Claims
- 1. A copper base alloy having a combination of high strength and high conductivity consisting essentially of from about 0.3 to about 1.6% by weight iron, with up to one-half the iron content being replaced by an element selected from the group consisting of nickel, manganese, cobalt and mixtures thereof; from about 0.01 to about 0.20% by weight magnesium; from about 0.10 to about 0.40% by weight phosphorus; up to about 0.5% by weight of an element selected from the group consisting of tin, antimony, and mixtures thereof; and the balance copper; with the proviso that the phosphorus to magnesium ratio comprises at least about 2.5 and that the ratio of phosphorus to the total content of phosphide formers (magnesium+iron+nickel+manganese+cobalt) ranges from about 0.22 to about 0.49.
- 2. A copper base alloy as in claim 1 wherein said iron content is from at least about 0.35% to about 1.6% by weight.
- 3. A copper base alloy as in claim 1 wherein said alloy consists essentially of from about 0.5 to about 1.0% by weight iron, with up to one-half the iron content being replaced by an element selected from the group consisting of nickel, manganese, cobalt and mixtures thereof; from about 0.15 to about 0.25% by weight phosphorus; from about 0.02 to about 0.1% by weight magnesium; up to about 0.35% by weight of an element selected from the group consisting of tin, antimony, and mixtures thereof; and the balance copper; with the proviso that the phosphorus to magnesium ratio ranges from about 2.5 to about 8.0 and that the ratio of phosphorus to the total content of phosphide formers ranges from about 0.25 to about 0.44.
- 4. A copper base alloy as in claim 1 wherein tin is present in an effective amount for increasing the strength of the alloy up to about 0.4% by weight and with the proviso that the ratio of phosphorus to the total content of phosphide formers ranges from about 0.22 to about 0.48.
- 5. A copper base alloy as in claim 4 wherein said ratio of phosphorus to the total content of phosphide formers ranges from about 0.22 to about 0.48.
- 6. A copper base alloy as in claim 3 wherein tin is present in an amount from 0.05 to about 0.35% by weight and with the proviso that the ratio of phosphorus to the total content of the phosphide formers ranges from about 0.27 to about 0.39.
- 7. A copper base alloy as in claims 1, 2 or 3 comprising a lead frame.
- 8. A copper base alloy as in claims 1, 2 or 3 which is essentially free of silicon.
- 9. A copper base alloy as in claims 1, 2 or 3 which is essentially free of silicon, aluminum and chromium.
- 10. A copper base alloy as in claims 1 or 4 wherein said alloy contains a mixture of phosphides comprising magnesium phosphide particles and phosphide particles of iron with or without an element selected from the group consisting of nickel, manganese, cobalt or mixtures thereof.
- 11. A copper base alloy as in claims 1 or 4 wherein the microstructure of the alloy consists essentially of some large 1 to 3 micron phosphide particles and a uniform dispersion of fine phosphide particles of less than about 0.5 microns in size.
- 12. A copper base alloy as in claims 4, 5 or 6 comprising an electrical connector.
- 13. A copper base alloy as in claim 1 wherein said ratio of phosphorus to magnesium ranges from about 3.0 to about 6.0.
- 14. A process for making a copper base alloy comprising:
- providing a copper base alloy consisting essentially of from about 0.3 to about 1.6% by weight iron, with up to one-half the iron content being replaced by an element selected from the group consisting of nickel, manganese, cobalt and mixtures thereof; from about 0.01 to about 0.20% by weight magnesium; from about 0.10 to about 0.40% by weight phosphorus; up to about 0.5% by weight of an element selected from the group consisting of tin, antimony, and mixtures thereof; and the balance copper; with the proviso that the phosphorus to magnesium ratio comprises at least about 2.5 and that the ratio of phosphorus to the total content of phosphide formers (magnesium+iron+nickel+manganese+cobalt) ranges from about 0.22 to about 0.49;
- hot working said alloy from a starting temperature of from about 850.degree. to about 980.degree. C. to a desired gauge;
- cold working said alloy from about 10 to about 90%; and
- annealing said alloy at a temperature of from about 400.degree. C. to about 800.degree. C. for an effective period of time to soften said alloy up to about 6 hours.
- 15. A process as in claim 14 wherein said alloy is further cold worked from about 10 to about 90% and then annealed at a temperature of from about 350.degree. to about 550.degree. C.
- 16. A process as in claim 14 wherein said annealed alloy is further cold worked from about 20 to about 80% to provide a desired temper.
- 17. A process as in claim 14 wherein said iron content is from at least about 0.35% to about 1.6% by weight.
- 18. A process as in claims 14 or 15 wherein said alloy consists essentially of from about 0.5 to about 1.0% by weight iron, with up to one-half the iron content being replaced by an element selected from the group consisting of nickel, manganese, cobalt and mixtures thereof; from about 0.15 to about 0.25% by weight phosphorus; from about 0.02 to about 0.1% by weight magnesium; up to about 0.35% by weight of an element selected from the group consisting of tin, antimony, and mixtures thereof; and the balance copper; with the proviso that the phosphorus to magnesium ratio ranges from about 2.5 to about 8.0 and that the ratio of phosphorus to the total content of phosphide formers ranges from about 0.25 to about 0.44.
- 19. A process as in claims 14 or 15 wherein tin is present in an effective amount for increasing the strength of the alloy up to about 0.4% by weight and with the proviso that the ratio of phosphorus to the total content of phosphide formers is from about 0.22 to about 0.48.
- 20. A process as in claims 14 or 15 wherein said ratio of phosphorus to the total content of phosphide formers is from about 0.24 to about 0.48.
- 21. A process as in claims 14 or 15 wherein tin is present in an amount from 0.05 to about 0.35% by weight and with the proviso that the ratio of phosphorus to the total content of phosphide formers ranges from about 0.27 to about 0.39.
- 22. A process as in claim 14 for providing an alloy having improved strength wherein said annealing step comprises an anneal for partial recrystallization and wherein said anneal is carried out at a temperature of from about 425.degree. to about 500.degree. C. so as to provide from about 10 to about 80% recrystallization of said alloy.
- 23. A process as in claim 22 wherein said alloy is further cold worked from about 10 to about 90% and then annealed to provide partial recrystallization of from about 10 to about 80% recrystallization of said alloy at a temperature of from about 375.degree. to about 475.degree. C.
- 24. A process as in claim 16 further including the step of forming said alloy into a semiconductor lead frame.
- 25. A process as in claim 16 wherein tin is present in an effective amount for increasing the strength of the alloy up to about 0.4% by weight and with the proviso that the ratio of phosphorus to the total content of phosphide formers is from about 0.24 to about 0.48 and further including the step of forming said alloy into an electrical connector.
Parent Case Info
This application is a continuation-in-part of Ser. No. 645,957, filed Aug. 31, 1984 by David B. Knorr et al. for "Copper Alloys Having An Improved Combination of Strength and Conductivity" now abandoned.
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Continuation in Parts (1)
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Number |
Date |
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Parent |
645957 |
Aug 1984 |
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