High-Strength, Heat-Resistant Superalloy for Extreme Environments
Product Overview
Inconel 718 bar stock is a nickel-chromium-based superalloy strengthened by age-hardening, delivering exceptional strength and oxidation resistance at temperatures up to 700°C (1292°F). Widely used in aerospace, oil & gas, nuclear energy, and high-end industrial applications, this material complies with ASTM B637, AMS 5662/5663, and other international standards. It is the premier choice for turbine blades, rocket engine components, and deep-sea drilling tools.
Product Specifications
- Material & Processing
- Composition: Nickel (Ni 50-55%), Chromium (Cr 17-21%), Iron (Fe balance), Niobium (Nb 4.75-5.5%)
- Standards: ASTM B637, AMS 5662, AMS 5663, DIN 17752
- Heat Treatment: Solution Annealed or Age Hardened
- Dimensions & Forms
- Diameter Range: Φ5mm to Φ300mm (custom sizes available)
- Surface Finish: Turned, Polished, Hot Rolled (Black)
- Length: Cut-to-Size (1m-6m) or Random
- Mechanical Properties
- Tensile Strength: ≥1275 MPa (Age Hardened)
- Yield Strength: ≥1035 MPa
- Elongation: ≥12%
- Hardness: ≥35 HRC
Key Advantages
✅ High-Temperature Performance: Superior oxidation and creep resistance at 700°C.
✅ Corrosion Resistance: Resists H2S, CO2, chlorides, and acidic environments (NACE MR0175 certified).
✅ Machinability: Excellent forgeability and weldability, ideal for CNC precision machining.
✅ Extended Lifespan: 3-5x longer service life vs. standard alloys due to fatigue and fretting resistance.
Applications
- Aerospace: Jet engine turbine disks, combustion chambers, rocket thrusters
- Oil & Gas: Downhole tools, deep-sea valve stems, LNG pump shafts
- Power Generation: Gas turbine blades, nuclear reactor fasteners
- Automotive: High-performance racing engine parts, turbochargers
- Chemical Processing: Agitator shafts for acidic reactors, high-temperature flangesHigh-Strength, Heat-Resistant Superalloy for Extreme Environments
Product Overview
Inconel 718 bar stock is a nickel-chromium-based superalloy strengthened by age-hardening, delivering exceptional strength and oxidation resistance at temperatures up to 700°C (1292°F). Widely used in aerospace, oil & gas, nuclear energy, and high-end industrial applications, this material complies with ASTM B637, AMS 5662/5663, and other international standards. It is the premier choice for turbine blades, rocket engine components, and deep-sea drilling tools.
Product Specifications
- Material & Processing
- Composition: Nickel (Ni 50-55%), Chromium (Cr 17-21%), Iron (Fe balance), Niobium (Nb 4.75-5.5%)
- Standards: ASTM B637, AMS 5662, AMS 5663, DIN 17752
- Heat Treatment: Solution Annealed or Age Hardened
- Dimensions & Forms
- Diameter Range: Φ5mm to Φ300mm (custom sizes available)
- Surface Finish: Turned, Polished, Hot Rolled (Black)
- Length: Cut-to-Size (1m-6m) or Random
- Mechanical Properties
- Tensile Strength: ≥1275 MPa (Age Hardened)
- Yield Strength: ≥1035 MPa
- Elongation: ≥12%
- Hardness: ≥35 HRC
Key Advantages
✅ High-Temperature Performance: Superior oxidation and creep resistance at 700°C.
✅ Corrosion Resistance: Resists H2S, CO2, chlorides, and acidic environments (NACE MR0175 certified).
✅ Machinability: Excellent forgeability and weldability, ideal for CNC precision machining.
✅ Extended Lifespan: 3-5x longer service life vs. standard alloys due to fatigue and fretting resistance.Applications
- Aerospace: Jet engine turbine disks, combustion chambers, rocket thrusters
- Oil & Gas: Downhole tools, deep-sea valve stems, LNG pump shafts
- Power Generation: Gas turbine blades, nuclear reactor fasteners
- Automotive: High-performance racing engine parts, turbochargers
- Chemical Processing: Agitator shafts for acidic reactors, high-temperature flanges