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>BSI Standards >49 AIRCRAFT AND SPACE VEHICLE ENGINEERING>49.025 Materials for aerospace construction>49.025.99 Other materials>BS 3HR 1:2010+A1:2016 Specification for nickel-chromium-titanium-aluminium heat-resisting alloy billets, bars, forgings and parts (Nickel base, Cr 19.5, Ti 2.2, Al 1.4)
immediate downloadReleased: 2016-07-31
BS 3HR 1:2010+A1:2016 Specification for nickel-chromium-titanium-aluminium heat-resisting alloy billets, bars, forgings and parts (Nickel base, Cr 19.5, Ti 2.2, Al 1.4)

BS 3HR 1:2010+A1:2016

Specification for nickel-chromium-titanium-aluminium heat-resisting alloy billets, bars, forgings and parts (Nickel base, Cr 19.5, Ti 2.2, Al 1.4)

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Standard number:BS 3HR 1:2010+A1:2016
Pages:16
Released:2016-07-31
ISBN:978 0 580 93962 4
Status:Standard
DESCRIPTION

BS 3HR 1:2010+A1:2016


This standard BS 3HR 1:2010+A1:2016 Specification for nickel-chromium-titanium-aluminium heat-resisting alloy billets, bars, forgings and parts (Nickel base, Cr 19.5, Ti 2.2, Al 1.4) is classified in these ICS categories:
  • 49.025.99 Other materials

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

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

  2. Extruded sections for subsequent forming: softened, designation HR 1B.

  3. Billets and bars for forging: hot or cold worked and subsequently machined or ground, designation HR 1C.

  4. Forgings: solution treated, designation HR 1D.


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