Principal Design Features
A nickel-chromium-cobalt alloy that is age-hardenable for high temperature strength.
Gas turbine hot section components or similar applications for industrial use.
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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