Customization: | Available |
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Processing Object: | Metal |
Molding Style: | Hot Forging |
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Chemical Composition of 2A16 | |||||||||||||
Alloy | Si | Fe | Cu | Mn | Mg | Cr | Ni | Zn | Ti | Zr | Others | Al | |
Each | Total | ||||||||||||
2A16 | 0.30 | 0.30 | 6.0~7.0 | 0.4~0.8 | 0.05 | - | - | 0.10 | 0.10~0.20 | 0.20 | 0.05 | 0.15 | Rest |
2219 | 0.20 | 0.30 | 5.8~6.8 | 0.20~0.40 | 0.02 | - | - | 0.10 | 0.02~0.10 | 0.10~0.25 | 0.05 | 0.15 | Rest |
Alloy | Type | Temper | Portrait | Transverse | HBS | Standard | ||||
σb/MPa | σp 0.2/MPa | δ/% | σb/MPa | σp 0.2/MPa | δ/% | |||||
2A16 | Die forging | T6 | 375 | 255 | 8 | 375 | 255 | 8 | 100 | GJB 2351 |
Free forging | 355 | 235 | 8 | 355 | 235 | 8 | 100 | |||
Die forging | T6 | 375 | 255 | 8 | 375 | 255 | 8 | 100 | HB 5204 | |
Free forging | 355 | 235 | 8 | 355 | 235 | 8 | 100 |
Alloy | Temper | Available airplane type | Application parts and typical parts |
2A16 | Forgings: T6 | MIG, B737-300,A320,Y8,ARJ21,JH7,J10 | Rocket fuel tank, engine blade, airtight cockpit, hood, wing integral mailbox, fuselage internal structure, etc. |
Type | Alloy | Projected area(m2)Or weight(kg) | Temper | Standard |
Free forgings | 5 series | ≤3000kg | O,F | GBn223 ASTMB247 |
2,6,7 series | ≤3000kg | T6,T4,O,F | ||
Mould forgings | 5 series | ≤2.5m2 | O,F | |
2,6,7 series | ≤2.5m2 | T6,T4,O,F |