Material Name and Equivalent Names: Inconel 718, or Alloy 718, complies with UNS N07718 and follows ASTM B637, B670, and DIN/EN 2.4668 standards. It is referred to by names like Nicrofer 5219, Altemp 718, and Chronin 718. Its Chinese equivalent is GH4169 under GB/T 15059.
Inconel 718 is a precipitation-hardened nickel-chromium alloy known for exceptional tensile strength, corrosion resistance, and high-temperature stability. It offers reliable performance under extreme stress and thermal cycling conditions, making it suitable for aerospace engines, gas turbines, and nuclear applications.
Designed to operate effectively at temperatures up to 650°C, the alloy maintains its mechanical properties over long service durations. Inconel 718’s fatigue resistance, high creep rupture strength, and ability to withstand oxidation make it a versatile solution for aerospace, energy, and oil and gas industries.
Potential alternatives to Inconel 718 include Hastelloy X, Waspaloy, and Rene 41. Hastelloy X offers improved oxidation resistance but slightly lower tensile strength. Waspaloy provides higher thermal stability but is more challenging for machines. Rene 41 exhibits superior creep resistance but lacks the corrosion protection found in Inconel 718.
Each of these alloys serves specific purposes, but Inconel 718 remains the go-to choice for applications demanding high strength and corrosion resistance over a wide temperature range.
Inconel 718 is designed for high-performance applications where strength, corrosion resistance, and fatigue durability are critical. The alloy's nickel content ensures thermal stability, while chromium improves oxidation resistance. Molybdenum and niobium provide added strength, and titanium enhances the precipitation-hardening process, contributing to long-term mechanical performance.
The design focused on creating a material capable of withstanding high temperatures, mechanical stress, and aggressive environments. Inconel 718's strength and corrosion resistance balance makes it ideal for aerospace engines, nuclear reactors, and gas turbines.
The chemical composition of Inconel 718 ensures durability under extreme conditions while enhancing corrosion resistance and mechanical stability.
Element | Composition (%) |
---|---|
Nickel (Ni) | 50.0 – 55.0 |
Chromium (Cr) | 17.0 – 21.0 |
Molybdenum (Mo) | 2.8 – 3.3 |
Iron (Fe) | Balance |
Niobium (Nb) | 4.75 – 5.50 |
Titanium (Ti) | 0.65 – 1.15 |
Inconel 718 offers a unique combination of thermal conductivity, density, and mechanical stiffness, making it highly reliable for high-temperature applications.
Property | Value |
---|---|
Density (g/cm³) | 8.19 |
Melting Point (°C) | 1260 |
Thermal Conductivity (W/(m·K)) | 11.4 |
Modulus of Elasticity (GPa) | 205 |
Inconel 718 has a face-centered cubic (FCC) structure, typical of nickel-based alloys. The alloy’s microstructure is strengthened through precipitation hardening, with gamma prime (γ') and gamma double prime (γ'') phases enhancing creep and tensile strength.
Niobium and titanium are critical in stabilizing the microstructure and preventing grain boundary precipitation. This structure ensures that Inconel 718 maintains mechanical integrity under cyclic thermal and mechanical loads, making it ideal for jet engines and gas turbines.
Inconel 718 provides excellent mechanical strength, fatigue resistance, and creep strength, ensuring reliable performance under extreme conditions.
Property | Value |
---|---|
Tensile Strength (MPa) | 1240 – 1375 |
Yield Strength (MPa) | 1035 – 1240 |
Creep Strength | High at 650°C / 20,000 hours |
Fatigue Strength (MPa) | 480 – 650 |
Hardness (HRC) | Rockwell C35 – 45 |
Elongation (%) | 15 – 25 |
Elastic Modulus (GPa) | ~210 |
1. Outstanding High-Temperature Performance: Inconel 718 offers excellent strength and creep resistance at temperatures up to 650°C, making it suitable for gas turbines, jet engines, and power plants.
