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This C95510 Aluminum nickel bronze alloy that combines high strength, ductility and good abrasion resistance under severe loading conditions. Higher and more consistent mechanical properties – higher yield strength and ductility minimums on product over 1.0 in and typical mechanical property values of 20 – 30% above specification minimums. It has improved service life – enhanced corrosion resistance and fatigue life due to the alloy dispersion and refined, “wrought-like” microstructure. C95510 is commonly used in demanding aerospace applications, including bushings, spherical and rod end bearings, rub pads, and wear strips. This material is also used for applications in the oil and gas industry.
| Weight % | Al | Fe | Mn | Ni | Sn | Cu | Zn |
|---|---|---|---|---|---|---|---|
| Minimum | 9.70 | 2.00 | — | 4.50 | — | 78.10 | — |
| Maximum | 10.90 | 3.50 | 1.5 | 5.50 | 0.20 | 83.80 | 0.30 |
| Characteristics | English | Metric | |
|---|---|---|---|
| Nominal density (68°F/20°C) | 0.272 lbs/in3 | 7.53 g/cm3 | |
| Melting range | 1900°F-1930°F | 1040°C-1050°C | |
| Specific heat | 70°F / 20°C | 0.09 BTU/lb – °F | 375 J/KG- °K |
| Coefficient of thermal
expansion |
Linear
68°F – 572°F 20°C – 300°C |
9.00 micro in/in- °F | 16.2 micro in/in- °K |
| Thermal Conductivity | 68°F / 20°C | 24 BTU/ft- hr – °F | 42 W/m – °K |
| Wall thickness | Tensile | ||||
|---|---|---|---|---|---|
| Ultimate | Yield | Elongation at break | |||
| KSI | MPa | KSI | MPa | % | |
| 0.25” – 1.0”
(6.35 – 25.4 mm) |
105 | 724 | 62.5 | 431 | 9 |
| 1.0” – 17.0”
(25.4 – 431.8 mm) |
95 | 655 | 50 | 345 | 8 |
| 1.0” – 4.0”
(25.4 – 101.6 mm) |
105 | 724 | 62.5 | 431 | 9 |
| 4.0” – 17.0”
(101.6 – 431.8 mm) |
95 | 655 | 56 | 386 | 9 |
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