Copper alloy and process for obtaining same

Abstract: A copper base alloy consisting essentially of tin in an amount from about 1.0 to 11.0% by weight, phosphorous in an amount from about 0.01 to 0.35% by weight, iron in an amount from about 0.01 to about 0.8% by weight, optionally up to 15 wt% zinc, and the balance essentially copper, including phosphide particles uniformly distributed throughout the matrix, is described. The alloy is characterized by an excellent combination of physical properties. The process of forming the copper base alloy described herein includes casting, homogenizing, rolling, process annealing and stress relief annealing.

Description: The present invention relates to copper base alloys having utility in electrical applications and to a process for producing said copper base alloys. There are a number of copper base alloys that are used in connector, lead frame and other electrical applications because their special properties are well suited for these applications. Despite the existence of these alloys, there remains a need for copper base alloys that can be used in applications that require high yield strength in the order of 56,25 to 105,46 kg/mm 2 (80 to 150 KSI), together with good forming properties that allow one to make 180° bad-way bends with a R/T ratio of 1 or less plus low relaxation of stress at elevated temperatures and freedom of stress corrosion cracking. Alloys presently available do not meet all of these requirements or have high costs that make them less economical in the marketplace or have other significant drawbacks. It remains highly desirable to develop a copper base alloy satisfying the foregoing goals. Beryllium copper generally has very high strength and conductivity along with good stress relaxation characteristics; however, these materials are limited in their forming ability. One such limitation is the difficulty with 180° bad-way bends. In addition, they are very expensive and often require extra heat treatment after preparation of a desired part. Naturally, this adds even further to the cost. Phosphor bronze materials are inexpensive alloys with good strength and excellent forming properties. They are widely used in the electronic and telecommunications industries. However, they tend to be undesirable where they are required to conduct very high current under very high temperature conditions, for example under conditions found in automotive applications for use under the hood. This combined with their high thermal stress relaxation rate makes these materials less suitable for many applications. High copper, high conductivity alloys also have many desirable properties, but generally do not have mechanical strength desired for numerous applications. Typical ones of these alloys include, but are not limited to, copper alloys 110, 122, 192 and 194. Representative prior art patents include U.S. Patents 4,666,667, 4,627,960, 2,062,427, 4,605,532, 4,586,967, and 4,822,562. JP 58147139, JP 57002849, JP 62116745, JP 6184679, US 4605532, JP 3087341 or US 3923558 disclose several type of such alloys. Accordingly, it is highly desirable to develop copper base alloys having a combination of desirable properties making them eminently suitable for many applications. In accordance with the present invention, it has been found that the foregoing objective is readily obtained. Copper base alloys in accordance with the present invention comprise of tin in an amount from about 1.0 to 11.0%, phosphorous in an amount from about 0.01 to 0.35%, preferably from about 0.01% to 0.1%, iron in an amount from about 0.01% to 0.8%, preferably from about 0.05% to 0.25%, and the balance copper and unavoidable impurities, said alloys including phosphide particles uniformly distributed throughout the matrix, said phosphide particles including fine particles and coarse particles with said fine particles having a particle size from 50 to 250 Angstroms and said coarse particles having a particle size from 0.075 to 0.5 microns, and said fine and coarse particles being present in an amount and a distribution sufficient to cause said alloy to have a 180° bad-way bend with a R/T ratio of 1 or less. It is particularly advantageous to include nickel and/or cobalt in an amount up to about 0.5% each, preferably in an amount from 0.001% to about 0.5% each. Alloys in accordance with the present invention may also include zinc in an amount from 0.1 to 15%, lead in an amount up to 0. 05%, and up to 0. 1% each of aluminum, silver, boron, beryllium, calcium, chromium, indium, lithium, magnesium, manganese, lead, silicon, antimony, titanium, and zirconium. In an embodiment of the present invention, the copper base alloy may include zinc in an amount from about 9.0% to 15.0%. It is desirable and advantageous in the alloys of the present invention to provide phosphide particles of iron and/or nickel and/or magnesium or a combination thereof, uniformly distributed throughout the matrix since these particles serve to increase strength, conductivity, and stress relaxation characteristics of the alloys. The phosphide particles have a particle size of 50 Angstroms to about 0.5 microns and include a finer component and a coarser component. The finer component has a particle size ranging from about 50 to 250 Angstroms, preferably from about 50 to 200 Angstroms. The coarser