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BS EN 4376:2016
Aerospace series. Heat resisting alloy NiCr19Fe19Nb5Mo3 (2.4668) solution treated and precipitation treated. Bar and section, De = 200 mm
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Summary
Nickel alloys;Mechanical properties of materials;Chemical composition;Heat-resistant materials;Metal sections;Solution heat treatment;Elongation;Air transport engineering;Wrought alloys;Tensile strength;Bars (materials);Heat treatment;Grain size;Dimensions;Rupture stress;Hardness;Proof stress
Technical characteristics
| Publisher | British Standards Institution (BSI) |
| Publication Date | 03/31/2016 |
| Page Count | 14 |
| Themes | Proof stress |
| EAN | --- |
| ISBN | --- |
| Weight (in grams) | --- |
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