US2002189729A1PendingUtilityA1
Copper, copper alloy, and manufacturing method therefor
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-modifiedWhat 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.Join the waitlist — get patent alerts
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