component has a particle size generally from 0.075 to 0.5 microns, preferably from 0.075 to 0.125 microns. Percentage ranges throughout this application are percentages by weight. The alloys of the present invention enjoy a variety of excellent properties making them eminently suitable for use as connectors, lead frames, springs and other electrical applications. The alloys should have an excellent and unusual combination of mechanical strength, formability, thermal and electrical conductivities, and stress relaxation properties. The process of the present invention comprises: casting a copper base alloy having a composition as aforesaid; homogenizing at least once for at least two hours at temperatures from about 537,8 to 787,8°C (1000 to 1450°F) ; rolling to finish gauge including at least one process anneal for at least one hour at 343,3 to 648,9°C (650 to 1200°F) ; optionally slow cooling at 11,1 to 111,1°C (20 to 200°F) per hour; and stress relief annealing for at least one hour at a temperature in the range of 148,9 to 315,6°C (300 to 600°F), thereby obtaining a copper alloy including phosphide particles uniformly distributed throughout the matrix. Nickel and/or cobalt may be included in the alloy as above. The alloys of the present invention are modified phosphor bronze alloys. They are characterized by higher strengths, better forming properties, higher conductivity, and stress relaxation properties that represent a significant improvement over the same properties of unmodified phosphor bronzes. Modified phosphor bronze alloys in accordance with an embodiment of the present invention include those copper base alloys comprising tin in an amount from about 1.5 to 11%, phosphorous in an amount from about 0.01 to 0.35%, preferably from about 0.01 to 0.1%, iron in an amount from about 0.01 to 0.8%, preferably from about 0.05 to 0.25%, and the balance copper and unavoidable impurities. These alloys have phosphide particles uniformly distributed throughout the matrix, said phosphide particles including fine particles and coarse particles with said fine particles having a particle size from 50 to 250 Angstroms and said coarse particles having a particle size from 0.075 to 0.5 microns, and said fine and coarse particles being present in an amount and a distribution sufficient to cause said alloy to have a 180° bad-way bend with a R/T ratio of 1 or less. These alloys may also include nickel and/or cobalt in an amount up to about 0.5% each, preferably from about 0.001 to 0.5% of one or combinations of both, zinc in an amount up to about 0.3% max, and lead in an amount up to about 0.05% max. one may include one or more of the following elements in the alloy combination: aluminum, silver, boron, beryllium, calcium, chromium, indium, lithium, magnesium, manganese, lead, silicon, antimony, titanium, and zirconium. These materials may be included in amounts less than 0.1%, each generally in excess of 0.001 each. The use of one or more of these materials improves the mechanical properties such as stress relaxation properties; however, larger amounts may affect conductivity and forming properties. The aforesaid phosphorous addition allows the metal to stay deoxidized making it possible to cast sound metal within the limits set for phosphorous, and with thermal treatment of the alloys, phosphorous forms a phosphide with iron and/or iron and nickel and/or iron and magnesium and/or a combination of these elements, if present, which significantly reduces the loss in conductivity that would result if these materials were entirely in solid solution in the matrix. It is particularly desirable to provide iron phosphide particles uniformly distributed throughout the matrix as these help improve the stress relaxation properties by blocking dislocation movement. Iron in the range of 0.01 to 0.8% and particularly 0.05 to 0.25% increases the strength of the alloys, promotes a fine grain structure by acting as a grain growth inhibitor and in combination with phosphorous in this range helps improve the stress relaxation properties without negative effect on electrical and thermal conductivities. Nickel and/or cobalt in an amount from about 0.001 to 0.5% each are desirable additives since they improve stress relaxation properties and strength by refining the grain and through distribution throughout the matrix, with a positive effect on the conductivity. The process for making these alloys includes casting an alloy having a composition as aforesaid. Any suitable casting technique known in the art such as horizontal continuous casting may be used to form a strip having a thickness in the range of from about 12,70 to 19,05 mm (0.500 to 0.750 inches). The processing includes at least one homogenization for at least two hours, and preferably for a time period in the range of from about 2 to about 24 hours, at temperatures in the range of from about 537,8 to 787,8°C (1000 to 1450°F). At least one homogenization step may be conducted after a rolling step. After homogenization, the strip may be milled once or twice to remove from about 0,508 to 2,54 mm (0.020 to 0.100 inches) of material from each face. The material is then rolled to final gauge, including at least one process anneal at 343,3 to 648,9°C (650 to 1200°F) for at least one hour and preferably for about 1 to 24 hours, followed by slow