The addition of nickel to copper improves the alloy's strength and durability. The mechanical properties of copper-nickel alloys show a combination of good tensile strength and excellent ductility when annealed. As solid solution alloys, the 90-10 and 70-30 alloys cannot be age hardened. Higher tensile strength and hardness can only be obtained when the alloys are cold worked. Whereas 90-10 Cu-Ni tubing can have a proof strength of 100-160 N/mm2 when supplied in the annealed condition, this could typically be 345-485 N/mm2 in the as-drawn condition.
Both age hardened Cu-Ni-Al and spinodally strengthened Cu-Ni-Sn alloy systems are able to achieve high strengths matching that of carbon steel.
Typical annealed mechanical properties for copper-nickel alloys are given in Table 1. Minimum mechanical properties for 90-10 Cu-Ni (CW 352H) based on Euronorm Standards are outlined in Table 2. Minimum mechanical properties for 90-10 Cu-Ni (C70600) based on ASTM Standards are outlined in Table 3. Minimum mechanical properties for 70-30 Cu-Ni (CW 354H) based on Euronorm Standards are outlined in Table 4. Minimum mechanical properties for 70-30 Cu-Ni (C71500) based on ASTM Standards are outlined in Table 5.
Note: The following data is for guidance only. Please check values for current design specifications.
Alloy | EN No or Other Identification | UNS No | 0.2% Proof Strength N/mm2 | Tensile Strength N/mm2 | Elongation % | Hardness HV |
---|---|---|---|---|---|---|
Cu-Ni |
CW352H CW353H (tube only) CW354H |
C70600 C71640 C71500 |
100-350 150min 130-450 |
290-420 420min 350-520 |
12-40 30min 12-35 |
80-160 110 90-190 |
Cu-Ni-Cr |
Def Stan 02-824 Part 1 - |
- C72200 |
300 min 110 min |
480 min 310 min |
18 min |
|
Cu-Ni-Al |
Cu-15Ni-3Al
|
-
|
555-630
|
770-850
|
12min
|
229-240
|
Cu-Ni-Sn |
Cu-15Cr-8Sn |
C72900 |
620-1030 |
825-1100 |
2-15 |
272-354 |
Source: Copper Alloys for Marine Environments; CDA Publication No. 206; Dec. 2012; Table 10 |
Form | Condition | Thickness t* | Tensile Strength | 0.2%Proof Strength | Elongation | Hardness |
---|---|---|---|---|---|---|
mm | N/mm2 | N/mm2 | % | HV | ||
Tubes EN 12449: 1999 |
R290 | 20max | 290 | 90 | 30 | - |
H075 | 20 max | - | - | - | 75-110 | |
R310 | 6 max | 310 | 220 | 12 | - | |
H105 | 6 max | - | - | - | 105 | |
R480 | 4 max | 480 | 400 | 8 | ||
H150 | 4 max | - | - | - | 150 | |
Sheet/Plate EN 1652: 1997 |
R300 | 0.3-15 | 300 | (100) | 20 for t<and=2.5
30 for t>2.5mm |
- |
H070 | 0.3-15 | - | - | - | 70-120 | |
R320 | 0.3-15 | 320 | (200) | 15 for >2.5mm t | ||
H100 | 0.3-15 | - | - | - | 100 | |
Plate for pressure vessels, heat exchangers EN 1653: (1997) |
R270 | 2.5-125 | 270 | 100 | 30 | (85) |
R280 | over10 | 280 | 110 | 20 | (85) | |
R300 | 2.5-10 | 300 | 120 | 25 | (90) | |
R320 | 2.5-60 | 320 | 200 | 15 | (110) | |
R350 | 10-40 | 350 | 250 | 14 | (120) | |
Figures in parentheses are not requirements but are given for information only. |
Form | Temper | Tensile Strength | Yield Strength | Elongation in 50mm | Hardness | |
---|---|---|---|---|---|---|
Standard | Former | MPa (N/mm2) | MPa (N/mm2) | % | Rockwell B | |
Seamless Condenser Tubes B111M-98 | O61 | Annealed | 275 | 105 | - | - |
H55 | Light drawn | 310 | 240 | - | - | |
