US3298828A - Treatment of leaded brass alloys for improving machineability and products so produced - Google Patents
Treatment of leaded brass alloys for improving machineability and products so produced Download PDFInfo
- Publication number
- US3298828A US3298828A US207802A US20780262A US3298828A US 3298828 A US3298828 A US 3298828A US 207802 A US207802 A US 207802A US 20780262 A US20780262 A US 20780262A US 3298828 A US3298828 A US 3298828A
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- Prior art keywords
- brass
- machineability
- lithium
- additive
- lead
- 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
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- 229910001340 Leaded brass Inorganic materials 0.000 title description 12
- 229910045601 alloy Inorganic materials 0.000 title description 6
- 239000000956 alloy Substances 0.000 title description 6
- 229910001369 Brass Inorganic materials 0.000 claims description 19
- 239000010951 brass Substances 0.000 claims description 19
- 239000000654 additive Substances 0.000 claims description 16
- 230000000996 additive effect Effects 0.000 claims description 16
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 claims description 14
- 229910052744 lithium Inorganic materials 0.000 claims description 14
- 238000003754 machining Methods 0.000 claims description 12
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 claims description 9
- 229910052791 calcium Inorganic materials 0.000 claims description 9
- 239000011575 calcium Substances 0.000 claims description 9
- 238000005520 cutting process Methods 0.000 claims description 9
- 239000011133 lead Substances 0.000 description 14
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 9
- 229910052725 zinc Inorganic materials 0.000 description 9
- 239000011701 zinc Substances 0.000 description 9
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 7
- 229910052802 copper Inorganic materials 0.000 description 7
- 239000010949 copper Substances 0.000 description 7
- 239000012535 impurity Substances 0.000 description 7
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 6
- 238000000034 method Methods 0.000 description 6
- 238000005266 casting Methods 0.000 description 5
- USOPFYZPGZGBEB-UHFFFAOYSA-N calcium lithium Chemical compound [Li].[Ca] USOPFYZPGZGBEB-UHFFFAOYSA-N 0.000 description 4
- 238000009826 distribution Methods 0.000 description 4
- 150000001875 compounds Chemical class 0.000 description 3
- 229910052742 iron Inorganic materials 0.000 description 3
- 239000002245 particle Substances 0.000 description 3
- 238000010008 shearing Methods 0.000 description 3
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- 241001275902 Parabramis pekinensis Species 0.000 description 2
- 238000005299 abrasion Methods 0.000 description 2
- 230000002411 adverse Effects 0.000 description 2
- 238000004140 cleaning Methods 0.000 description 2
- 238000005553 drilling Methods 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 239000002516 radical scavenger Substances 0.000 description 2
- QPLDLSVMHZLSFG-UHFFFAOYSA-N Copper oxide Chemical compound [Cu]=O QPLDLSVMHZLSFG-UHFFFAOYSA-N 0.000 description 1
- 239000005751 Copper oxide Substances 0.000 description 1
- 229910000997 High-speed steel Inorganic materials 0.000 description 1
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- NIPNSKYNPDTRPC-UHFFFAOYSA-N N-[2-oxo-2-(2,4,6,7-tetrahydrotriazolo[4,5-c]pyridin-5-yl)ethyl]-2-[[3-(trifluoromethoxy)phenyl]methylamino]pyrimidine-5-carboxamide Chemical compound O=C(CNC(=O)C=1C=NC(=NC=1)NCC1=CC(=CC=C1)OC(F)(F)F)N1CC2=C(CC1)NN=N2 NIPNSKYNPDTRPC-UHFFFAOYSA-N 0.000 description 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 1
- 229910001297 Zn alloy Inorganic materials 0.000 description 1
- 239000004411 aluminium Substances 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
- 238000000137 annealing Methods 0.000 description 1
- 229910052787 antimony Inorganic materials 0.000 description 1
- WATWJIUSRGPENY-UHFFFAOYSA-N antimony atom Chemical compound [Sb] WATWJIUSRGPENY-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 229910052793 cadmium Inorganic materials 0.000 description 1
- BDOSMKKIYDKNTQ-UHFFFAOYSA-N cadmium atom Chemical compound [Cd] BDOSMKKIYDKNTQ-UHFFFAOYSA-N 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 229910000431 copper oxide Inorganic materials 0.000 description 1
- TVZPLCNGKSPOJA-UHFFFAOYSA-N copper zinc Chemical compound [Cu].[Zn] TVZPLCNGKSPOJA-UHFFFAOYSA-N 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000001627 detrimental effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 239000011777 magnesium Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 238000003801 milling Methods 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 230000002028 premature Effects 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 229910052718 tin Inorganic materials 0.000 description 1
- 239000011135 tin 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 the treatment of copperbase alloys, and more particularly to the treatment of leaded brass, or free-cutting brass, to improve machineability.
