Superalloy Series
0102030405
Summus euismod Nickel Alloy GH4738 ad Extremae Environments
CHEMICAL COMPOSITIONE
TRACTUS | % | C | And | Mn | P | S | Cr | In | Mo | cum | Al | Of | Fe | Co | B | Zr |
GH4738 | MIN | 0.03 | - | - | - | - | 18.0 | statera | 3.5 | - | 1.20 | 2.75 | - | 12.0 | 0.003 | 0.02 |
MAX | 0.10 | 0.15 | 0.10 | 0.014 | 0.014 | 21.0 | statera | 5.0 | 0.10 | 1.60 | 3.25 | 2.00 | 15.0 | 0.01 | 0.08 |
Corporalia Properties
density | Liquefaciens temperatus range |
ρ=8.22g/cm | 1330-1360℃ |
EXSECUTOR VEXILLUM
Standard No | Sample statum | Crassitudo laminae 8/mm | possessiones distrahentes | 730°C Durability | Locus temperatus duritiem | |||||
θ/℃ | distrahentes vires | cedere viribus | A5% | s/MPa | Tempus / h * | A% | ||||
QJ/DT01.63026 | Supple statum | ≤0.50 | 20 | ≥1170 | ≥760 | ≥15 |
| - | L | (34 ad 44) HRC vel aequivalens |
540 | ≥1000 | ≥690 | ≥13 |
| - |
|
| |||
>0.50 | 20 | ≥1205 | ≥795 | ≥20 | - |
| - | (34 ad 44) HRC vel aequivalens | ||
540 | ≥1035 | ≥725 | ≥15 |
|
| - |
| |||
>0.40～0.50 |
|
|
|
| 430 | ≥23 | ≥4 |
| ||
>0.50 |
|
|
|
| 430 | ≥23 | ≥4 | |||
Product pluma
GH738 est nickel-substructio summus temperatura mixtura obdurata per γ' phase praecipitatio, cum bono gas corrosio resistentia, alta vires ac lassitudines cedunt proprietates, processus bonus plasticitas et ordo stabilis. Late usus est in machinis aircraft rotatione partium, usus temperaturae non altior quam 815 . Frigus involutum et calidum involutum producere potest laminas, tibias, ligamenta, fila, malleos, fusuras et ligatores.
Product application
Aeroplana tormenta, machinae gasorum turbines, turbines laminarum et turbines orbis ac aliarum partium rotationis.