cooling to ambient at 11,1 to 111,1°C (20 to 200°F) per hour. The material is then stress relief annealed at final gauge at a temperature in the range of 148,9 to 315,6°C (300 to 600°F) for at least one hour and preferably for a time period in the range of about 1 to 20 hours. This advantageously improves formability and stress relaxation properties. The thermal treatments provide the alloys of the present invention with phosphide particles of iron and/or nickel and/or magnesium or a combination thereof uniformly distributed throughout the matrix. The phosphide particles increase the strength, conductivity, and stress relaxation characteristics of the alloys. The phosphide particles have a particle size of about 50 Angstroms to about 0.5 microns and include a finer component and a coarser component. The finer component has a particle size of about 50 to 250 Angstroms, preferably from about 50 to 200 Angstroms. The coarser component has a particle size generally from 0.075 to 0.5 microns, preferably from 0.075 to 0.125 microns. Alloys formed in accordance with the process of the present invention and having the aforesaid compositions are capable of achieving an electrical conductivity of from about 12 to 35% IACS. The foregoing coupled with the desired metallurgical structure should give the alloys a high stress retention ability, for example over 60% at 150°C, after 1000 hours with a stress equal to 75% of its yield strength on samples cut parallel to the direction of rolling, makes these alloys very suitable for a wide variety of applications requiring high stress retention capabilities. Moreover, the present alloys do not require further treatment by stampers. The alloys of the present invention may be tailored to provide a desired set of properties by varying the tin content of the alloys while maintaining the other constituents within the aforesaid ranges and processing the alloy in the manner described above. The following table demonstrates the properties which may be obtained for different tin contents. No. Tin Content wt% Tensile Strength kg/mm 2 (ksi) Yield Strength 0.2% Offset kg/mm 2 (ksi) 1 9 - 11 91,40-105,46 (130-150) 87,88-101,94 (125-145) 2 7 - 9 84,37-98,43 (120-140) 80,85-94,91 (115-135) 3 5 - 7 77,34-91,40 (110-130) 73,82-87,88 (105-125) 4 3 - 5 70,31-84,37 (100-120) 66,79-80,85 (95-115) 5 1.5 - 3 63,28-77,34 (90-110) 59,76-73,82 (85-105) Alloys in accordance with the present invention are also capable of achieving a very desirable set of mechanical and forming properties, also by varying the tin content of the alloy while maintaining the other constituents within the aforesaid ranges and processing the alloy as described above. The following table illustrates the types of properties which may be achieved. Tin (wt%) Tensile Strength kg/mm 2 (ksi) Yield Strength 0.2% Offset kg/mm 2 (ksi) Elongation % Bad-way 180° Bend Width To Thickness Ratio of up to 10:1 7-9 77,34-91,40 (110-130) 73,82-87,88 (105-125) 5-10 Radius to Thickness Ratio = 1 5-7 70,31-84,37 (100-120) 67,49-81,56 (96-116) 5-10 Radius to Thickness Ratio = 1 3-5 64,68-78,74 (92-112) 61,87-75,93 (88-108) 5-10 Radius to Thickness Ratio = 1 1.5-3 59,76-73,82 (85-105) 56,24-70,31 (80-100) 5-10 Radius to Thickness Ratio = 1 As can be seen from the foregoing tables, alloys in accordance with the present invention not only have higher strengths, but also have particularly desirable combinations of strength and formability. The properties are such that the alloys of the present invention can replace alloys like beryllium coppers and copper alloys with nickel silicon, e.g. CDA 7025 and 7026, in many applications. This is particularly useful to connector manufacturers since the alloys of the present invention cost less than the alloys which they can replace. Yet another embodiment of a modified phosphor bronze in accordance with the present invention comprises a copper base alloy comprising tin in an amount from about 1.0 to 4.0%, zinc in an amount from about 9.0 to 15.0%, phosphorous in an amount from about 0. 01 to 0.2%, iron in an amount from about 0.01 to 0.8%, nickel and/or cobalt in an amount from about 0.001 to 0.5%, and the balance copper and unavoidable impurities, said alloy including phosphide particles uniformly distributed throughout the matrix, said phosphide particles including fine particles and coarse particles with said fine particles having a particle size from 50 to 250 Angstroms and said coarse particles having a particle size from 0.075 to 0.5 microns, and said fine and coarse particles being present in an amount and a distribution sufficient to cause said alloy to have a 180° bad-way bend with a R/T ratio of 1 or less. The aforesaid phosphorous addition allows the metal to stay deoxidized making it possible to cast sound metal within the limits set for phosphorous, and with thermal treatment of the alloy, phosphorous forms a phosphide with iron and/or iron and nickel and/or iron and magnesium or a combination of these elements, if present, which significantly reduces the loss in conductivity that would result if these materials were entirely in solid solution in the matrix. It is particularly desirable to provide iron phosphide particles uniformly distributed throughout the matrix as these help improve the stress relaxation properties by blocking dislocation movement. Iron in