- An important object of the invention therefore is to provide a leaded brass alloy having improved qualities for machining purposes.
- a further object is in the provision of a leaded brass which will reduce abrasion to toolfaces during machining operations therebyincreasing tool life and decreasing tool wear.
- leaded brass is a lead-copper-zinc alloy consisting essentially of 6090% copper, 0.25- 4.0% lead, and the balance of zinc.
- the commercially most important brass within this range comprises 60- 65% copper, 0.254.0% lead, and the remainder zinc.
- Operations contemplated Within the purview of this invention are those such as are performed in screw machines, drill presses, milling machines, turret lathes, embossers, and the like, and may include threading and knurling.
- the impurities may exist on the surface or be disbursed throughout more particularly on the lead particles. Since it is well known that the lead is added as a chip breaker, the impurities existing on the lead particles are detrimental to the machineability. Moreover the machineability of leaded brasses does not necessarily conform to the standard properties, such as tensile strength, percent elongation, etc. Thus machineability cannot be adequately determined in this manner.
- the present invention contemplates the use of very specific proportions of certain elements added to the leaded brass, for example, calcium, lithium and magnesium. Apparently lithium is most effective, 'with calcium next in effectiveness.
- the use of such metals has been known for the casting of copper oxide scavenger for improving the pouring and casting qualities. These additive metals usually substantially boil off in casting. Moreover, it has always been felt that the more added the better, with cost being the only consideration. Effectiveness of such additive elements as calcium-lithium, on cleaning lead when zinc is present, was unknown. Zinc itself has been acting as a scavenging agent for the casting and whether the additive elements react with the zinc and copper, and not the lead has been heretofore 3,298,828 Patented Jan. 17, 1967 ice undetermined. Furthermore, before machining, the leaded brass must undergo operations such as drawing to rod. The effect of such operations was not entirely clear, particularly since grain size and distribution is affected.
- the present invention contemplates the use of a substantial portion of scrap. This is probably, but not necessarily, due to the formation of complex chemical compounds not removed before casting, which complex compounds, although sub-microscopic in size, seriously affect tool wear by abrasion. Excessive use of the additive elemerits would adversely affect machineability, as would insufficient use. The exact reason for this is not readily determined, but the following examples provide some evidence. Distribution, quality, and size of the lead particles may be a factor, and excessive addition of these elements may cause too much cleaning in one area, thereby reducing uniformity and consequently machineability. Moreover, for fine machining an excess would seem to increase the tendency of undesirable firecracking. I
- Example 1 A lot of free cutting brass billets for use as rod were cast at 2100 using the following charges:
- Example 2 A lot of billets was cast at 2l00 using proportions similar to Example 1, but before pouring the melt, calcium and lithium in equal proportions were added using a standard phosphorizer, at a ratio of 8 ounces of calcium and lithium per 1000 lbs. of brass melt. The resulting analysis showed 62.04% copper, 3.12% lead, 0.20% iron and the other impurities, and the remainder zinc. Again alpha-beta structure was present in apparently normal proportion. Extruding, drawing and annealing was conducted in the manner of Example 1 with the result being all Alpha structure and apparently similar leaid distribution. Properties tested indicated 78,500 p.s.i. tensile strength, 61,200 p.s.i. yield strength, 10% elongation in 2" with consequent 45.2% reduction. Machining operations indicated a shearing off and a tendency to firecrack. The machine tools remained relatively sharp, since the shearing and firecracking were premature.
