US2309100A - Copper base alloy - Google Patents
Copper base alloy Download PDFInfo
- Publication number
- US2309100A US2309100A US407216A US40721641A US2309100A US 2309100 A US2309100 A US 2309100A US 407216 A US407216 A US 407216A US 40721641 A US40721641 A US 40721641A US 2309100 A US2309100 A US 2309100A
- Authority
- US
- United States
- Prior art keywords
- alloy
- copper
- zinc
- base alloy
- 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
- 229910045601 alloy Inorganic materials 0.000 title description 28
- 239000000956 alloy Substances 0.000 title description 28
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 title description 14
- 229910052802 copper Inorganic materials 0.000 title description 14
- 239000010949 copper Substances 0.000 title description 14
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 20
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 13
- 239000011701 zinc Substances 0.000 description 13
- 229910052725 zinc Inorganic materials 0.000 description 13
- 229910000906 Bronze Inorganic materials 0.000 description 10
- 239000010974 bronze Substances 0.000 description 10
- 229910052759 nickel Inorganic materials 0.000 description 10
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 8
- 229910052698 phosphorus Inorganic materials 0.000 description 8
- 239000011574 phosphorus Substances 0.000 description 8
- 229910052714 tellurium Inorganic materials 0.000 description 8
- PORWMNRCUJJQNO-UHFFFAOYSA-N tellurium atom Chemical compound [Te] PORWMNRCUJJQNO-UHFFFAOYSA-N 0.000 description 8
- 238000011282 treatment Methods 0.000 description 8
- BUGBHKTXTAQXES-UHFFFAOYSA-N Selenium Chemical compound [Se] BUGBHKTXTAQXES-UHFFFAOYSA-N 0.000 description 7
- 229910052711 selenium Inorganic materials 0.000 description 7
- 239000011669 selenium Substances 0.000 description 7
- 239000000463 material Substances 0.000 description 6
- 230000032683 aging Effects 0.000 description 5
- 238000001816 cooling Methods 0.000 description 4
- KUNSUQLRTQLHQQ-UHFFFAOYSA-N copper tin Chemical compound [Cu].[Sn] KUNSUQLRTQLHQQ-UHFFFAOYSA-N 0.000 description 4
- 238000001125 extrusion Methods 0.000 description 4
- 238000010438 heat treatment Methods 0.000 description 3
- 238000003483 aging Methods 0.000 description 2
- 238000000137 annealing Methods 0.000 description 2
- 238000003754 machining Methods 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 238000010791 quenching Methods 0.000 description 2
- 230000000171 quenching effect Effects 0.000 description 2
- BPQQTUXANYXVAA-UHFFFAOYSA-N Orthosilicate Chemical compound [O-][Si]([O-])([O-])[O-] BPQQTUXANYXVAA-UHFFFAOYSA-N 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052797 bismuth Inorganic materials 0.000 description 1
- JCXGWMGPZLAOME-UHFFFAOYSA-N bismuth atom Chemical compound [Bi] JCXGWMGPZLAOME-UHFFFAOYSA-N 0.000 description 1
- 238000010622 cold drawing Methods 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000002706 hydrostatic effect Effects 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000001556 precipitation Methods 0.000 description 1
- 125000003748 selenium group Chemical group *[Se]* 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 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
- This invention relates to improvements in copper-base alloys.
- One object of this invention is to provide an improved copper-base alloy free from fissuring and having high strength and hardness, easy machining qualities, good corrosion-resistance, and a certain well-known red-bronze color desired for hardware use.
- This improved alloy contains by weight, copper from 85% to 90%, nickel from /2% to 1 4%, phosphorus from 0.06% to 0.3% and from A; to A of the weight of the nickel content but preferably about of the nickel, from 0.2% to 2 of metal from the group consisting of lead, tellurium and selenium to render the alloy freely machinable, and the balance substantially of zinc, the zinc being from 7% to 14%, and the total of the copper and zinc being at least 95%. Where lead is used, it would be from to 2 /2 Where tellurium and/or selenium is used, it would total from 0.2% to A more preferred alloy is to have the foregoing alloy modified by having the nickel from 0.6% to 1%, and the phosphorus from 0.08% to 0.2%.