the range of 0.01 to 0.8% increases the strength of the alloys, promotes a fine grain structure by acting as a grain growth inhibitor and in combination with phosphorous in this range helps improve the stress relaxation properties without negative effect on electrical and thermal conductivities. Zinc in an amount from 9.0 to 15.0% helps deoxidize the metal, helping the castings to be sound without use of excessive phosphorous that can hurt conductivities. Zinc also helps in keeping the metal oxide free for good adhesion in plating and increases strength. Nickel and/or cobalt in an amount from about 0.001 to 0.5% each are desirable additives since they improve stress relaxation properties and strength by refining the grain and through distribution throughout the matrix, with a positive effect on the conductivity. One may include one or more of the following elements in the alloy combination: aluminum, silver, boron, beryllium, calcium, chromium, cobalt, indium, lithium, magnesium, manganese, zirconium, lead, silicon, antimony, and titanium. These materials may be included in amounts less than 0.1% each generally in excess of 0.001 each. The use of one or more of these materials improves the mechanical properties such as stress relaxation properties; however, larger amounts may effect conductivity and forming properties. This alternative alloy may be processed using the technique described hereinbefore. Using such a technique, the alloy is capable of achieving the following properties: a tensile strength in the range of 63,28 to 73,82 kg/mm 2 (90 to 105 ksi), a yield strength at 0.2% offset in the range of 59,76 to 70,31 kg/mm 2 (85 to 100 ksi), elongation in the range of 5 to 10%, and bend properties for a 180° bad-way bend (width:thickness ratio up to 10:1) of radius: thickness ratio equal to 1. The alloy is also characterized by the presence of the aforementioned desirable phosphide particles uniformly distributed throughout the matrix. Still other alloys in accordance with the present invention and a third embodiment include tin from 2.5-4%, phosphorus from 0.01-0.20%, iron from 0.05-0.80%, zinc from 0.3-5%, balance copper and unavoidable impurities, with phosphide particles uniformly distributed throughout the matrix. These alloys of the present invention have a 0.2% offset yield strength of 80 to 100 KSI along with the ability of the alloys to make 180° bad-way bends at a radius no more than the thickness of the alloy strip. In addition, the alloys achieve an electrical conductivity of approximately 30% IACS or better which makes the alloys suitable for high current applications. The foregoing combined with a good thermal conductivity of 1,298 J/cm 2 /s/°C/cm (75 BTU/SQ FT/FT/HR/DEGREE F) and a metallurgical structure that give the alloys a high stress retention ability, for example, over 60% at 150°C, after 1,000 hours with a stress equal to 75% of its yield strength, on samples cut parallel to direction of rolling, makes these alloys very suitable for the high temperature conditions under an automobile hood as well as other applications requiring a combination of high conductivity and high stress retention capabilities. Moreover, the present alloys do not require further treatment by stampers and are relatively inexpensive. A variation of this third embodiment alloy may include tin in an amount greater than 2.5% and up to 4.0%, phosphorous is present in an amount from 0.01 to 0.2% and particularly 0.01 to 0.05%. Phosphorous allows the metal to stay deoxidized making it possible to cast sound metal within the limits set for phosphorous, and with thermal treatment of the alloys phosphorous forms a phosphide with iron and/or iron and nickel and/or iron and magnesium or combinations of these elements, if present, which significantly reduces the loss in conductivity that would result if these materials were entirely in solid solution in the matrix. It is particularly desirable to provide iron phosphide particles uniformly distributed throughout the matrix as these help improve the stress relaxation properties by blocking dislocation movement. Iron may be added to the third embodiment alloy in the range of 0.05 to 0.8% and particularly 0.05 to 0.25% increases the strength of the alloys, promotes a fine grain structure by acting as a grain growth inhibitor and in combination with phosphorous in this range helps improve the stress relaxation properties without negative effect on electrical and thermal conductivities. Zinc may be added to the third embodiment alloy in the range of 0.3 to 5.0% helps deoxidize the metal, helping the castings to be sound without use of excessive phosphorous that can hurt conductivities. Zinc also helps in keeping the metal oxide free for good adhesion in plating. It is desirable to restrict the upper zinc level under 5.0% and particularly under 2.5% in order to keep the conductivities high. Zinc in the lower amounts of this range will achieve even higher conductivities. Nickel and/or cobalt may be added to the third embodiment alloy in an amount from 0.001 to 0.5% each, and preferably 0.01 to 0.3% each, are desirable additives since they improve stress relaxation properties and strength by refining the grain and through distribution throughout the matrix, with a positive effect on the conductivity. Nickel is preferred. One may include one or more of the following elements in the alloy combination: aluminum, silver, boron, beryllium, calcium, chromium, cobalt, indium, lithium, magnesium, manganese, zirconium, lead, silicon, antimony and titanium. These materials may be included in amounts less than 0. 