- Example 3 The procedure according to Example 2 was followed except that the calcium lithium added was 2 ounces per 1000 pounds of leaded brass. Analysis disclosed a similar proportion of elements, with alpha-beta structure Q3 present. Preparation of rod-was as in the previous examples, and resulted in all Alpha structure. Tested properties were 73,500 p.s.i. tensile strength, 58,100 p.s.i. yield strength, 10% elongation in 2 inches with 46.9% area reduction. Results in machining were erratic, with some samples showing improved machineability and longer tool life, while other samples gave results similar to Example 1.
- Example 4 The procedure according to Example 2 was again followed except that the calcium lithium ratio was 4 ounces per 1000 pounds melt. A similar proportion of elements again with alpha-beta structure present in normal percentages. After processing to rod as in the previous examples, apparently all Alpha structure was again the result. Properties were 70,600 p.s.i. tensile strength, 58,700 p.s.i. yield strength, 8.5% elongation in 2 inches with 41.1% area reduction. Machining was markedly improved, with tool life for the various samples being at least one third longer, with some samples as much as 200 percent longer. Neither shearing nor firecracking were evident, even with extremely thin walled machine parts.
- Example Samples of the rod prepared in Example 4 were relief annealed at 525 F. The mechanical properties were then 70,900 p.s.i. tensile strength, 61,300 p.s.i. yield strength, 11% elongation in 2 inches, with 44.4% area reduction. Results in machining were as good as EX- ample' 4, again with no firccracking in thinwalled parts.
- the test consisted of a horizontal /s" drill acting on the specimen, with the drill mounted on a track and driven by a constant weight, the depth of drill in millimeters being measured over a constant time.
- Example 1 (3 samples) A 4.5-5.0-50
- Example 2 (3 samples) 4.54.0-4.0
- Example 1 3 samples
- Example 4 (2 samples) 3.53.5
- Example 5 (2 samples) 3.0-3.0
- Example 1 (3 samples) 3.03.0-3.5
- Example 4 (3 samples) 3.S4.03.5
- Example 3 (3 samples) 4.53.02.5
- Example 4 exhibited regular superiority, while Example 3 was erratic, and suprisingly, Example 1 for drilling was superior to Example 2.
- a method of treating brass to improve the machineability thereof which comprises adding to molten brass an additive selected from the group consisting of lithium and admixtures of lithium and calcium in an amount of from two to eight ounces of additive per thousand pounds of molten brass.
- a method according to claim 2 wherein the additive is a mixture of equal parts by weight of lithium and calcium.
- Free-cutting brass having improved machining qualities containing an additive selected from the group of lithium and admixtures of lithium and calcium in an amount of from two to eight ounces of additive per thousand pounds of brass, said amount being determined by the addition of the said amount of additive to the brass when said brass is in a molten state.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Lubricants (AREA)
Description
United States Patent Lewis E. Thelin, Waterbury, Conn., assignor to The Bristol Brass Corporation, Bristol, Conn., a corporation of Connecticut No Drawing.
8 Claims.
Filed July 5, 1962, Ser. No. 207,802
This invention relates to the treatment of copperbase alloys, and more particularly to the treatment of leaded brass, or free-cutting brass, to improve machineability.
For many years, the leaded brass alloys in use have been considered as adequate for the machine tools in use. More recently, however, the development of machine tools with high peripheral and machine speeds have indicated deficiencies in the usefulness and adaptability of the available free-cutting brasses.
An important object of the invention therefore is to provide a leaded brass alloy having improved qualities for machining purposes.