- a still more preferred alloy is .to have the copper from 85% to 90%, the nickel about phosphorus about 0.15%, from 0.3% to 2%% of material from the group consisting of lead, tellurium and selenium to render the alloy freely machinable, and the balance substantially all zinc, the zinc being from 7%% to 14%, and the total of the copper and zinc being at least 96%.
- lead it would be from to 2
- tellurium and/or selenium it would total from 0.3% to If any bismuth is to be present in the alloy, it should not exceed 0.1% as it very seriously embrittles the alloy. If any aluminum is to be present in the alloy, it should not exceed 0.2% as it prevents obtaining the desired red-bronze color.
- any silicon is to be present in the alloy, it should not exceed 0.1%, as with lead it forms a lead silicate which is very abrasive on cutting tools, and with tellurium or selenium forms a refractory scale and renders control of the alloy composition dimcult.
- a lot of alloy made in accordance with the present invention was melted in an induction furnace and cast in the form of round billets 7% inches in diameter.
- the actual composition of this alloy was copper 87.65%, nickel 0.49%, phosphorus 0.08%, lead 1.98%, zinc 9.8%.
- the billets were cut to about 30-inch lengths and extruded at about 1600 F. in a hydraulic extrusion press to 2-inch round rods. No difficulty was encountered, the hydrostatic pressure required being only about 3,000 lbs. per square inch, whereas the well known hardware bronze requires about 4,000 to 4,500 lbs. per square inch.
- the rods were scalped according to usual procedure and some were drawn to various diameters from about one to two inches, and others were cold-rolled in grooved rolls and then drawn to smaller sizes.
- rods of our improved alloy were substantially immune to flssuring when subjected to commercial heating, as compared to rods of the well known hardware bronze. No fissures were encountered even when drawn rods were pulled directly into a very hot furnace, whereas fissures always occur in rods of the well known hardware bronze under such circumstances.
- the fissures usually extend throughout the length of a rod and to a depth near to or beyond the center of hardening nickel and phosphorus, and quenching, or cooling sufliciently rapidly, from such temperature to hold age-hardening material in solution, and can be subsequently age-hardened by re-heatlng or aging at temperature in the range from about 700 F. to about 1000 F. for from about one-half to six hours or longer, depending on the temperature, to precipitate age-hardening material out of solution. Further, it was found that our alloys could be cold-drawn either before or after the aging and give improved tensile and yield strength either way.
- the preferred treatment consists in annealing at about 1200" F. to about 1350 F. and air-cooling, and later aging for about two hours at about 800 F., and colddrawing to produce a reduction of area of 20% or more, depending on the size and shape of the rod and the exact properties desired.
- a rod finished on 1% inches diameter and so treated showed the following properties:
- a copper-base alloy consisting substantially of: copper from to nickel from 0.06% to 1%; phosphorus from 0.08% to 0.2%; from 0.2% to 2 of material from the group consisting of lead, tellurium and selenium; and the balance substantially of zinc and at least 7% ,'and the total of the copper and zinc being at least the alloy being characterized by a redbronze color, and by being relatively free from fissuring.
- a copper-base alloy consisting substantially of copper from 85% to 90%; nickel about phosphorus about 0.15%; from 0.3% to 2 of material from the group consisting of lead, tellurium and selenium; and the balance substantially of zinc and at least l /2%, the total of the copper and zinc being at least 96%; the alloy being characterized by a red-bronze color, and by being relatively free from fissuring.
- a copper-base alloy consisting substantially of copper from 85% to 90%; nickel from to l%%; phosphorus from 0.06% to 0.3%; from 0.2% to 2 /2% of material from the group consisting of lead, tellurium and selenium; and the balance substantially of zinc and at least 7%, and the total of the copper and zinc being at least 95%; the alloy being characterized by a redbronze color, and by being relatively free from flssuring, and said alloy having been given a solution treatment by having been suitably cooled from temperature in the range from about 1200 F. to about 1600 F. and having been hardened by having been given a precipitation treatment at temperature in the range from about 700 F. to
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Adornments (AREA)
Description
Patented Jan. 2t, 1943 COPPER BASE ALLOY- Donald K. Crampton, Marion, and Henry L. Burghofl', Waterbury, Conn, assignors to Chase Brass & Copper 00. Incorporated, Waterbury,
Conn., a. corporation No Drawing. Application August 16, 1941,
\ Serial No. 407,216
4 Claims. .(Cl. 148-32) This invention relates to improvements in copper-base alloys.
One object of this invention is to provide an improved copper-base alloy free from fissuring and having high strength and hardness, easy machining qualities, good corrosion-resistance, and a certain well-known red-bronze color desired for hardware use. e
Other objects of this invention will appear from the present disclosure.