1% each generally in excess of 0. 001 each. The use of one or more of these materials improves mechanical properties such as stress relaxation properties; however, larger amounts may effect conductivity and forming properties. The process of the present invention includes casting an alloy having a composition as aforesaid, and including at least one homogenization for at least one hour, and preferably for 2-20 hours, at 537,8-787,8°C (1000-1450°F). At least one homogenization step may be conducted after a rolling step. The casting process forms a tin-copper compound and the homogenization treatment breaks up the unstable tin-copper compound and puts the tin in solution. The material is rolled to final gauge, including at least one process anneal at 343,3-648,9°C (650-1200°F) for at least one hour and preferably for 2-20 hours, followed by slow cooling to ambient at 11,1-111,1°C (20-200°F) per hour. The material is stress relief annealed at final gauge at 148,9-315,6°C (300-600°F) for at least one hour and preferably for 2-16 hours. This advantageously improves formability and stress relaxation properties. The thermal treatments form the desirable particles of phosphides of iron or nickel or magnesium or combinations thereof and uniformly distributes same throughout the matrix, and aids in obtaining the improved properties of the alloy of the present invention. The phosphide particles have a particle size of 50 Angstroms to 0.3 microns and generally and advantageously include a finer component and a coarser component. The finer component has a particle size of 50-250 Angstroms preferably from 50-200 Angstroms, and the coarser component has a particle size generally from 0.075 to 0.3 microns and preferably from 0.075 to 0.125 microns. As an alternative and fourth embodiment, the present invention includes an alloy containing tin in an amount from 1.0% and up to 4.0%, zinc from 0.1 to less than 1%, balance copper and unavoidable impurities. The phosphorus and iron contents are as in the third embodiment, and nickel and/or cobalt may be added as in the third embodiment, with phosphide particles as aforesaid. The above fourth embodiment alloy is processed as in the third embodiment alloy and is capable of achieving an electrical conductivity of approximately 33% IACS or better which makes the alloy suitable for high current applications. The foregoing combined with a good thermal conductivity of 1,419 J/cm 2 /s/°C/cm (82 BTU/SQ FT/FT/HR/DEGREE F) and a metallurgical structure that gives the alloy a high stress retention ability of over 60% at 150°C after 1,000 hours with a stress equal to 75% of its yield strength on samples cut parallel to direction of rolling, makes this alloy as suitable for high temperature conditions as the previous alloy. This alloy also forms phosphides as with the third embodiment alloy. Also, the additional alloying ingredients noted for the third embodiment alloy may be used for this alloy. This alloy is capable of achieving the following properties: Tensile Strength kg/mm 2 (KSI) Yield Strength 0.2% Offset kg/mm 2 (KSI) Elongation % Bend Properties 180° Bad-way Bend (Width: Thickness Ratio Up to 10:1) 56,24-70,31 (80-100) 56,24-70,31 (80-100) 5-10 Radius: Thickness Ratio = 1 As a fifth embodiment alloy, the present invention includes an alloy containing tin in an amount from 1.0% and up to 4.0%, tin and zinc from 1.0 to 6.0%, balance copper and unavoidable impurities. The phosphorus and iron contents are as in the third embodiment and nickel and/or cobalt are added in the amount of 0.11 to 0.50% each, and phosphide particles are present as in the third embodiment. The above fifth embodiment alloy is processed as for the third embodiment and is capable of achieving electrical conductivity of approximately 32% or better which makes the alloy suitable for high current applications. The foregoing combined with a good thermal conductivity of 1,384 J/cm 2 /s/°C/cm (80 BTU/SQ FT/FT/HR DEGREE F) and a metallurgical structure that gives the alloy a high stress retention ability of over 60% at 150°C after 1,000 hours with a stress equal to 75% of its yield strength, on samples cut parallel to direction of rolling, makes this alloy as suitable for high temperature conditions as the previous alloys. This alloy also forms phosphides as with the third embodiment alloy. Also, the additional alloying ingredients noted for the third embodiment alloy may be used for this alloy. This alloy is capable of achieving the following properties: Tensile Strength kg/mm 2 (KSI) Yield Strength 0.2% Offset kg/mm 2 (KSI) Elongation % Bend Properties 180° Bad-way Bend (Width: Thickness Ratio Up to 10:1) 59,76-70,31 (85-100) 59,76-70,31 (85-100) 5-10 Radius: Thickness Ratio = 1 As a sixth embodiment alloy, the present invention includes an alloy containing tin in an amount from 1.0% up to 4.0% and zinc from 6.0 to 12.0%, balance copper and unavoidable impurities. The phosphorus and iron contents are as in the third embodiment and nickel and/or cobalt may be added as in the third embodiment, and phosphide particles