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2A70 Aircraft aerospace aluminum plate forgings profile
Chemical Property of 2A70 Alloy | |||||||||||||
Alloy | Si | Fe | Cu | Mn | Mg | Cr | Ni | Zn | Ti | Zr | Others | Al | |
Each | Total | ||||||||||||
2A70 | 0.35 | 0.9~1.5 | 1.9~2.5 | 0.2 | 1.4~1.8 | - | 0.9~1.5 | 0.30 | 0.02~0.10 | - | 0.05 | 0.15 | Remainder |
Alloy | Alloy series | Main Features |
2A70 | Al-Cu-Mg-Ni | Heat treatment strengthened alloy, Al-Cu-Mg-Si heat treated aluminum alloy, heat resistant alloy used in artificial aging, and 2A70, 2A80 and 2A90 alloy used in aviation industry. 2A70 alloy has the highest heat resistance, the most widely applied and the applied temperature is 200~250 C. the alloy has good technological characteristics, and can be processed into plates, strips, rods, profiles and free forgings, die forgings and so on. In aircraft manufacturing, it is mostly used for forging engine piston, impeller, wheel, compressor blade, and other parts used at high temperature. |
Calibration mechanical properties of 2A70 T6 alloy | ||||||
Standard | Type | d/mm | Direction | Rm/Mpa | A5/% | HBS |
GB/T 3191 | Extrusion aluminum round bar | ≤150 | L | 355 | 8 | - |
GJB 2054 | Aluminum round bar | 5~150 | L | 355 | 8 | - |
>150 | 345 | 6 | ||||
HB 5202 | Extruded aluminum round bar | ≤22 | L | 355 | 8.0 | - |
23~160 | 375 | 8.0 | ||||
GJB 2351 | Free forgings and die forgings | - | L | 375 | 4.0 | 110 |
LT | 375 | 4.0 | ||||
ST | 375 | 4.0 | ||||
HB 5204 | Free forgings | - | L | 375 | 5.0 | 110 |
LT | 375 | 5.0 | ||||
ST | 375 | 5.0 | ||||
Die forgings | - | L | 380 | 5.0 | 110 | |
LT | 380 | 5.0 | ||||
ST | 380 | 5.0 | ||||
Typical room temperature mechanical properties of alloy 2A70 T6 | ||||||
Type | Temper | δ/mm | Direction | Rm/Mpa | Rp0.2/Mpa | A5/% |
Clad aluminum sheet | O | 1.0~10 | L | 245 | 15 | |
T6 | 1.0~1.5 | L | 392 | 265 | 13 | |
1.6~2.5 | 402 | 275 | 12 | |||
2.6~6.0 | 407 | 280 | 11 | |||
6.0~10 | 407 | 280 | 10 | |||
Die forgings | T6 | - | L | 431 | 294 | 19.6 |
LT | 425 | 284 | 10.8 |
Mechanical properties of stabilized treatment of 2A70 | |||||||||||
Type | Stabilized treatment | Rm/Mpa | Rp0.2/Mpa | A/% | Type | Stabilized treatment | Rm/Mpa | Rp0.2/Mpa | A/% | ||
θ/℃ | t/h | θ/℃ | t/h | ||||||||
Aluminum sheet | 125 | 1000 | 363 | 324 | 9 | Forgings sheet stock | 175 | 100 | 333 | 8 | |
5000 | 363 | - | 9 | 1000 | 333 | 9 | |||||
10000 | 363 | 314 | 8 | 5000 | 314 | 9 | |||||
20000 | 363 | 294 | 7 | 10000 | 304 | 8 | |||||
150 | 100 | 402 | 343 | - | 20000 | 275 | 7 | ||||
1000 | 412 | 363 | 5 | 30000 | 265 | 8 | |||||
5000 | 382 | 333 | 6 | 195 | 100 | 314 | 10 | ||||
10000 | 314 | 284 | 8 | 1000 | 284 | 10 | |||||
20000 | 314 | 294 | 8 | 5000 | 275 | 12 | |||||
175 | 10 | 402 | 343 | 6 | 10000 | 255 | 12 | ||||
100 | 392 | 338 | 5 | 20000 | 245 | 12 | |||||
1000 | 392 | 324 | 6 | 30000 | 245 | 12 | |||||
200 | 10 | 412 | 353 | 5 | Extrusion aluminum profile | 125 | 100 | 402 | 373 | 7.5 | |
100 | 373 | 314 | 6 | 1000 | 402 | 373 | 7.5 | ||||
Forgings sheet stock | 125 | 100 | 402 | - | 8 | 5000 | 392 | 358 | 7.5 | ||
1000 | 422 | - | 6 | 10000 | 384 | 343 | 7 | ||||
5000 | 402 | - | 7 | 30000 | 384 | 333 | 8 | ||||
10000 | 402 | - | 7 | 150 | 100 | 397 | 363 | 8 | |||
20000 | 373 | - | 7 | 1000 | 422 | 373 | 7 | ||||
30000 | 373 | - | 6 | 5000 | 384 | 358 | 7 | ||||
150 | 100 | 402 | - | 6 | 10000 | 343 | 343 | 8 | |||
1000 | 392 | - | 6 | 30000 | 314 | 333 | 8 | ||||
5000 | 353 | - | 8 | 175 | 100 | 392 | 363 | 7.5 | |||
10000 | 353 | - | 8 | 1000 | 373 | 333 | 8 | ||||
20000 | 314 | - | 7 | Die forgings | 130 | 100 | 412 | 343 | 12 | ||
30000 | 314 | - | 6 | 1000 | 412 | 343 | 12 | ||||
150 | 10 | 412 | 333 | 11 | 10000 | 412 | 343 | 12 | |||
100 | 407 | 333 | 10 | 30000 | 373 | - | 16 | ||||
1000 | 392 | 314 | 10 | Die forgings | 200 | 10 | 324 | 237 | 14 | ||
30000 | 314 | - | 4 | 100 | 284 | 226 | 17 | ||||
175 | 10 | 363 | 314 | 11 | 1000 | 245 | 196 | 20 | |||
100 | 353 | 304 | 13 | 250 | 10 | 196 | 177 | 18 | |||
1000 | 333 | 255 | 15 | 100 | 177 | 118 | 20 | ||||
3000 | 255 | - | 18 | 1000 | 127 | 88 | 25 |