It has long been desired to have an alloy free from fissuring and having high strength and hardness, easy machining qua1ities,.good corrosion-resistance, a certain well-known red-bronze color desired for hardware use, and a high tensile strength considerably higher than 50,000 lbs. per square inch, and preferably at least 60,000 lbs. per square inch. Previous efforts to produce such an alloy have not been satisfactory as the alloying metals added to give the required characteristics have caused excessive difliculty'in producing the rods, or an unwarranted increase in cost, or an intolerable change in the particular importantred-bronze color. We have invented, however, an alloy which we are about to set forth which possesses all of the desired properties even including substantial freedom from flssuring, the desired red-bronze color, with no sacrifice of workability and at less cost due to the subtantial freedom from losses due to fissuring, and in rods in sizes of from one-inch to two-inch diameter has a tensile strength of at least 60,000 lbs. per
square inch, and in sizes under one-inch diameter has a tensile strength of at least 65,000 lbs. per square inch.
This improved alloy contains by weight, copper from 85% to 90%, nickel from /2% to 1 4%, phosphorus from 0.06% to 0.3% and from A; to A of the weight of the nickel content but preferably about of the nickel, from 0.2% to 2 of metal from the group consisting of lead, tellurium and selenium to render the alloy freely machinable, and the balance substantially of zinc, the zinc being from 7% to 14%, and the total of the copper and zinc being at least 95%. Where lead is used, it would be from to 2 /2 Where tellurium and/or selenium is used, it would total from 0.2% to A more preferred alloy is to have the foregoing alloy modified by having the nickel from 0.6% to 1%, and the phosphorus from 0.08% to 0.2%.
A still more preferred alloy is .to have the copper from 85% to 90%, the nickel about phosphorus about 0.15%, from 0.3% to 2%% of material from the group consisting of lead, tellurium and selenium to render the alloy freely machinable, and the balance substantially all zinc, the zinc being from 7%% to 14%, and the total of the copper and zinc being at least 96%. Where lead is used, it would be from to 2 Where tellurium and/or selenium is used, it would total from 0.3% to If any bismuth is to be present in the alloy, it should not exceed 0.1% as it very seriously embrittles the alloy. If any aluminum is to be present in the alloy, it should not exceed 0.2% as it prevents obtaining the desired red-bronze color. If any silicon is to be present in the alloy, it should not exceed 0.1%, as with lead it forms a lead silicate which is very abrasive on cutting tools, and with tellurium or selenium forms a refractory scale and renders control of the alloy composition dimcult.
A lot of alloy made in accordance with the present invention was melted in an induction furnace and cast in the form of round billets 7% inches in diameter. The actual composition of this alloy was copper 87.65%, nickel 0.49%, phosphorus 0.08%, lead 1.98%, zinc 9.8%. The billets were cut to about 30-inch lengths and extruded at about 1600 F. in a hydraulic extrusion press to 2-inch round rods. No difficulty was encountered, the hydrostatic pressure required being only about 3,000 lbs. per square inch, whereas the well known hardware bronze requires about 4,000 to 4,500 lbs. per square inch. The rods were scalped according to usual procedure and some were drawn to various diameters from about one to two inches, and others were cold-rolled in grooved rolls and then drawn to smaller sizes. No difficulties were encountered in drawing or annealing. Surprisingly, rods of our improved alloy were substantially immune to flssuring when subjected to commercial heating, as compared to rods of the well known hardware bronze. No fissures were encountered even when drawn rods were pulled directly into a very hot furnace, whereas fissures always occur in rods of the well known hardware bronze under such circumstances. Inasmuch as the fissures usually extend throughout the length of a rod and to a depth near to or beyond the center of hardening nickel and phosphorus, and quenching, or cooling sufliciently rapidly, from such temperature to hold age-hardening material in solution, and can be subsequently age-hardened by re-heatlng or aging at temperature in the range from about 700 F. to about 1000 F. for from about one-half to six hours or longer, depending on the temperature, to precipitate age-hardening material out of solution. Further, it was found that our alloys could be cold-drawn either before or after the aging and give improved tensile and yield strength either way.
