US2003029532A1PendingUtilityA1

Nickel containing high copper alloy

Assignee: OLIN CORPPriority: May 24, 2001Filed: May 24, 2001Published: Feb 13, 2003
Est. expiryMay 24, 2021(expired)· nominal 20-yr term from priority
C22F 1/08C22C 9/02C22C 9/06C22C 9/00
43
PatentIndex Score
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Claims

Abstract

A high copper alloy with good resistance to stress relaxation at temperatures of up to at least 150° C., consists, by weight, essentially of from 0.8% to 3% of iron, from 0.3% to 2% of nickel, from 0.6% to 1.4% of tin, from 0.005% to 0.35% phosphorous and the remainder copper and inevitable impurities. The alloy has an electrical conductivity in excess of 40% IACS and a yield strength of 70 ksi or higher at final gauge following a relief anneal. Over 75% of an imposed stress remains after exposure to 150° C. for 3000 hours. The combination of good electrical conductivity, high strength and high stress relaxation resistance makes the alloys particularly suitable for under the hood automotive electrical connectors.

Claims

exact text as granted — not AI-modified
We claim:  
     
         1 . A copper alloy consisting, by weight, essentially of: 
 from 0.8% to 3% of iron;    from 0.3% to 2% of nickel;    from 0.6% to 1.4% of tin;    from 0.005% to 0.35% of phosphorous; and    the balance copper and inevitable impurities.    
     
     
         2 . The copper alloy of  claim 1  wherein said iron is present in an amount of from 1% to 2%.  
     
     
         3 . The copper alloy of  claim 2  wherein said iron is present in an amount of from 1% to 1.5%.  
     
     
         4 . The copper alloy of  claim 2  wherein said nickel is present in an amount of from 0.5% to 1.3%.  
     
     
         5 . The copper alloy of  claim 4  wherein said nickel is present in an amount of from 0.5% to 1%.  
     
     
         6 . The copper alloy of  claim 4  wherein said tin is present in an amount of from 0.7% to 1.1%.  
     
     
         7 . The copper alloy of  claim 6  wherein said tin is present in an amount of from 0.8% to 1%.  
     
     
         8 . The copper alloy of  claim 6  wherein said phosphorous is present in an amount of from 0.01% to 0.1%.  
     
     
         9 . The copper alloy of  claim 8  being formed into an electrical connector.  
     
     
         10 . A copper alloy consisting, by weight, essentially of: 
 from 1% to 1.5% of iron;    from 0.5% to 1% of nickel;    from 0.8% to 1% of tin;    from 0.01% to 0.1% of phosphorous; and    the balance copper and inevitable impurities, said alloy having a yield strength of 70 ksi or higher, an electrical conductivity in excess of 40% IACS and sufficient resistance to stress relaxation that over 75% of an imposed stress remains when exposed to temperatures of up to 150° C. for up to 3000 hours.    
     
     
         11 . The copper alloy of  claim 19  formed into an electrical connector.  
     
     
         12 . A method for the manufacture of a copper alloy having an electrical conductivity in excess of 40% IACS and sufficient resistance to stress relaxation that over 75% of an imposed stress remains when exposed to temperatures of up to 150° C. for up to 3000 hours, comprising the steps of: 
 (a) casting a copper base alloy containing, by weight, 0.8% to 3% of iron, 0.3% to 2% of nickel, 0.6% to 1.4% of tin, 0.005% to 0.35% of phosphorous and the balance copper and inevitable impurities;  
 (b) hot working said copper alloy at a temperature in excess of 700° C. thereby forming a slab:  
 (c) cold working said slab to a first desired thickness thereby forming a strip;  
 (d) annealing said strip at a temperature of between 500° C. and 650° C. for from 2 hours to 6 hours;  
 (e) cold working said strip to an intermediate thickness;  
 (f) annealing said strip at a temperature of between 450° C. and 600° C. for from one to six ours;  
 (g) cold working said strip to a desired final gauge; and  
 (f) relief annealing said strip at final gauge at a temperature of between 200° C. and 350° C. for from thirty minutes to six hours.  
 
     
     
         13 . The method of  claim 12  wherein said hot working occurs at a temperature of between 750° C. and 950°.  
     
     
         14 . The method of  claim 13  including the additional stirp of removing surface oxides from said slab following hot working.  
     
     
         15 . The method of  claim 14  wherein said intermediate thickness is selected so that said strip has a yield strength of 70 ksi or higher following said relief anneal step (f).  
     
     
         16 . The method of  claim 15  wherein said relief anneal is at a temperature of between 250° C. and 325° C. for a time of from one to three hours.  
     
     
         17 . The method of  claim 16  including forming said copper alloy at desired final gauge into an electrical connector.  
     
     
         18 . The method of  claim 14  wherein said intermediate thickness is selected so that said strip has a yield strength of 75 ksi or higher following said relief anneal step (f).  
     
     
         19 . The method of  claim 18  wherein said relief anneal is at a temperature of between 250° C. and 325° C. for a time of from one to three hours.  
     
     
         20 . The method of  claim 19  including forming said copper alloy at desired final gauge into an electrical connector.

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