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>BSI Standards >49 AIRCRAFT AND SPACE VEHICLE ENGINEERING>49.025 Materials for aerospace construction>49.025.99 Other materials>BS 2HR 3:2010 Specification for nickel-cobalt-chromium-molybdenum-aluminium-titanium heat-resisting alloy billets, bars, forgings and parts (nickel base, Co 20, Cr 14.8, Mo 5, Al 4.8, Ti 1.2)
immediate downloadReleased: 2010-01-31
BS 2HR 3:2010 Specification for nickel-cobalt-chromium-molybdenum-aluminium-titanium heat-resisting alloy billets, bars, forgings and parts (nickel base, Co 20, Cr 14.8, Mo 5, Al 4.8, Ti 1.2)

BS 2HR 3:2010

Specification for nickel-cobalt-chromium-molybdenum-aluminium-titanium heat-resisting alloy billets, bars, forgings and parts (nickel base, Co 20, Cr 14.8, Mo 5, Al 4.8, Ti 1.2)

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Standard number:BS 2HR 3:2010
Pages:16
Released:2010-01-31
ISBN:978 0 580 67041 1
Status:Standard
DESCRIPTION

BS 2HR 3:2010


This standard BS 2HR 3:2010 Specification for nickel-cobalt-chromium-molybdenum-aluminium-titanium heat-resisting alloy billets, bars, forgings and parts (nickel base, Co 20, Cr 14.8, Mo 5, Al 4.8, Ti 1.2) is classified in these ICS categories:
  • 49.025.99 Other materials

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

  1. Bars and extruded sections for machining: solution treated, designation HR 3A.

  2. Extruded sections for subsequent forming: softened, designation HR 3B.

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

  4. Forgings: solution treated, designation HR 3D.


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