It was found, also, that it was not necessary to apply the usual solution treatment by heating at a high temperature and quenching when producing large rods, since it was found that heating to above 1450 F. for extrusion, together with the normal rate of cooling during and after extrusion, apparently constitutes a sumciently adequate solution treatment, so that simple aging after extrusion gave substantially the same results as when the usual solution plus aging treatments were used. In fact, it was further found that during reduction from the two-inch extruded size to smaller finishing sizes, the intermediate anneals followed by ordinary air cooling, also constituted a sufficient solution treatment.
Of the several possible treatment procedures, all show decided improvements in tensile properties over those obtainable with the well known hardware bronze. The preferred treatment, however, consists in annealing at about 1200" F. to about 1350 F. and air-cooling, and later aging for about two hours at about 800 F., and colddrawing to produce a reduction of area of 20% or more, depending on the size and shape of the rod and the exact properties desired. A rod finished on 1% inches diameter and so treated showed the following properties:
Tensile strength p; s. i.-- 64,700 Yield strength do 62,000 Elongation in 2" per cent 25 Rockwell F" hardness 99 Rockwell B" hardness 74 The invention may be carried out in other specific ways than those herein set forth without departing from the spirit and essential characteristics of the invention, and the present embodiments are, therefore, to be considered in all respects as illustrative and not restrictive, and
from fissuring.
2. A copper-base alloy consisting substantially of: copper from to nickel from 0.06% to 1%; phosphorus from 0.08% to 0.2%; from 0.2% to 2 of material from the group consisting of lead, tellurium and selenium; and the balance substantially of zinc and at least 7% ,'and the total of the copper and zinc being at least the alloy being characterized by a redbronze color, and by being relatively free from fissuring.
3. A copper-base alloy consisting substantially of copper from 85% to 90%; nickel about phosphorus about 0.15%; from 0.3% to 2 of material from the group consisting of lead, tellurium and selenium; and the balance substantially of zinc and at least l /2%, the total of the copper and zinc being at least 96%; the alloy being characterized by a red-bronze color, and by being relatively free from fissuring.
4. A copper-base alloy consisting substantially of copper from 85% to 90%; nickel from to l%%; phosphorus from 0.06% to 0.3%; from 0.2% to 2 /2% of material from the group consisting of lead, tellurium and selenium; and the balance substantially of zinc and at least 7%, and the total of the copper and zinc being at least 95%; the alloy being characterized by a redbronze color, and by being relatively free from flssuring, and said alloy having been given a solution treatment by having been suitably cooled from temperature in the range from about 1200 F. to about 1600 F. and having been hardened by having been given a precipitation treatment at temperature in the range from about 700 F. to
about 1000 F.
DONALD K. CRAMP'ION. HENRY L. BURGHOFF.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US407216A US2309100A (en) | 1941-08-16 | 1941-08-16 | Copper base alloy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US407216A US2309100A (en) | 1941-08-16 | 1941-08-16 | Copper base alloy |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2309100A true US2309100A (en) | 1943-01-26 |
Family
ID=23611124
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US407216A Expired - Lifetime US2309100A (en) | 1941-08-16 | 1941-08-16 | Copper base alloy |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2309100A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4366117A (en) * | 1980-06-06 | 1982-12-28 | Nikon Kogyo Kabushiki Kaisha | Copper alloy for use as lead material for semiconductor devices |
| US20050239327A1 (en) * | 2002-06-10 | 2005-10-27 | Thomas Cantz | Device for electronically contacting an electrically conductive part of a high-frequency system |
-
1941
- 1941-08-16 US US407216A patent/US2309100A/en not_active Expired - Lifetime
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4366117A (en) * | 1980-06-06 | 1982-12-28 | Nikon Kogyo Kabushiki Kaisha | Copper alloy for use as lead material for semiconductor devices |
| US20050239327A1 (en) * | 2002-06-10 | 2005-10-27 | Thomas Cantz | Device for electronically contacting an electrically conductive part of a high-frequency system |
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