D16 (1160)
for strength of structural elements of aircraft, car bodies, tubes, etc .; nesses for operating at temperatures up to -230 degrees.
for strength of structural elements of aircraft, car bodies, tubes, etc .; nesses for operating at temperatures up to -230 degrees.
| Standard | Fe, % | Si, % | Mg, % | Mn, % | Cr, % | Ti, % | Cu, % | Zn, % | Al, % |
|---|---|---|---|---|---|---|---|---|---|
| Standard | Fe, % | Si, % | Mg, % | Mn, % | Cr, % | Ti, % | Cu, % | Zn, % | Al, % |
| GOST 4784-97 | < 0.5 | < 0.5 | 1.2–1.8 | 0.3–0.9 | < 0.1 | < 0.15 | 3.8–4.9 | < 0.25 | 90.9–94.7 |
| Temperature, °C | E\cdot 10^{9}, MPa | \alpha\cdot 10^{6}, K^{-1} | \varkappa, \frac{W}{m\cdot K} | \rho, \frac{kg}{m^3} | c\cdot 10^{-3}, \frac{J}{kg\cdot K} |
|---|---|---|---|---|---|
| Temperature, °C | E\cdot 10^{9}, MPa | \alpha\cdot 10^{6}, K^{-1} | \varkappa, \frac{W}{m\cdot K} | \rho, \frac{kg}{m^3} | c\cdot 10^{-3}, \frac{J}{kg\cdot K} |
| 20 | 72 | 2770 | |||
| 100 | 22.9 | 130 | 0.922 |
| Rolling | Standard | Size, mm | Tension | Classifiers | \sigma _{U}, MPa | \sigma_{P}, MPa | \epsilon_L, % | Treatment |
|---|---|---|---|---|---|---|---|---|
| Rolling | Standard | Size, mm | Tension | Classifiers | \sigma _{U}, MPa | \sigma_{P}, MPa | \epsilon_L, % | Treatment |
| Trumpet | 390–420 | 255–275 | 10–12 | |||||
| Round | GOST 21488-97 | 245 | 120 | 12 | ||||
| Round | GOST 21488-97 | 8–300 | 390–410 | 275–295 | 8–10 | Quenching and aging | ||
| Round | high strength | 450–470 | 325–345 | 8–10 | Quenching and aging | |||
| Round | increased plasticity | 410 | 265 | 12 | Quenching and aging | |||
| Tape | annealing | 235 | 10 | |||||
| Profile | 10–150 | 412 | 284 | 10 | Hardening and artificial aging | |||
| Profile | annealing | 245 | 12 | |||||
| Sheet | 345–420 | 245–275 | 3–7 | Quenching and aging |
| Standard | Description |
|---|---|
| Standard | Description |
| GOST 4784-97 |
| Parameter | Units of measurement | Description |
|---|---|---|
| Parameter | Units of measurement | Description |
| E\cdot 10^{9} | MPa | Elastic modulus |
| \alpha\cdot 10^{6} | K^{-1} | Coefficient of thermal (linear) expansion (range 20°C–T) |
| \varkappa | \frac{W}{m\cdot K} | Coefficient of thermal conductivity (the heat capacity of the material) |
| \rho | \frac{kg}{m^3} | The density of the material |
| c\cdot 10^{-3} | \frac{J}{kg\cdot K} | The specific heat of the material (range 20°C–T) |