US2002189729A1PendingUtilityA1

Copper, copper alloy, and manufacturing method therefor

Assignee: NIPPON MINING COPriority: Mar 27, 2001Filed: Mar 26, 2002Published: Dec 19, 2002
Est. expiryMar 27, 2021(expired)· nominal 20-yr term from priority
B21B 3/00C22C 9/00C22F 1/08B21B 2003/005
39
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Claims

Abstract

Copper and copper alloy comprises: a structure having fine crystal grains with grain size of 1 μm or less after a final cold rolling with a reduction η, wherein η is expressed in the following formula and satisfying η≧3; and an elongation of 2% or more in a tensile test. η=ln( T 0 /T 1 ) T 0 : plate thickness before rolling, T 1 : plate thickness after rolling.

Claims

exact text as granted — not AI-modified
What is claimed is:  
     
         1 . Copper and copper alloy comprising: 
 a structure having fine crystal grains with grain size of 1 μm or less composed of crystal grain boundaries mainly formed of curved portions after a final cold rolling, the structure obtained by dynamic continuous recrystallization caused by the final cold rolling, and    an elongation of 2% or more in a tensile test.    
     
     
         2 . Copper and copper alloy comprising: 
 a structure having fine crystal grains with grain size of 1 μm or less after a final cold rolling with a reduction η, wherein η is expressed in the following formula and satisfying η≧3; and    an elongation of 2% or more in a tensile test.   η=ln( T   0   /T   1 )   T 0 : plate thickness before rolling, T 1 : plate thickness after rolling.    
     
     
         3 . A manufacturing method for copper and copper alloy, the method comprising: 
 a final cold rolling with a reduction η, wherein η is expressed in the following formula and satisfying η≧3,    thereby obtaining a structure having fine crystal grains with grain size of 1 μm or less after the final cold rolling, and    an elongation of 2% or more in a tensile test.   η=ln( T   0   /T   1 )   T 0 : plate thickness before rolling, T 1 : plate thickness after rolling.    
     
     
         4 . A manufacturing method for copper and copper alloy according to  claim 3 , wherein the copper and copper alloy recited in  claim 1  is processed by stress relief annealing, and elongation by a tensile test is improved to 6% or more.  
     
     
         5 . A manufacturing method for copper and copper alloy according to  claim 3 , wherein the copper and copper alloy recited in  claim 2  is processed by stress relief annealing, and elongation by a tensile test is improved to 6% or more.  
     
     
         6 . Copper and copper alloy manufactured by the manufacturing method of  claim 4 .  
     
     
         7 . Copper and copper alloy manufactured by the manufacturing method of  claim 5 .  
     
     
         8 . A manufacturing method of copper and copper alloy according to  claim 3 , wherein the copper alloy is Cu—Ni—Si alloy or Cu—Cr—Zr alloy.  
     
     
         9 . A manufacturing method of copper and copper alloy according to  claim 4 , wherein the copper alloy is Cu—Ni—Si alloy or Cu—Cr—Zr alloy.  
     
     
         10 . A manufacturing method of copper and copper alloy according to  claim 5 , wherein the copper alloy is Cu—Ni—Si alloy or Cu—Cr—Zr alloy.  
     
     
         11 . Copper and copper alloy of  claim 6 , wherein the copper alloy is Cu—Ni—Si alloy or Cu—Cr—Zr alloy.  
     
     
         12 . Copper and copper alloy of  claim 7 , wherein the copper alloy is Cu—Ni—Si alloy or Cu—Cr—Zr alloy.

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