5A02/5A03/5A05 Aircraft Aerospace Aluminum Structural Shapes for AviationThe magnesium content of 5A05 alloy is high, although the cold deformation can increase its strength, but the plasticity will decrease. The O state material has higher plasticity, and the plasticity of H * 4 material is moderat......
| Chemical Composition of 5A05 alloy | |||||||||||
| Alloy | Si | Fe | Cu | Mn | Mg | Zn | Ti | Others | Al | ||
| Each | Total | ||||||||||
| 5A05 | 0.5 | 0.5 | 0.1 | 0.30~0.6 | 4.8~5.5 | - | - | - | 0.05 | 0.15 | Remainder |
| Calibration mechanical strength of 5A05 aluminum alloy sheet profile forgings wire | ||||||
| Technical standard | Type | Temper | δ or d/mm | Tension strength Rm/Mpa | Rp0.2/Mpa | A/% |
| GB/T 3880 | Aluminum sheet | O | 0.5~4.5 | ≤275 | ≥145 | ≥16 |
| H112 | >4.5~10.0 | ≥275 | ≥125 | ≥16 | ||
| >10.0~12.5 | ≥265 | ≥115 | ≥14 | |||
| >12.5~25.0 | ≥265 | ≥115 | ≥14 | |||
| >25.0~50.0 | ≥255 | ≥105 | ≥13 | |||
| GJB 2503 | Aluminum sheet | O | 0.5~4.0 | ≤275 | ≥147 | ≥15 |
| GJB 2662 | Aluminum plate | H112 | 7~10 | ≥275 | ≥127 | ≥15 |
| >10~25 | ≥265 | ≥118 | ≥13 | |||
| >25~50 | ≥255 | ≥108 | ≥12 | |||
| GB/T 3191 | Extruded aluminum round bar | H112, O | ≤150 | ≥265 | ≥120 | ≥15 |
| GJB 2504 | Extruded aluminum round bar | 150~250 | ≥265 | ≥120 | ≥15 | |
| HB 5202 | Extruded aluminum round bar | ≤240 | ≥230 | ≥118 | ≥10 | |
| GJB 2507 | Extruded aluminum round bar | H112, O | All | ≥265 | ≥118 | ≥15 |
| GB/T 4437 | Aluminum tube | H112 | All | ≥255 | ≥108 | ≥15 |
| GJB 2381 | Aluminum tube | H112 | >25~180 | ≥255 | ≥108 | ≥12 |
| >180~250 | ≥10 | |||||
| H112 | >25~180 | ≤255 | ≥108 | ≥15 | ||
| >180~250 | ≥12 | |||||
| GJB 2379 | Cold drawn aluminum tube | O | All | ≤215 | ≥88 | ≥15 |
| H×4 | All | ≥245 | ≥147 | ≥8 | ||
| GJB 2351 | Free forgings,Die forgings | H112 | As agreed | ≥196 ≥220 | - - | ≥10 ≥12 |
| GJB 2055 | Aluminum wire | H×8 | 1.6~10.0 | ≥166 | - | - |
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