A further object is in the provision of a leaded brass which will reduce abrasion to toolfaces during machining operations therebyincreasing tool life and decreasing tool wear.
Broadly speaking, leaded brass is a lead-copper-zinc alloy consisting essentially of 6090% copper, 0.25- 4.0% lead, and the balance of zinc. The commercially most important brass within this range comprises 60- 65% copper, 0.254.0% lead, and the remainder zinc. Operations contemplated Within the purview of this invention are those such as are performed in screw machines, drill presses, milling machines, turret lathes, embossers, and the like, and may include threading and knurling.
Of necessity, commercial brasses are made with a high proportion of scrap and remelt. Therefore, it is usually quite difficult to control the specific proportions of impurities within the alloy while still remaining within the A.S.T.M. standards of about .25% permissible impurities. Such elements as iron, tin, aluminium, nickel, cadmium, antimony, and silicon may be present in uncontrollable quantities. These impurities, including complex lead-copper-zinc oxides and other compounds, al-
though sub-microscopic in size, seriously affect the machineability of leaded brasses. The impurities may exist on the surface or be disbursed throughout more particularly on the lead particles. Since it is well known that the lead is added as a chip breaker, the impurities existing on the lead particles are detrimental to the machineability. Moreover the machineability of leaded brasses does not necessarily conform to the standard properties, such as tensile strength, percent elongation, etc. Thus machineability cannot be adequately determined in this manner.
The present invention contemplates the use of very specific proportions of certain elements added to the leaded brass, for example, calcium, lithium and magnesium. Apparently lithium is most effective, 'with calcium next in effectiveness. The use of such metals has been known for the casting of copper oxide scavenger for improving the pouring and casting qualities. These additive metals usually substantially boil off in casting. Moreover, it has always been felt that the more added the better, with cost being the only consideration. Effectiveness of such additive elements as calcium-lithium, on cleaning lead when zinc is present, was unknown. Zinc itself has been acting as a scavenging agent for the casting and whether the additive elements react with the zinc and copper, and not the lead has been heretofore 3,298,828 Patented Jan. 17, 1967 ice undetermined. Furthermore, before machining, the leaded brass must undergo operations such as drawing to rod. The effect of such operations was not entirely clear, particularly since grain size and distribution is affected.
The addition of these elements must be controlled very carefully to the type of material being melted. Otherwise adverse properties will result. For example the present invention contemplates the use of a substantial portion of scrap. This is probably, but not necessarily, due to the formation of complex chemical compounds not removed before casting, which complex compounds, although sub-microscopic in size, seriously affect tool wear by abrasion. Excessive use of the additive elemerits would adversely affect machineability, as would insufficient use. The exact reason for this is not readily determined, but the following examples provide some evidence. Distribution, quality, and size of the lead particles may be a factor, and excessive addition of these elements may cause too much cleaning in one area, thereby reducing uniformity and consequently machineability. Moreover, for fine machining an excess would seem to increase the tendency of undesirable firecracking. I
1 Example 1 A lot of free cutting brass billets for use as rod were cast at 2100 using the following charges:
Pounds Leaded brass alloy'scrap 850 Copper- Zinc 82 Lead 8 The resulting analysis showed 62.03% copper, 2.95% lead, 0.15% iron and other impurities, and the remainder zinc. Alpha-beta structure was present in normal proportion. The bil lets were extruded to round rod, drawn to 0.406 round, annealed to between 8001100, and again drawn to 0.328" round The resulting rod was all Alpha structure with normal lead distribution. The properties tested showed a tensile strength of 74,000 p.s.i., yield strength of 61,000 p.s.i., 10% elongation in 2 inches, with a consequent 48.7% reduction of area. On a subsequent machining operation the rod ran 34 hours before the high speed steel tools required sharpening to maintain the set machining depth. This was normal for free cutting, or leaded, brass.