Plate Sheet Strip and Rolled Bar B122/122M-95 | M20 | As hot rolled | 275-425 | - | - | - |
H01 | Quarter hard | 350-460 | - | - | 51-78 | |
H02 | Half hard | 400-495 | - | - | 66-81 | |
H04 | Hard | 490-570 | - | - | 76-86 | |
H06 | Extra Hard | 505-585 | - | - | 80-88 | |
H08 | Spring | 540-605 | - | - | 83-91 | |
Plate and sheet for pressure vessels, condensers and heat exchangers B171M-96 | M20 and 025 | (80mm and under) | 275 | 105 | 30 | |
(>60 to 140mm) | 275 | 105 | 30 | |||
1N/mm2 is equivalent to 1MPa |
Form | Condition | Thickness t* | Tensile Strength | 0.2% Proof Strength | Elongation | Hardness |
---|---|---|---|---|---|---|
mm | N/mm2 | N/mm2 | % | HV | ||
Tube EN 12449: 1999 |
R370 | 10 max | 370 | 120 | 35 | - |
H085 | 10 max | - | - | - | 85-120 | |
R480 | 5 max | 480 | 300 | 12 | - | |
H135 | 5 max | - | - | - | 135 | |
Sheet/plate EN 1652: 1997 |
R350 | 0.3-15 | 350-420 | (120) | 35 for t>2.5mm | - |
H080 | 0.3-15 | - | - | - | 80-120 | |
R410 | 0.3-15 | 410 | (300) | 14 for t>2.5mm | - | |
H110 | 0.3-15 | - | - | - | 110 | |
Heavy PlateFor pressure vessels EN 1653:1997 |
R320 | 2.5-125 | 320 | 120 | 30 | (100) |
R410 | 10-40 | 410 | 300 | 14 | (140) | |
Figures in parentheses are not requirements but are given for information only. |
Form | >Temper | Tensile Strength | Yield Strength | Elongation in 50mm | Hardness | |
---|---|---|---|---|---|---|
Standard | Former | MPa (N/mm2) | MPa (N/mm2) | % | Rockwell B | |
Seamless Condenser Tubes B111M-98 | O61 | Annealed | 360 | 125 | - | - |
HR50 ( up to 1.21mm wall) | Drawn, stress relieved | 495 | 345 | 12 | - | |
HR50 ( over 1.21mm wall) | Drawn, stress relieved | 495 | 345 | 15 | ||
Plate Sheet Strip and Rolled Bar B122/122M-95 | M20 | As hot rolled | 310-450 | - | - | - |
H01 | Quarter hard | 400-495 | - | - | 67-81 | |
H02 | Half hard | 455-550 | - | - | 76-85 | |
H04 | Hard | 515-605 | - | - | 83-89 | |
H06 | Extra Hard | 550-635 | - | - | 85-91 | |
H08 | Spring | 580-650 | - | - | 87-91 | |
Plate and sheet for pressure vessels, condensers and heat exchangers B171M-96 | M20 and 025 | (80mm and under) | 345 | 140 | 30 | |
(>60 to 140mm) | 310 | 125 | 30 | |||
1N/mm2 is equivalent to 1MPa |
References
- 90/10 and 70/30 Alloys Technical Data, Publication TN 31, , CDA UK, .
- Copper-Nickel Alloys: Properties, Processing, Application, Booklet, German Copper Institute (DKI), English translation .
- Cryogenic Properties, .
- Fatigue of Thin-Walled Tubes in Copper Alloy CuNi10, Ships and Offshore Structures, Søren Heide Lambertsen, Lars Damkilde & Michael S. Jepsen, Ships and Offshore Structures, Vol. 11, 1, pp 1-6, , DOI: 10.1080/17445302.2014.992609, .
- High Strength Copper-Nickels, Tuck, C.D.S., , UK, Langley Alloys, .
- Mechanical Properties of Copper and Copper Alloys at Low Temperatures, Application Data Sheet 144/8 R, CDA, .
- Performance Advances in Copper-Nickel-Tin Spinodal Alloys, W. Raymond Cribb, Michael J. Gedeon, and Fritz C. Grensing, Advanced Materials and Processes, Vol. 171, 9, , ASM, .
- Properties and Uses of Copper Alloys, .
- The Development of Very High Strength Copper Alloys with Resistance to Hydrogen Embrittlement and Stress Corrosion Cracking, C.D.S. Tuck, , Corrosion/2005 Annual Conference and Exhibition, Houston, ©NACE, .