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Processing for improved stress relaxation resistance in copper alloys exhibiting spinodal decomposition

Assignee: Olin Corp
•
Filing: 1976-11-19
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Granted: 1978-02-14
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Expires: 1996-11-19
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Abstract

Abstract A process for providing copper base alloys with a combination of high strength and high strength to ductility characteristics is disclosed. The alloys should be those copper alloys which exhibit continuous, homogeneous precipitation of coherent particles such as spinodal decomposition upon precipitation hardening. The alloys are hot worked, solution annealed and subjected to a controlled cooling to provide the desirable strength-ductility combinations.

Inventors

  • 👤 Ronald N. Caron
  • 👤 Stanley Shapiro

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-26 17:04
CPC Classifications
C; C22; C22F; C22F1/00; C22F1/08

Claims Analysis

Total Claims: 19
Claim 1
Independent Claim 144 words
A method for obtaining precipitation hardened copper base alloys via continuous, coherent precipitation such as spinodal decomposition having high strength and favorable strength to ductility characteristics which comprises: a. providing a copper base alloy selected from the group consisting of those Cu-Ti alloys, Cu-Be alloys and Cu-Ni base alloys which exhibit continuous, homogeneous precipitation of coherent particles upon precipitation hardening; b. hot working said alloy with a finishing temperature in excess of 400° C; c. solution annealing said alloy for from 10 seconds to 24 hours at a temperature of from 650° to 1100° C; and d. cooling the alloy to room temperature at a rate of less than 650° C per minute to provide a spinodal, precipitation hardened copper base alloy wherein the microstructure is characterized by the presence of finely dispersed precipitates of alloying element-rich particles dispersed throughout the copper alloy matrix.
Claim 2
Independent Claim 144 words
A method for obtaining precipitation hardened copper base alloys via continuous, coherent precipitation such as spinodal decomposition having high strength and favorable strength to ductility characteristics which comprises: a. providing a copper base alloy selected from the group consisting of those Cu-Ti alloys, Cu-Be alloys and Cu-Ni base alloys which exhibit continuous, homogeneous precipitation of coherent particles upon precipitation hardening; b. hot working said alloy with a finishing temperature in excess of 400° C; c. solution annealing said alloy for from 10 seconds to 24 hours at a temperature of from 650° to 1100° C; and d. cooling the alloy to room temperature at a rate of less than 650° C per minute to provide a spinodal, precipitation hardened copper base alloy wherein the microstructure is characterized by the presence of finely dispersed precipitates of alloying element-rich particles dispersed throughout the copper alloy matrix.
Claim 3
Dependent Claim 71 words
A method according to claim 1 wherein said alloy includes a total of up to 20% of a material selected from the group consisting of from 0.01 to 10% zinc, from 0.01 to 10% iron, from 0.01 to 10% tin, from 0.01 to 5% each of zirconium, beryllium, vanadium, niobium, tantalum, chromium, molybdenum, tungsten and mixtures thereof, and wherein the resultant microstructure is characterized by the presence of second precipitate particles.
Claim 4
Dependent Claim 54 words
A method according to claim 1 wherein said alloy includes a total of up to 5% of a material selected from the group consisting of lead, arsenic, antimony, boron, phosphorus, manganese, silicon, a lanthanide metal, magnesium, lithium and mixtures thereof, with each of said materials being present in an amount from 0.001 to 3%.
Claim 5
Dependent Claim 33 words
A method according to claim 1 wherein said alloy is homogenized prior to hot working at a temperature between 600° C and the solidus temperature of the alloy for at least 15 minutes.
Claim 6
Dependent Claim 19 words
A method according to claim 1 wherein said alloy is cold worked following hot working but before solution annealing.
Claim 7
Dependent Claim 12 words
A method according to claim 5 wherein all working steps are rolling.
Claim 8
Dependent Claim 34 words
A method according to claim 6 wherein said alloy is cold rolled with intermediate annealing at from 250° C to within 50° C of the solidus temperature for from 10 seconds to 24 hours.
Claim 9
Dependent Claim 24 words
A method according to claim 1 wherein said alloy is cooled at a rate between 0.5° C per minute and 650° C per minute.
Claim 10
Dependent Claim 29 words
A method according to claim 8 wherein the alloy is aged following cooling at a temperature of from 250° to 650° C for from 30 minutes to 24 hours.
Claim 11
Dependent Claim 16 words
A method according to claim 9 wherein the alloy is cold rolled and aged following cooling.
Claim 12
Dependent Claim 24 words
A method according to claim 1 wherein said alloy is a Cu-Ti alloy consisting essentially of 0.5 to 4.7% by weight Ti, balance Cu.
Claim 13
Dependent Claim 24 words
A method according to claim 1 wherein said alloy is a Cu-Be alloy consisting essentially of 0.2 to 2.7% by weight Be, balance Cu.
Claim 14
Dependent Claim 30 words
A method according to claim 1 wherein said alloy is a Cu-Ni-Al alloy consisting essentially of 5 to 30% by weight Ni, 0.5 to 5% by weight Al, balance Cu.
Claim 15
Dependent Claim 30 words
A method according to claim 1 wherein said alloy is a Cu-Ni-Si alloy consisting essentially of 0.5 to 15% by weight Ni, 0.5 to 3% by weight Si, balance Cu.
Claim 16
Dependent Claim 30 words
A method according to claim 1 wherein said alloy is a Cu-Ni-Sn alloy consisting essentially of 3 to 30% by weight Ni, 2 to 15% by weight Sn, balance Cu.
Claim 17
Dependent Claim 18 words
A method according to claim 7 wherein said alloy is cold rolled at a temperature below 200° C.
Claim 18
Dependent Claim 20 words
A method according to claim 1 wherein said solution annealing is at a temperature of from 800° to 1100° C.
Claim 19
Dependent Claim 31 words
A method according to claim 9 wherein said alloy is formed into parts and subjected to a low temperature thermal treatment at 150° to 300° C for at least 15 minutes.

References Cited (Backward Citations)

US2783143A Cited
US2943960A Cited
US3258334A Cited
US3663311A Cited
US4012240A Cited
US4016010A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1981-02-13 1981-08-15 1982-02-14 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1985-02-13 1985-08-15 1986-02-14 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1989-02-13 1989-08-15 1990-02-14 $7700.00 Window Closed / Lapsed

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