Alloys according to claim 1 containing, approximately, 57% copper, 2.5% nickel, 1.75% iron, 0.75% arsenic, balance zinc.
EDWARD S. BUNN.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US148561A US2123840A (en) | 1937-06-16 | 1937-06-16 | Alloys |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US148561A US2123840A (en) | 1937-06-16 | 1937-06-16 | Alloys |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2123840A true US2123840A (en) | 1938-07-12 |
Family
ID=22526295
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US148561A Expired - Lifetime US2123840A (en) | 1937-06-16 | 1937-06-16 | Alloys |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2123840A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3404977A (en) * | 1965-12-09 | 1968-10-08 | American Standard Inc | Brass alloy |
| US4101317A (en) * | 1972-10-03 | 1978-07-18 | Toyo Valve Co., Ltd. | Copper alloys with improved corrosion resistance and machinability |
| US4362579A (en) * | 1979-12-25 | 1982-12-07 | Nihon Kogyo Kabushiki Kaisha | High-strength-conductivity copper alloy |
| EP0193004A1 (en) * | 1985-02-14 | 1986-09-03 | Olin Corporation | Corrosion resistant modified cu-zn alloy for heat exchanger tubes |
| CN102899525A (en) * | 2011-07-26 | 2013-01-30 | 宁波金田铜业(集团)股份有限公司 | High strength and toughness wear-resisting complex brass and production method thereof |
-
1937
- 1937-06-16 US US148561A patent/US2123840A/en not_active Expired - Lifetime
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3404977A (en) * | 1965-12-09 | 1968-10-08 | American Standard Inc | Brass alloy |
| US4101317A (en) * | 1972-10-03 | 1978-07-18 | Toyo Valve Co., Ltd. | Copper alloys with improved corrosion resistance and machinability |
| US4362579A (en) * | 1979-12-25 | 1982-12-07 | Nihon Kogyo Kabushiki Kaisha | High-strength-conductivity copper alloy |
| EP0193004A1 (en) * | 1985-02-14 | 1986-09-03 | Olin Corporation | Corrosion resistant modified cu-zn alloy for heat exchanger tubes |
| US4674566A (en) * | 1985-02-14 | 1987-06-23 | Olin Corporation | Corrosion resistant modified Cu-Zn alloy for heat exchanger tubes |
| CN102899525A (en) * | 2011-07-26 | 2013-01-30 | 宁波金田铜业(集团)股份有限公司 | High strength and toughness wear-resisting complex brass and production method thereof |
| CN102899525B (en) * | 2011-07-26 | 2014-12-10 | 宁波金田铜业(集团)股份有限公司 | High strength and toughness wear-resisting complex brass and production method thereof |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US3912503A (en) | Galling resistant austenitic stainless steel | |
| US3615365A (en) | Austenitic stainless steel | |
| US2123840A (en) | Alloys | |
| US3031299A (en) | Aluminum base alloy | |
| US3703367A (en) | Copper-zinc alloys | |
| US2074604A (en) | Alloy | |
| US2357450A (en) | Aluminum alloy | |
| US2229622A (en) | Piston and rod-packing ring | |
| US2137283A (en) | Copper alloys | |
| US3337335A (en) | Leaded silicon manganese bearing brass | |
| US2081394A (en) | Weld rod | |
| US2101626A (en) | Hot workable copper alloys | |
| US2195435A (en) | Copper alloy | |
| US2708159A (en) | Heat treated, hardened alloy steel elements | |
| US2026541A (en) | Free cutting alloys | |
| US2101625A (en) | High strength corrosion resistant copper alloy | |
| US2253385A (en) | Steel | |
| US1986825A (en) | Free cutting alloy | |
| US1485158A (en) | Gear | |
| US2107223A (en) | Bearing metal alloy | |
| US2309102A (en) | Copper base alloy | |
| US1572458A (en) | Alloy steel | |
| US2153977A (en) | Condenser tube | |
| US2338756A (en) | Copper-base alloy | |
| US3224875A (en) | Non-magnetic copper base alloys |