2. Superior Corrosion Resistance: With a high chromium and molybdenum content, Inconel 718 withstands oxidation and corrosion in harsh environments, ensuring durability in chemical and marine applications.
3. High Fatigue Resistance: The alloy exhibits remarkable resistance to fatigue, making it ideal for cyclic loading conditions found in aerospace engines and rotating machinery.
4. Excellent Creep Rupture Strength: Inconel 718 retains its mechanical integrity under continuous stress, with a creep rupture life of 20,000 hours at 650°C and 345 MPa.
5. Ease of Fabrication and Weldability: Unlike many superalloys, Inconel 718 offers good machinability and weldability, allowing cost-effective fabrication without compromising performance.
Inconel 718 can be effectively used in Vacuum Investment Casting. This process ensures high-quality precision components, minimizing defects while maintaining the alloy’s superior mechanical properties for aerospace and turbine applications.
It is not suited for Single Crystal Casting due to its precipitation-hardening design, which relies on grain structures rather than single-crystal formation for strength.
Inconel 718 is a good candidate for Equiaxed Crystal Casting, where its uniform grain structure enhances fatigue resistance and high-temperature performance, making it ideal for turbine disks and engine components.
It also works well in Superalloy Directional Casting, as aligned grains improve creep resistance, extending service life in high-temperature applications.
Inconel 718 is commonly used in powder metallurgy turbine discs as it has exceptional resistance to creep and fatigue at elevated temperatures.
Superalloy Precision Forging enhances the material’s fatigue strength and durability, making Inconel 718 an excellent choice for high-performance aerospace and power generation components.
While not commonly employed in Superalloy 3D Printing, research advances additive manufacturing techniques to achieve near-cast properties.
Inconel 718 offers excellent machinability through CNC Machining with proper tool management to address work hardening, ensuring precision in complex components.
Superalloy Welding is feasible with Inconel 718, thanks to its low susceptibility to post-weld cracking, making it suitable for aerospace and industrial applications.
Hot Isostatic Pressing (HIP) further enhances the alloy’s density, eliminating porosity and improving fatigue life for critical components in aerospace and power industries.
In Aerospace and Aviation, Inconel 718 is widely used for turbine blades, engine components, and exhaust systems due to its high fatigue resistance and thermal stability.
In Power Generation, the alloy’s ability to withstand long-term exposure to high temperatures makes it ideal for gas turbines and heat exchangers.
In Oil and Gas, Inconel 718 is used in downhole tools and flow-control equipment, offering corrosion resistance under extreme conditions.
In Energy applications, Inconel 718 ensures reliability in turbines and reactors, reducing maintenance costs and enhancing performance.
In the Marine sector, the alloy’s corrosion resistance makes it valuable for components exposed to seawater, such as exhaust systems and valves.
In Mining, the alloy is used for high-stress applications like pumps and valves that withstand both wear and extreme temperatures.
In the automotive industry, Inconel 718 is applied to turbochargers and exhaust components, where heat resistance and strength are essential for efficiency.
In Chemical Processing, the alloy offers excellent corrosion resistance, making it ideal for reactors and heat exchangers exposed to harsh chemicals.
In the Pharmaceutical and Food industries, Inconel 718 ensures contamination-free environments by resisting chemical exposure in processing equipment.
In Military and Defense, the alloy provides reliability in missiles, jet engines, and other high-stress military systems.
In the Nuclear industry, Inconel 718 is used for reactor components, offering exceptional thermal stability and corrosion resistance under radiation exposure.
Inconel 718 is preferred for applications requiring long-term mechanical stability, corrosion resistance, and fatigue performance at elevated temperatures. It is ideal for custom superalloy parts used in jet engines, turbines, and exhaust systems, where mechanical stress and thermal cycling are constant challenges.
The alloy’s versatility makes it suitable for aerospace and industrial applications, providing reliability in environments ranging from ocean floors to nuclear reactors. With its balance of machinability, weldability, and high-performance properties, Inconel 718 ensures durability and reduced downtime, meeting the critical needs of today’s demanding industries.