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Other
Alloy:
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| Alloy
A-286
: Nickel-iron-chromium alloy with good strength and
oxidation resistance at temperatures up to about 1300`F (705`C).
Gas-turbine components including blades, vanes, shaft, tail,
cones, afterburners, springs, fasteners. |
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Nimonic Alloy 75: An
80-20 nickel-chromium alloy with controlled additions of titanium
and carbon, aircraft gas-turbine components needing resistance
to oxidation and scaling combined with medium strength at high
temperature. |
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