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Homepage>BS Standards>49 AIRCRAFT AND SPACE VEHICLE ENGINEERING>49.025 Materials for aerospace construction>49.025.99 Other materials>BS 3HR 2:2010+A2:2012 Specification for nickel-chromium-cobalt-titanium-aluminiumheat-resistin g alloy billets, bars, forgings and parts (Nickel base, Cr19.5, Co 18.0 , Ti 2.5, Al 1.5)
immediate downloadReleased: 2012-07-31
BS 3HR 2:2010+A2:2012 Specification for nickel-chromium-cobalt-titanium-aluminiumheat-resistin g alloy billets, bars, forgings and parts (Nickel base, Cr19.5, Co 18.0 , Ti 2.5, Al 1.5)

BS 3HR 2:2010+A2:2012

Specification for nickel-chromium-cobalt-titanium-aluminiumheat-resistin g alloy billets, bars, forgings and parts (Nickel base, Cr19.5, Co 18.0 , Ti 2.5, Al 1.5)

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Standard number:BS 3HR 2:2010+A2:2012
Pages:20
Released:2012-07-31
ISBN:978 0 580 78018 9
Status:Standard
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BS 3HR 2:2010+A2:2012


This standard BS 3HR 2:2010+A2:2012 Specification for nickel-chromium-cobalt-titanium-aluminiumheat-resistin g alloy billets, bars, forgings and parts (Nickel base, Cr19.5, Co 18.0 , Ti 2.5, Al 1.5) is classified in these ICS categories:
  • 49.025.99 Other materials

This British Standard specifies requirements for nickel-chromium-cobalt-titanium-aluminium heat-resisting alloy supplied in the following forms, and as parts.

  1. Bars and extruded sections for machining: solution treated, designation HR 2A.

  2. Extruded sections for subsequent forming: softened, designation HR 2B.

  3. Billets and bars for forging: hot or cold worked and subsequently machined or ground, designation HR 2C.

  4. Forgings: solution treated, designation HR 2D.