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Features:
Inconel X750 is an age-hardenable nickel-chromium alloy. It has good corrosion and oxidation resistance. The high strength at temperatures can be up to 700℃. Inconel X-750 also has good properties when it comes to cryogenic temperatures. Its corrosion resistance performance is similar to Inconel 600.
Applications:
Inconel X-750 can be applied in Gas turbine engines, rocket motors, heat treating fixtures, nuclear reactors, pressure vessels and airframes.
Inconel X-750 Chemical composition:
| Alloy | % | Ni | Cr | Fe | Nb | Co | C | Mn | Si | S | Cu | Al | Ti |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Inconel X-750 | Min. | 14 | 5.0 | 0.7 | 0.4 | 2.25 | |||||||
| Max. | 70 | 17 | 9.0 | 1.2 | 1.00 | 0.08 | 1.00 | 0.5 | 0.01 | 0.5 | 1.0 | 2.75 |
Inconel X-750 Physical properties:
| Density | 8.28 g/cm3 |
| Melting range | 1393-1427℃ |
Inconel X-750 Alloy m inimum Mechanical properties in the room temperature:
| Alloy | Tensile strength Rm N/mm2 | Yield strength RP0.2N/mm2 | Elongation A5 % | Brinell hardness HB |
| Solution treatment | 1267 | 868 | 25 | ≤400 |
Features:
Inconel X750 is an age-hardenable nickel-chromium alloy. It has good corrosion and oxidation resistance. The high strength at temperatures can be up to 700℃. Inconel X-750 also has good properties when it comes to cryogenic temperatures. Its corrosion resistance performance is similar to Inconel 600.
Applications:
Inconel X-750 can be applied in Gas turbine engines, rocket motors, heat treating fixtures, nuclear reactors, pressure vessels and airframes.
Inconel X-750 Chemical composition:
| Alloy | % | Ni | Cr | Fe | Nb | Co | C | Mn | Si | S | Cu | Al | Ti |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Inconel X-750 | Min. | 14 | 5.0 | 0.7 | 0.4 | 2.25 | |||||||
| Max. | 70 | 17 | 9.0 | 1.2 | 1.00 | 0.08 | 1.00 | 0.5 | 0.01 | 0.5 | 1.0 | 2.75 |
Inconel X-750 Physical properties:
| Density | 8.28 g/cm3 |
| Melting range | 1393-1427℃ |
Inconel X-750 Alloy m inimum Mechanical properties in the room temperature:
| Alloy | Tensile strength Rm N/mm2 | Yield strength RP0.2N/mm2 | Elongation A5 % | Brinell hardness HB |
| Solution treatment | 1267 | 868 | 25 | ≤400 |