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X-750 Inconel Nickel Alloy Corrosion Oxidation Resistance High Strength Below 1300°F
|Equal Grades||UNS N07750, W. Nr. 2.4669, GH4145||Density||8.28g/cm3|
|Melting Range||1393-1427°C||Curie Piont||-225°C|
|Forms Of Supply||Bar, Wire, Sheet, Plate, Forgings, Pipe Fittings, Flanges, Seamless & Welded Pipe, Seamless Tube & Welded Tube, Weld Rod||Specifications||AMS 5598, ASME SB-637, ASTM B 637, UNS N07750, W. Nr./EN 2.4669|
chromium nickel alloy,
corrosion resistant alloys
Inconel X-750 Corrosion and Oxidation Resistance and High Strength up to 1300°F
Inconel X750 is a precipitation-hardenable nickel-chromium alloy used for its corrosion and oxidation resistance and high strength at temperatures to 1300°F. Although much of the effect of precipitation hardening is lost with increasing temperature over 1300°F, heat-treated material has useful strength up to 1800°F. Alloy X-750 also has excellent properties down to cryogenic termperatures.
The economics of INCONEL alloy X-750 coupled with its availability in all standard mill forms has resulted in applications in a wide variety of industrial fields. In gas turbines, it is used for rotor blades and wheels, bolts, and other structural members. INCONEL X-750 is used extensively in rocket-engine thrust chambers. Airframe applications include thrust reversers and hot-air ducting systems. Large pressure vessels are formed from INCONEL alloy X-750. Other applications are heat-treating fixtures, forming tools, extrusion dies, and test machine grips. For springs and fasteners, INCONEL X-750 is used from sub-zero to 1200°F.
|Weight(%)||70.0 min||14.0~17.0||5.0~9.0||2.25~2.7||0.4~1.0||0.7~1.2||1.0 max||0.5 max||0.010 max||0.5 max||0.08 max||1.0 max|
- Good mechanical properties at high temperatures
- Good formability
- Good oxidation resistance
- Oil and gas production
- Gas turbine engines
- Nuclear engineering