Principal Design Features
A nickel-chromium-cobalt alloy similar to Udimet 500 but with greater aluminum and titanium content for age-hardening heat treatment.
Gas turbine hot section components.
Conventional machining techniques used for iron based alloys may be used. This alloy does work-harden during machining and has higher strength and “gumminess” not typical of steels. Heavy duty machining equipment and tooling should be used to minimize chatter or work-hardening of the alloy ahead of the cutting.
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