Example 2 A lot of billets was cast at 2l00 using proportions similar to Example 1, but before pouring the melt, calcium and lithium in equal proportions were added using a standard phosphorizer, at a ratio of 8 ounces of calcium and lithium per 1000 lbs. of brass melt. The resulting analysis showed 62.04% copper, 3.12% lead, 0.20% iron and the other impurities, and the remainder zinc. Again alpha-beta structure was present in apparently normal proportion. Extruding, drawing and annealing was conducted in the manner of Example 1 with the result being all Alpha structure and apparently similar leaid distribution. Properties tested indicated 78,500 p.s.i. tensile strength, 61,200 p.s.i. yield strength, 10% elongation in 2" with consequent 45.2% reduction. Machining operations indicated a shearing off and a tendency to firecrack. The machine tools remained relatively sharp, since the shearing and firecracking were premature.
Example 3 The procedure according to Example 2 was followed except that the calcium lithium added was 2 ounces per 1000 pounds of leaded brass. Analysis disclosed a similar proportion of elements, with alpha-beta structure Q3 present. Preparation of rod-was as in the previous examples, and resulted in all Alpha structure. Tested properties were 73,500 p.s.i. tensile strength, 58,100 p.s.i. yield strength, 10% elongation in 2 inches with 46.9% area reduction. Results in machining were erratic, with some samples showing improved machineability and longer tool life, while other samples gave results similar to Example 1.
Example 4 The procedure according to Example 2 was again followed except that the calcium lithium ratio was 4 ounces per 1000 pounds melt. A similar proportion of elements again with alpha-beta structure present in normal percentages. After processing to rod as in the previous examples, apparently all Alpha structure was again the result. Properties were 70,600 p.s.i. tensile strength, 58,700 p.s.i. yield strength, 8.5% elongation in 2 inches with 41.1% area reduction. Machining was markedly improved, with tool life for the various samples being at least one third longer, with some samples as much as 200 percent longer. Neither shearing nor firecracking were evident, even with extremely thin walled machine parts.
Example Samples of the rod prepared in Example 4 were relief annealed at 525 F. The mechanical properties were then 70,900 p.s.i. tensile strength, 61,300 p.s.i. yield strength, 11% elongation in 2 inches, with 44.4% area reduction. Results in machining were as good as EX- ample' 4, again with no firccracking in thinwalled parts.
By using a typical comparative drill test, the superiority of the intermediate range was confirmed. The test consisted of a horizontal /s" drill acting on the specimen, with the drill mounted on a track and driven by a constant weight, the depth of drill in millimeters being measured over a constant time.
Using a drilling time of 60 seconds, to compare Examples 1 and 2, the following depth of drill resulted:
Example 1 (3 samples) A 4.5-5.0-50 Example 2 (3 samples) 4.54.0-4.0
This indicates relative superiority of no calciumlithium over the 8 ounce ratio.
Using a drill time of 30 seconds to compare Examples 1, 4 and 5 Example 1 3 samples) 2.0-2.0 2.s Example 4 (2 samples) 3.53.5 Example 5 (2 samples) 3.0-3.0
4 Using a drill time of 30 seconds to compare Examples 1, 3 and 4.
Example 1 (3 samples) 3.03.0-3.5 Example 4 (3 samples) 3.S4.03.5 Example 3 (3 samples) 4.53.02.5
Thus, example 4 exhibited regular superiority, while Example 3 was erratic, and suprisingly, Example 1 for drilling was superior to Example 2.
Having thus described certain details of my invention, I claim:
1. A method of treating brass to improve the machineability thereof which comprises adding to molten brass an additive selected from the group consisting of lithium and admixtures of lithium and calcium in an amount of from two to eight ounces of additive per thousand pounds of molten brass.
2. A method according to claim 1 wherein the brass consists essentially of copper, lead and zinc.
3. A method according to claim 2 wherein the additive is a mixture of equal parts by weight of lithium and calcium.
4. A method according to claim 2 wherein the additive is lithium.
5. Free-cutting brass having improved machining qualities containing an additive selected from the group of lithium and admixtures of lithium and calcium in an amount of from two to eight ounces of additive per thousand pounds of brass, said amount being determined by the addition of the said amount of additive to the brass when said brass is in a molten state.
