Specification for nickel-cobalt-chromium-molybdenum-titanium-aluminium heat-resisting alloy billets, bars, forgings and parts (nickel base, Co 20, Cr 20, Mo 5.9, Ti 2.1, Al 0.5) Ingestion-build-242630 Technical requirements for aeronautical ground

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Specification for nickel-cobalt-chromium-molybdenum-titanium-aluminium heat-resisting alloy billets, bars, forgings and parts (nickel base, Co 20, Cr 20, Mo 5.9, Ti 2.1, Al 0.5) Ingestion-build-242630 Technical requirements for aeronautical ground1 Scope This British Standard specifies requirements for nickel cobalt chromium molybdenum titanium aluminium heat resisting alloy supplied in the following forms, and as parts. a) Bars and extruded sections for machining: solution treated, designation HR 10A. b) Extruded sections for subsequent forming: solution treated, designation HR 10B. c) Billets and bars for forging: hot or cold worked and subsequently machined or ground, designation HR 10C. d)