الوصف
Aircraft Structures Inconel Alloy,X750 Material Inconel Titanium,760 MPA Strip Inconel Alloy
- Inconel Series
Inconel Alloy X-750, inconel x750 Strip is a nickel-chromium austenitic alloy sim
ilar to Alloy 600 but made precipitation-hardenable by additions of aluminum and titanium. It has good resistance to corrosion and oxidation along with high tensile and creep-rupture properties at high temperatures to 1300°F (700°C). Extended applications that require high strength
at temperatures beyond 1100°F (593°C) may require a solution treatment, with air cooling between intermediate and final aging.
This material has excellent relaxation resistance and is non-magnetic. It has good elevated temperature strength properties to 1300ºF (700°C) and oxidation resistance to 1800ºF (983˚C). Inconel® X-750 is resistant to a wide variety of industrial corrosives under both oxidizing and reducing conditions. This alloy also has excellent resistance to chloride stress corrosion cracking in the fully age hardened condition.
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Chemical Properties of Inconel X750
| Element | Ni +Co | كر | ن ب | Ti | C | من | Si | النحاس | آل | S | Iron |
| Chemical Composition (%) |
70% Min |
14%- 17% |
0.7%- 1.2% |
2.25%- 2.75% |
0.08% max | 1% max | 0.5% max | 0.30% max | 0.4%-1.0% | 0.01% max | 5%-9% |
- Application
Some typical applications are:
- Gas turbines
- Jet engine parts
- Nuclear power plant applications
- Heat-treating fixtures
- Forming tools and extrusion dies
- Pressure vessels
- Aircraft structures
