Inconel X750 is a nickel chromium alloy made precipitation hardenable by the additions of Titanium and aluminum. This nickel alloy exhibits high creep-rupture strength at elevated temperatures to about 130.0°F (700°C). It also has excellent properties down to cryogenic temperatures. The alloy maintains high strength at high temperature, resists corrosion and has good oxidation resistance at up to 1300°F.
Nickel + Cobalt: 70.00 min
Chromium: 14.0-17.0
Iron: 5.0-9.0
Titanium: 2.25-2.75
Aluminum: 0.40-1.00
Columbium + Tantalum: 0.70-1.20
Manganese: 1.00 max.
Silicon: 0.50 max.
Sulfur: 0.01 max.
Copper: 0.50 max.
Carbon: 0.08 max.
Cobalt: 1.00 max
Density: 8.28g/cm3
Melting point: 1390 ℃ -1420 ℃
AlloyX-750 Mechanical Properties - Solution Annealing
Tensile strength: ≤ 1267 MPa;
Yield strength: ≤ 868MPa;
Elongation: ≤ 25%
Inconel X-750 is a member of the Inconel alloy series. Inconel X-750 nickel based alloys have excellent high-temperature strength and thermal stability, and can maintain high mechanical properties at high temperatures. Its creep resistance and antioxidant properties make it an ideal choice for many high-temperature applications.
The Inconel X-750 has excellent corrosion resistance, exhibiting good corrosion resistance in acidic, alkaline, and oxidizing environments. Therefore, it is widely used in corrosion resistant equipment in the chemical and petroleum industries.
Inconel X-750 alloy has good strength and plasticity. It can be strengthened through heat treatment and still maintain a certain degree of plasticity at high temperatures, making it suitable for manufacturing various complex shaped parts.
Inconel X-750 alloy is widely used in aerospace, petrochemical, nuclear energy, shipbuilding, automotive, medical equipment and other fields. It is often used to manufacture high-temperature components, turbine engine blades, combustion chamber parts, high-temperature gas turbines, springs, valves, and corrosion-resistant equipment.
Inconel X750 is a nickel chromium alloy made precipitation hardenable by the additions of Titanium and aluminum. This nickel alloy exhibits high creep-rupture strength at elevated temperatures to about 130.0°F (700°C). It also has excellent properties down to cryogenic temperatures. The alloy maintains high strength at high temperature, resists corrosion and has good oxidation resistance at up to 1300°F.
Nickel + Cobalt: 70.00 min
Chromium: 14.0-17.0
Iron: 5.0-9.0
Titanium: 2.25-2.75
Aluminum: 0.40-1.00
Columbium + Tantalum: 0.70-1.20
Manganese: 1.00 max.
Silicon: 0.50 max.
Sulfur: 0.01 max.
Copper: 0.50 max.
Carbon: 0.08 max.
Cobalt: 1.00 max
Density: 8.28g/cm3
Melting point: 1390 ℃ -1420 ℃
AlloyX-750 Mechanical Properties - Solution Annealing
Tensile strength: ≤ 1267 MPa;
Yield strength: ≤ 868MPa;
Elongation: ≤ 25%
Inconel X-750 is a member of the Inconel alloy series. Inconel X-750 nickel based alloys have excellent high-temperature strength and thermal stability, and can maintain high mechanical properties at high temperatures. Its creep resistance and antioxidant properties make it an ideal choice for many high-temperature applications.
The Inconel X-750 has excellent corrosion resistance, exhibiting good corrosion resistance in acidic, alkaline, and oxidizing environments. Therefore, it is widely used in corrosion resistant equipment in the chemical and petroleum industries.
Inconel X-750 alloy has good strength and plasticity. It can be strengthened through heat treatment and still maintain a certain degree of plasticity at high temperatures, making it suitable for manufacturing various complex shaped parts.
Inconel X-750 alloy is widely used in aerospace, petrochemical, nuclear energy, shipbuilding, automotive, medical equipment and other fields. It is often used to manufacture high-temperature components, turbine engine blades, combustion chamber parts, high-temperature gas turbines, springs, valves, and corrosion-resistant equipment.