are present as in the third embodiment. The above alloy is processed as for the third embodiment and is capable of achieving electrical conductivity of approximately 30% which makes the alloy suitable for high current applications. The foregoing combined with a good thermal conductivity of 1,298 J/cm 2 /s/°C/cm (75 BTU/SQ FT/FT/HR/DEGREE F) and a metallurgical structure that is capable of giving the alloy a high stress retention ability of over 60% at 150°C after 1,000 hours with a stress equal to 75% of yield strength, on samples cut parallel to direction of rolling, makes this alloy as suitable for high temperature conditions as the previous alloys. This alloy also forms phosphides as with the third embodiment alloy. Also, the additional alloying ingredients noted for the third embodiment alloy may be used for this alloy. This alloy is capable of achieving the following properties: Tensile Strength kg/mm 2 (KSI) Yield Strength 0.2% Offset kg/mm 2 (KSI) Elongation % Bend Properties 180° Bad-way Bend (Width: Thickness Ratio Up to 10:1) 63,28-73,82 (90-105) 59,76-70,31 (85-100) 5-10 Radius: Thickness Ratio = 1 As a seventh embodiment alloy, the present invention includes an alloy containing tin in an amount from 1.0% up to 4.0%, zinc from 1.0 to 6.0% and iron from 0.01 to 0.05%, balance copper and unavoidable impurities. The phosphorus content is as in the third embodiment alloy and nickel and/or cobalt may be added as in the third embodiment, and phosphide particles are present as in the third embodiment. The above alloy is processed as in the third embodiment and is capable of achieving electrical conductivity of approximately 33% which makes the alloy suitable for high current applications. The foregoing combined with a good thermal conductivity of 1,419 J/cm 2 /s/°C/cm (82 BTU/SQ FT/FT/HR/DEGREE F) and a metallurgical structure that is capable of giving the alloy a high stress retention ability of over 60% at 150°C after 1,000 hours with a stress equal to 75% of its yield strength, on samples cut parallel to direction of rolling, makes this alloy as suitable for high temperature conditions as the previous alloys. This alloy also forms phosphides as with the third embodiment alloy. Also, the additional alloying ingredients noted for the third embodiment alloy may be used for this alloy. This alloy is capable of achieving the following properties: Tensile Strength kg/mm 2 (KSI) Yield Strength 0.2% Offset kg/mm 2 (KSI) Elongation % Bend Properties 180° Bad-way Bend (Width: Thickness Ratio Up to 10:1) 56,24-70,31 (80-100) 56,24-70,31 (80-100) 5-10 Radius: Thickness Ratio = 1 The present invention will be more readily understood from a consideration of the following examples. EXAMPLE I An alloy having the following composition: tin-2.7%; phosphorous-0.04%; iron-0.09%; zinc-2.2%; nickel-0.12%; balance copper and unavoidable impurities was cast using a horizontal continuous casting machine in a thickness of 15,75 mm (.620") and width of 381 mm (15"). The material was thermally treated at 732,2°C (1350°F) for 14 hours followed by milling to remove 0,508 mm (.020") per side. The alloys were then cold rolled to 9,144 mm (0.360") followed by another thermal treatment at 732,2°C (1350°F) for 12 hours and another milling of 5,08 mm (.20") per side to enhance the surface quality. The material was then cold rolled on a 2-high mill to 3,048 mm (.120") followed by bell annealing at 537,8°C (1000°F) for 12 hours. The materials were then further cold worked and thermally treated at 398,9 and 365,6°C (750°F and 690°F) at 8 and 11 hours, respectively, followed by slow cooling, followed by finish rolling to final gauge at 0,2489 mm (0.0098"). Material samples were finally stress relief annealed at 218,3 and 260°C (425°F and 500°F) for 4 hours, respectively. The materials were tested for mechanical properties and forming properties to determine the capabilities to make bends at angles up to 180° at different radii. The results are shown in TABLE III, below. The samples were characterized by the presence of iron-nickel-phosphide-particles distributed throughout the matrix. Tensile Strength kg/mm 2 (KSI) 0.2% Offset Yield Strength kg/mm 2 (KSI) Elongation 50,8 mm (2") Gauge Length Min. R/T Ratio For 180° Bad-way Bend As Rolled 67,49 (96) 65,39 (93) 5,08 (2) 1 Relief Annealed at 218°C (425°F) 64,68 (92) 64,33 (91.5) 17,78 (7) <1 Relief Annealed at 260°C (500°F) 63,28 (90) 61,17 (87) 27,64 (11) <1 EXAMPLE 2 The procedure of Example 1 was repeated using a 260°C (500°F) stress relief anneal and with an alloy having the following composition. tin 2.7% phosphorous 0.03% iron 0.09% zinc 1.9% nickel 0.08% copper balance The results are shown in Table IV, below. The samples were characterized by the presence of iron-nickel-phosphide particles distributed throughout the matrix. Tensile Strength kg/mm 2 (KSI) Elongation 50,8 mm (2") Gauge Length Relief Annealed at 260°C (500°F) 6328 (90) 10%