6. Free-cutting brass according to claim 5 wherein the brass consists essentially of copper, lead and zinc.
7. Free-cutting brass according to claim 6 wherein the additive is a mixture of equal parts by weight of lithium and calcium.
8. Free-cutting brass according to claim 6 wherein the additive is lithium.
References Cited by the Examiner UNITED STATES PATENTS 2,062,426 12/1936 Pierson -157.5 2,169,188 3/1939 Kelly 75157.5 3,158,470 11/1964 Burgholf et al. 75-135 HYLAND BIZOT, Primary Examiner.
ROGER L. CAMPBELL, DAVID L. RECK,
Examiners.
D. L. REISDORF, R. O. DEAN, Assistant Examiners.
Claims (1)
- 5. FREE-CUTTING BRASS HAVING IMPROVED MACHINING QUALITIES CONTAINING AN ADDITIVE SELECTED FROM THE GROUP OF LITHIUM AND ADMIXTURES OF LITHIUM AND CALCIUM IN AN AMOUNT OF FROM TWO TO EIGHT OUNCES OF ADDITIVE PER THOUSAND POUNDS OF BRASS, SAID AMOUNT BEING DETERMINED BY THE ADDITION OF THE SAID AMOUNT OF ADDITIVE TO THE BRASS WHEN SAID BRASS IS IN A MOLTEN STATE.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US207802A US3298828A (en) | 1962-07-05 | 1962-07-05 | Treatment of leaded brass alloys for improving machineability and products so produced |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US207802A US3298828A (en) | 1962-07-05 | 1962-07-05 | Treatment of leaded brass alloys for improving machineability and products so produced |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3298828A true US3298828A (en) | 1967-01-17 |
Family
ID=22772056
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US207802A Expired - Lifetime US3298828A (en) | 1962-07-05 | 1962-07-05 | Treatment of leaded brass alloys for improving machineability and products so produced |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US3298828A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4139378A (en) * | 1973-11-21 | 1979-02-13 | The New Jersey Zinc Company | Powder-metallurgy of cobalt containing brass alloys |
| EP0007883A1 (en) * | 1978-07-31 | 1980-02-06 | Trefimetaux | Process for the heat treatment of drawn rods of brass containing lead |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2062426A (en) * | 1936-08-26 | 1936-12-01 | American Brass Co | Copper-zinc-lead-phosphorous alloy and articles |
| US2169188A (en) * | 1938-10-21 | 1939-08-08 | Westinghouse Electric & Mfg Co | Copper base alloy |
| US3158470A (en) * | 1961-05-08 | 1964-11-24 | Chase Brass & Copper Co | Copper base alloys and the method of treating the same to improve their machinability |
-
1962
- 1962-07-05 US US207802A patent/US3298828A/en not_active Expired - Lifetime
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2062426A (en) * | 1936-08-26 | 1936-12-01 | American Brass Co | Copper-zinc-lead-phosphorous alloy and articles |
| US2169188A (en) * | 1938-10-21 | 1939-08-08 | Westinghouse Electric & Mfg Co | Copper base alloy |
| US3158470A (en) * | 1961-05-08 | 1964-11-24 | Chase Brass & Copper Co | Copper base alloys and the method of treating the same to improve their machinability |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4139378A (en) * | 1973-11-21 | 1979-02-13 | The New Jersey Zinc Company | Powder-metallurgy of cobalt containing brass alloys |
| EP0007883A1 (en) * | 1978-07-31 | 1980-02-06 | Trefimetaux | Process for the heat treatment of drawn rods of brass containing lead |
| FR2432558A1 (en) * | 1978-07-31 | 1980-02-29 | Trefimetaux | LEADED BRASS STRETCHED BARS AND HEAT TREATMENT METHOD FOR SAID BARS |
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