BS L 161:1976
Withdrawn
Specification. Hand and die forgings of aluminium-zinc-magnesium-copper-chromium alloy (solution treated and artificially aged to an overaged condition) (Zn 5.6, Mg 2.5, Cu 1.6, Cr 0.22)
Hardcopy , PDF
English
05-28-1976
09-27-2012
NO CONTENTS SECTION
Describes manufacture, inspection and testing of heat resisting alloys for aerospace use. Gives chemical composition and mechanical properties. This covers hand and die forgings of aluminium zinc magnesium copper chromium alloy.
| Committee |
ACE/61/-/24
|
| DevelopmentNote |
Supersedes 72/36415 DC. (08/2005) Inactive for the new design. (12/2007)
|
| DocumentType |
Standard
|
| Pages |
8
|
| PublisherName |
British Standards Institution
|
| Status |
Withdrawn
|
| BS L 160:1976 | Specification. Bars and extruded sections of aluminium-zinc-magnesium-copper-chromium alloy (solution treated and artificially aged to an overaged condition) (Zn 5.6, Mg 2.5, Cu 1.6, Cr 0.22) |
| BS L 162:1976 | Specification. Cold compressed hand forgings of aluminium-zinc-magnesium-copper-chromium alloy (solution treated and artificially aged to an overaged condition) (Zn 5.6, Mg 2.5, Cu 1.6, Cr 0.22) |
| BS L 162:1976 | Specification. Cold compressed hand forgings of aluminium-zinc-magnesium-copper-chromium alloy (solution treated and artificially aged to an overaged condition) (Zn 5.6, Mg 2.5, Cu 1.6, Cr 0.22) |
| BS 3763:1970 | The International System of units (SI) |
| BS 350:2004 | Conversion factors for units |
| BS L 160:1976 | Specification. Bars and extruded sections of aluminium-zinc-magnesium-copper-chromium alloy (solution treated and artificially aged to an overaged condition) (Zn 5.6, Mg 2.5, Cu 1.6, Cr 0.22) |
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