Claims: A copper base alloy comprising tin in an amount from 1.0 to 11.0% by weight, phosphorous in an amount from 0.01 to 0.35% by weight, iron in an amount from 0.01 to 0.8% by weight, and the balance copper and unavoidable impurities, said alloy including phosphide particles uniformly distributed throughout the matrix, said phosphide particles including fine particles and coarse particles with said fine particles having a particle size from 50 to 250 Angstroms and said coarse particles having a particle size from 0.075 to 0.5 microns, and said fine and coarse particles being present in an amount and a distribution sufficient to cause said alloy to have a 180° bad-way bend with a R/T ratio of 1 or less. A copper base alloy comprising tin in an amount from 1.0 to 4.0% by weight, phosphorous in an amount from 0.01 to 0.20% by weight, iron in an amount from 0.01 to 0.80% by weight, zinc from 0.1 to 12.0% and the balance copper and unavoidable impurities, said alloy including phosphide particles uniformly distributed throughout the matrix, said phosphide particles including fine particles and coarse particles with said fine particles having a particle size from 50 to 250 Angstroms and said coarse particles having a particle size from 0.075 to 0.5 microns, and said fine and coarse particles being present in an amount and a distribution sufficient to cause said alloy to have a 180° bad-way bend with a R/T ratio of 1 or less. A copper base alloy according to claim 1 or claim 2, including a material selected from the group consisting of nickel, cobalt and mixtures thereof in an amount from 0.001 to 0.5% by weight each, and at the expense of copper. A copper base alloy according to any one of claims 1-3, wherein said alloy further includes magnesium in an amount up to 0.1% by weight at the expense of copper said phosphide particles are selected from the group consisting of iron nickel phosphide particles, iron magnesium phosphide particles, iron phosphide particles, magnesium nickel phosphide particles, magnesium phosphide particles and mixtures thereof. A copper base alloy according to claim 1, further including zinc in an amount up to 0.3% by weight and lead in an amount up to 0.05% by weight, at the expense of copper. A copper base alloy according to claim 1, wherein said tin content is from 1.5 to 11.0% by weight, said phosphorous content is from 0.01 to 0.10% by weight, and said iron content is from 0.05 to 0.25% by weight. A copper base alloy according to claim 1, wherein said tin content is from 1.0 to 4.0% by weight and said phosphorous content is from 0.01 to 0.2% by weight and wherein said alloy further includes zinc in an amount of from 9.0 to 15.0% by weight and a material selected from the group consisting of nickel, cobalt and mixtures thereof in an amount from 0.001 to 0.5% by weight each, at the expense of copper. A copper base alloy according to claim 1, wherein said tin content is from 1.5 to 3.0% by weight. A copper base alloy according to claim 1, wherein said tin content is from 3.0 to 5.0% by weight. A copper base alloy according to claim 1, wherein said tin content is from 5.0 to 7.0% by weight. A copper base alloy according to claim 1, wherein said tin content is from 7.0 to 9.0% by weight. A copper base alloy according to claim 1, wherein said tin content is from 9.0 to 11.0% by weight. Copper base alloys according to claim 2, wherein said tin content is from 2.5% up to 4.0%, said iron content is from 0.05 to 0.80%, and said zinc content is from 0.3 to 5.0%. Copper base alloys according to claim 2, wherein said zinc content is from 0.1 to less than 1% and said iron content is from 0.05 to 0.80%. Copper base alloys according to claim 2, wherein said iron content is from 0.05 to 0.80% and said zinc content is from 1.0 to 6.0%. Copper base alloys according to claim 2, wherein said iron content is from 0.05 to 0.80% and said zinc content is from 6.0 to 12.0%. Copper base alloys according to claim 2, wherein said iron content is from 0.01 to 0.05% and said zinc content is from 1.0 to 6.0%. Copper base alloys according to claim 3, including nickel in an amount from 0.01 to 0.3%. Copper base alloys according to claim 1 or claim 2 further comprising a material selected from the group consisting of nickel, cobalt and mixtures thereof in an amount from 0.001 to 0.5% each and at least one material selected from the group consisting of aluminum, silver, boron, beryllium, calcium, chromium, cobalt, indium, lithium, magnesium, manganese, zirconium, lead, silicon, antimony, and titanium each in an amount in excess of 0.001% and less than 0.1%, at the expense of copper. A copper base alloy comprising tin in an amount from 1.0 to 4.0% by weight, zinc in an amount from 9.0 to 15.0% by weight, phosphorous in an amount from 0.01 to 0.2% by weight, iron in an amount from 0.01 to 0.8% by weight, a material selected from the group consisting of nickel, cobalt, and mixtures thereof in an amount from 0.001 to 0.5% by weight each, and the balance copper and unavoidable impurities, said alloy including phosphide particles uniformly distributed throughout the matrix, said phosphide particles including fine particles and coarse particles with said fine particles having a particle size from 50 to 250 Angstroms and said coarse particles having a particle size from 0.075 to 0.5 microns, and said fine and coarse particles being present in an amount and a distribution sufficient to cause said alloy to have a 180° bad-way bend with a R/T ratio of 1 or less. A process for preparing a copper base alloy which comprises: casting a copper base alloy comprising tin in an amount from 1.5 to 11.0% by weight, phosphorous in an amount from 0.01 to 0.35% by weight, iron in an amount from 0.01 to 