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The Hastelloy X Nickel Alloy, with higher iron content, has favorable resistance to oxidation and corrosion combined with excellent creep and rupture strength at temperatures under 900℃. In addition to this, The Inconel X Pipe has great fabricability by cold and hot working and good weldability. This oxidation resistant alloy can be used for combustor components and other high temperature parts of aircraft engines, for long term use at temperature under 900℃ and short time use up to 1080℃.
Inconel X Sheet
Specifications
| UNS | W. Nr |
| N06602 | 2.4665 |
Chemical Compositions of Hastelloy X Nickel Alloy
| Composition | Ni | Cr | Fe | Mo | W | Co | C | Mn | Si | S | Cu | Al | Ti | |
| Content(%) | Min. | Bal. | 20.5 | 17.0 | 8.0 | 0.2 | 0.5 | 0.05 | | | | | | |
| Max. | 23.0 | 20.0 | 10.0 | 1.0 | 2.5 | 0.15 | 1.0 | 1.0 | 0.015 | 0.5 | 0.15 | 0.5 | ||
Mechanical Properties (Minimum value at 20℃)
| Tensile Strength (σb/MPa) | Yield Strength (σp0.2/MPa) | Elongation (σ5/%) |
| 690 | 275 | 30 |
Product Forms and Standards
| Bar | Forging | Sheet/Strip | Wire | Pipe |
| ASTM B572 | ASTM B435 | ASTM B166 | ASTM B408 | ASTM B622 ASTM B619 ASTM B626 |
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