FAMILY | ALLOY | DESCRIPTION |
---|---|---|
Nickel-Aluminum Bronze | C63000 |
C63000 NICKEL ALUMINUM BRONZE C63000 Aluminum Bronze is a high strength copper aluminum alloy, containing 81% copper, 10% aluminum, 5% nickel, 4% iron, and an excellent choice for applications involving heavy loads, abrasive wear resistant, friction, abrasive wear and corrosion. The addition of nickel increases the alloys strength without diminishing its excellent ductility, toughness and corrosion resistance. |
C95500 |
C95500 Nickel Aluminum BronzeOne of the toughest non-ferrous alloys known. Characterized as a high tensile, nickel bearing aluminum bronze, with exceptional yield, compressive strength, high hardness, and fairly high elongation. Exhibits good shock and high stress qualities. Excellent bearing material suitable for heavy duty, high shock, and high impact applications. Has good resistance to sea water corrosion, heat resistance, good machinability, and weldability. Can be heat treated. |
|
C95500HT |
C95500HT Nickel Aluminum BronzeC95500 Nickel Aluminum Bronze is the toughest non-ferrous alloys known. The additional heat treating process further strengthens the mechanical properties of this alloy making it a perfect fit for heavy duty applications. C95500HT is available from Dura-Bar Metal Services in solids, tubes and rectangles. |
|
C95510HT |
C95510HT Nickel Aluminum BronzeOne of the more popular landing gear bushing materials specified today along with C63000 material. The continuous cast alloy is heat treated and exhibits high mechanical strength which meets the properties of C63000. |
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C95800 |
C95800 Nickel Aluminum BronzeC95800 Nickel Aluminum Bronze is used to produce nuts, worm wheels, bushings, propeller blades, wear plates and gears. C95800 is available from Dura-Bar Metal Services in solids, tubes and rectangles. |
Chemical Composition (according to ASTM B505/B505M-14)
Alloy | Cu% | Fe% | Ni%1 | Al% | Mn% | ||||||
---|---|---|---|---|---|---|---|---|---|---|---|
1Ni value includes Co. Note: Cu + Sum of Named Elements, 99.5% min. Single values, unless otherwise noted, represent maximums. |
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C95500 | 78.00 MIN | 3.00- 5.00 |
3.00- 5.50 |
10.00- 11.50 |
3.50 |
Tensile Strength(min) | Yield Strength(at .5% extention under load min) | Elongation(in 2in. or 50mm min, %) | Brinell Hardness(min) | Remarks | ||
---|---|---|---|---|---|---|
Ksi | MPa | Ksi | MPa | |||
95 | 655 | 42 | 290 | 10 | N/A |
Similar or Equivalent Specification
CDA | ASTM | ASARCON | SAE | AMS | Federal | Military | Other |
---|---|---|---|---|---|---|---|
C95800 | B505 | QQ-C-390, G8 | APHA NICKEL ALUMINUM BRONZE |
Alloy | Cu% | Pb% | Fe%1 | Ni%2 | Al% | Mn% | Si% | ||||
---|---|---|---|---|---|---|---|---|---|---|---|
1Fe content shall not exceed Ni content. 2Ni value includes Co. Note: Cu + Sum of Named Elements, 99.5% min. Single values, unless otherwise noted, represent maximums. |
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C95800 | 79.00 MIN | 0.03 | 3.50- 4.50 |
4.00- 5.00 |
8.50- 9.50 |
0.80- 1.50 |
0.10 |
Tensile Strength(min) | Yield Strength(at .5% extention under load min) | Elongation(in 2in. or 50mm min, %) | Brinell Hardness(min) | Remarks | ||
---|---|---|---|---|---|---|
Ksi | MPa | Ksi | MPa | |||
85 | 586 | 35 | 241 | 18 | N/A |
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