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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 2HR 4:2010 Specification for nickel-chromium-cobalt-aluminium-molybdenum-titanium heat-resisting alloy billets, bars, forgings and parts (nickel base, Cr 15, Co 14.2, Al 5, Mo 4, Ti 4)
immediate downloadReleased: 2010-01-31
BS 2HR 4:2010 Specification for nickel-chromium-cobalt-aluminium-molybdenum-titanium heat-resisting alloy billets, bars, forgings and parts (nickel base, Cr 15, Co 14.2, Al 5, Mo 4, Ti 4)

BS 2HR 4:2010

Specification for nickel-chromium-cobalt-aluminium-molybdenum-titanium heat-resisting alloy billets, bars, forgings and parts (nickel base, Cr 15, Co 14.2, Al 5, Mo 4, Ti 4)

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Standard number:BS 2HR 4:2010
Pages:14
Released:2010-01-31
ISBN:978 0 580 67042 8
Status:Standard
DESCRIPTION

BS 2HR 4:2010


This standard BS 2HR 4:2010 Specification for nickel-chromium-cobalt-aluminium-molybdenum-titanium heat-resisting alloy billets, bars, forgings and parts (nickel base, Cr 15, Co 14.2, Al 5, Mo 4, Ti 4) is classified in these ICS categories:
  • 49.025.99 Other materials

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

  1. Bars and extruded sections for machining: solution treated, designation HR 4A.

  2. Billets and bars for forging: hot or cold worked and subsequently machined or ground, designation HR 4B.

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


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