BS 4HR 601:2010
BS 4HR 601:2010
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BS 4HR 601:2010

Specification for nickel-chromium-titanium-aluminium heat-resisting alloy bar and wire (maximum diameter or minor sectional dimension of 30 mm) for the manufacture of fasteners (nickel base, Cr 19.5, Ti 2.2, Al 1.4)

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BS 4HR 601:2010

Specification for nickel-chromium-titanium-aluminium heat-resisting alloy bar and wire (maximum diameter or minor sectional dimension of 30 mm) for the manufacture of fasteners (nickel base, Cr 19.5, Ti 2.2, Al 1.4)

Purchase Options: Immediate PDF Download

Printed publication for Next Day or Standard Delivery
Price:  £106 (50% discount for members - click here for more information)

BS 4HR 601:2010

Specification for nickel-chromium-titanium-aluminium heat-resisting alloy bar and wire (maximum diameter or minor sectional dimension of 30 mm) for the manufacture of fasteners (nickel base, Cr 19.5, Ti 2.2, Al 1.4)

Purchase Options: Immediate PDF Download

Printed publication for Next Day or Standard Delivery
Price:  £106 (50% discount for members - click here for more information)
Product details for BS 4HR 601:2010
Category: AIRCRAFT AND SPACE VEHICLE ENGINEERING

Publication date:

Product detail: 10 pages

ISBN reference: 978 0 580 72045 1

Cross references to standards relating to BS 4HR 601:2010:

Keywords: Air transport engineering, Aircraft components, Nickel alloys, Chromium-containing alloys, Titanium-containing alloys, Aluminium-containing alloys, Heat-resistant materials, Bars (materials), Wires, Fasteners, Chemical composition, Dimensions, Heat treatment, Proof stress, Tensile strength, Elongation, Hardness, Precipitation hardening, Rupture stress, Grain size

Variations and abbreviations: BS4HR601:2010,BS4HR601,BS 4HR 601

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