0.8% by weight, and the balance copper and unavoidable impurities; homogenizing said cast alloy at least once for at least two hours at a temperature from 537,8 to 787,8°C (1000 to 1450°F) ; rolling to final gauge including at least one process anneal for at least one hour at 343,3 to 648,9°C (650 to 1200°F) followed by slow cooling at a rate of 11,1 to 111,1°C (20 to 200°F) per hour; and stress relief annealing at final gauge for at least one hour at 148,9 to 315,6°C (300 to 600°F), thereby obtaining a copper base alloy including phosphide particles uniformly distributed throughout the matrix and said phosphide particles including coarse particles having a particle size from 0.075 to 0.5 microns and fine particles having a particle size from 50 to 250 Angstroms. Process for preparing copper base alloys, which comprises: casting a copper base alloy comprising tin in an amount from 1.0% up to 4.0%, phosphorous from 0.01 to 0.20%, iron from 0.01 to 0.80%, zinc from 0.1 to 12.0%, and the balance copper and unavoidable impurities; homogenizing said cast alloy at least once for at least two hours at a temperature from 537,8 to 787,8°C (1000 to 1450°F) ; rolling to final gauge including at least one process anneal for at least one hour at 343,3 to 648,9°C (650 to 1200°F) followed by slow cooling at a rate of 11,1 to 111,1°C (20 to 200°F) per hour; and stress relief annealing at final gauge for at least one hour at 148,9 to 315,6°C (300 to 600°F), thereby obtaining a copper alloy including phosphide particles uniformly distributed throughout the matrix and said phosphide particles including coarse particles having a particle size from 0.075 to 0.5 microns and fine particles having a particle size from 50 to 250 Angstroms. Process according to claim 21 or claim 22, wherein said copper base alloy being cast includes a material selected from the group consisting of nickel, cobalt and mixtures thereof in an amount from 0.001 to 0.5% each, at the expense of copper. Process according to claim 23, wherein said copper base alloy being cast includes magnesium and said phosphide particles are selected from the group consisting of iron nickel phosphide particles, iron magnesium phosphide particles, iron phosphide particles, magnesium nickel phosphide particles, magnesium phosphide and mixtures thereof, and wherein said phosphide particles have a particle size of from 50 Angstroms to 0.5 microns. Process according to claim 21 or claim 22, including two homogenization steps, wherein at least one homogenization step is subsequent to a rolling step and wherein the homogenization steps are for 2 to 24 hours each. Process according to claim 21 or claim 22, wherein said process anneal is for 1 to 24 hours and said stress relief anneal is for 1 to 20 hours. A process for preparing a copper base alloy which comprises: casting a copper base alloy comprising tin in an amount from 1.0 to 4.0% by weight, zinc in an amount from 9.0 to 15.0% by weight, phosphorous in an amount from 0.01 to 0.2% by weight, iron in an amount from 0.01 to 0.8% by weight, a material selected from the group consisting of nickel, cobalt and mixtures thereof in an amount from 0.001 to 0.5% by weight each, and the balance copper and unavoidable impurities; homogenizing at least once for at least two hours at a temperature from 537,8 to 787,8°C (1000 to 1450°F) ; rolling to final gauge including at least one process anneal for at least one hour at 343,3 to 648,9°C (650 to 1200°F) followed by slow cooling at a rate of 11,1 to 111,1°C (20 to 200°F) per hour; and stress relief annealing at final gauge for at least one hour at 148,9 to 315,6°C (300 to 600°F), thereby obtaining a copper base alloy including phosphide particles uniformly distributed throughout the matrix and said phosphide particles including coarse particles having a particle size from 0.075 to 0.5 microns and fine particles having a particle size from 50 to 250 Angstroms. Process according to claim 21 or claim 22 wherein said copper base alloy being cast includes a material selected from the group consisting of nickel, cobalt and mixtures thereof in an amount from 0.001 to 0.5% each and at least one material selected from the group consisting of aluminum, silver, boron, beryllium, calcium, chromium, cobalt, indium, lithium, magnesium, manganese, zirconium, lead, silicon, antimony and titanium each in an amount in excess of 0.001% and less than 0.1%, at the expense of copper. Process according to claim 27 wherein said copper base alloy being cast includes a material selected from the group consisting of aluminum, silver, boron, beryllium, calcium, chromium, cobalt, indium, lithium, magnesium, manganese, zirconium, lead, silicon, antimony, and titanium each in an amount in excess of 0.001% and less than 0.1%, at the expense of copper. Copper base alloy according to claim 20 further comprising a material selected from the group consisting of aluminum, silver, boron, beryllium, calcium, chromium, cobalt, indium, lithium, magnesium, manganese, zirconium, lead, silicon, antimony, and titanium each in an amount in excess of 0.001% and less than 0.1%, at the expense of copper.

Inventors: BHARGAVA ASHOK K, BHARGAVA, ASHOK K.
Applicants: WATERBURY ROLLING MILLS INC, WATERBURY ROLLING MILLS, INC.
Application year: 1997
Main classification: C22C9
IPC codes: C22C9, C22F1, H01B1