Copper-nickel-tin alloy with high toughness

Patent metadata

Field	Value
Publication number	US-10858723-B2
Application number	US-201916257446-A
Country	US
Kind code	B2
Filing date	Jan 25, 2019
Priority date	Apr 23, 2013
Publication date	Dec 8, 2020
Grant date	Dec 8, 2020

Abstract

A spinodal copper-nickel-tin alloy with a combination of improved impact strength, yield strength, and ductility is disclosed. The alloy is formed by process treatment steps including solution annealing, cold working and spinodal hardening. These include such processes as a first heat treatment/homogenization step followed by hot working, solution annealing, cold working, and a second heat treatment/spinodally hardening step. The spinodal alloys so produced are useful for applications demanding enhanced strength and ductility such as for pipes and tubes used in the oil and gas industry.

First claim

The invention claimed is:

1. A spinodal copper-nickel-tin alloy having a 0.2% offset yield strength of at least 110 ksi, an impact toughness of at least 12 foot-pounds when measured according to ASTM E23, V notch at room temperature, and an ultimate tensile strength of at least 120 ksi, and a minimum elongation of 20%.

2. The spinodal copper-nickel-tin alloy of claim 1 , wherein the alloy comprises from about 5 wt % to about 20 wt % nickel, from about 5 wt % to about 10 wt % tin, and the remainder copper.

3. The spinodal copper-nickel-tin alloy of claim 1 , wherein the alloy comprises from about 14 wt % to about 16 wt % nickel, from about 7 wt % to about 9 wt % tin, and the remainder copper.

4. The spinodal copper-nickel-tin alloy of claim 1 , having an impact toughness of at least 30 foot-pounds and up to about 100 foot-pounds, when measured according to ASTM E23, V notch at room temperature.

5. The spinodal copper-nickel-tin alloy of claim 1 , having a magnetic permeability of less than 1.02.

6. The spinodal copper-nickel-tin alloy of claim 1 , further comprising a minor addition of not more than about 0.3 wt % of at least one element selected from the group consisting of zirconium, iron, and magnesium.

7. A spinodal copper-nickel-tin alloy produced by a process comprising:
casting a copper-nickel-tin alloy;
homogenizing the alloy;
hot working the homogenized alloy to obtain a reduction ratio which is a minimum of about 5:1;
solution annealing the hot worked alloy at a temperature of from about 1470° F. to about 1650° F.;
cold working the solution annealed alloy until a reduction of area of from about 15% to about 80% occurs in the alloy; and
spinodally hardening the alloy after the cold working to produce the spinodal alloy;
wherein the spinodal alloy has a 0.2% offset yield strength of at least 110 ksi, an impact toughness of at least 12 foot-pounds when measured according to ASTM E23, V notch at room temperature, and an ultimate tensile strength of at least 120 ksi, and a minimum elongation of 20%.

8. The method of claim 7 , wherein the copper-nickel-tin alloy comprises from about 14 wt % to about 16 wt % nickel, from about 7 wt % to about 9 wt % tin, and the balance copper.

9. The method of claim 7 , wherein the homogenizing occurs at a temperature of about 1400° F. or higher, or at a temperature from about 1475° F. to about 1650° F.

10. The method of claim 7 , wherein the homogenizing occurs for a time of from about 4 hours to about 48 hours.

11. The method of claim 7 , wherein the hot working occurs at a temperature of from about 1300° F. to about 1650° F.

12. The method of claim 7 , wherein the reheat for hot working occurs for a time of at least 6 hours.

13. The method of claim 7 , wherein the solution annealing occurs for a time of from about 0.5 hours to about 6 hours.

14. The method of claim 7 , further comprising a quenching after the solution annealing.

15. The method of claim 14 , wherein the quenching occurs within 2 minutes of completion of the solution annealing.

16. The method of claim 7 , wherein the cold working occurs at room temperature.

17. The method of claim 7 , wherein the steps of cold working or solution annealing are repeated until a desired size is obtained.

18. The method of claim 7 , wherein the spinodal hardening occurs at a temperature of from about 400° F. to about 1000° F., or at a temperature of from about 450° F. to about 725° F., or at a temperature of from about 500° F. to about 675° F.

19. The method of claim 7 , wherein the spinodal hardening occurs for a time of from about 10 seconds to about 40,000 seconds, for a time of from about 5,000 seconds to about 10,000 seconds, or for a time of from about 0.5 hours to about 8 hours.

20. A spinodal copper-nickel-tin alloy produced by a method comprising:
solution annealing a copper-nickel-tin alloy wherein the solution annealing occurs at a temperature of from about 1475° F. to about 1650° F. and for a time of from about 0.5 hours to about 6 hours;
cold working the solution annealed alloy, wherein the cold working results in a reduction of area in the alloy of from about 15% to about 80%; and
spinodally hardening the alloy after cold working, wherein the spinodal hardening occurs at a temperature of from about 500° F. to about 675° F. and for a time of from about 0.5 hours to about 8 hours.

Assignees

• Materion Corp

Inventors

• Cribb W Raymond
• Finkbeiner Chad A
• Grensing Fritz C

Classifications

• C22C9/06 Primary

  with nickel or cobalt as the next major constituent · CPC title

• C22C9/02

  with tin as the next major constituent · CPC title

• C22F1/08 Primary

  of copper or alloys based thereon · CPC title