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BS 3HR 502:2011 (R2016)
Specification for nickel-chromium-cobalt-titanium- aluminium heat-resisting alloy cold drawn and solution treated wire for springs and springs (Nickel base, Cr 19.5, Co 18.0, Ti 2.5, Al 1.5)
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Summary
Aircraft components;Heat-resistant materials;Air transport engineering;Nickel alloys;Aluminium-containing alloys;Cold-working;Diameter;Wires;Titanium-containing alloys;Solution heat treatment;Chromium-containing alloys;Mechanical properties of materials;Springs;Cobalt-containing alloys;Heat treatment;Chemical composition
Technical characteristics
| Publisher | British Standards Institution (BSI) |
| Publication Date | 01/31/2011 |
| Confirmation Date | 06/01/2016 |
| Page Count | 10 |
| Themes | Chemical composition |
| EAN | --- |
| ISBN | --- |
| Weight (in grams) | --- |
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