Material Name and Equivalent Names: Inconel 718C, or Alloy 718C, complies with UNS N07718 and follows ASTM B637 standards. Its German designation is DIN/EN 2.4668, and it is listed in China as GH4169C under GB/T 15059.
Inconel 718C is a high-performance nickel-chromium superalloy designed for applications requiring exceptional strength, fatigue resistance, and thermal stability. It performs reliably at temperatures ranging from 700°C to 800°C, making it a preferred material for aerospace engines, turbines, and power generation systems.
The alloy’s creep resistance and long service life at elevated temperatures ensure that it meets the demands of industries that require sustained operation under extreme mechanical stress. Its versatility and robust mechanical properties make it valuable in various critical environments, from jet engines to nuclear reactors.
Alternatives to Inconel 718C include Waspaloy, Rene 41, and Hastelloy X. Waspaloy offers superior thermal stability but has limited weldability. Rene 41 provides enhanced creep resistance but is more challenging to machine. Hastelloy X delivers excellent oxidation resistance but slightly lower strength at elevated temperatures.
Inconel 718C is favored in applications where a combination of strength, corrosion resistance, and long-term fatigue performance is essential. Its ease of fabrication and weldability give it an edge over other superalloys for high-performance applications.
Inconel 718C is designed to provide exceptional strength and fatigue resistance at high temperatures, specifically for components subjected to thermal cycling. The alloy's nickel base ensures thermal stability, while chromium and molybdenum resist corrosion. Niobium and titanium strengthen the alloy through precipitation hardening, improving long-term mechanical performance.
The design focus of Inconel 718C was to develop a material that could withstand prolonged exposure to high temperatures without losing mechanical integrity. This makes it suitable for aerospace engines, gas turbines, and nuclear reactors, where reliability and durability are critical.
The carefully balanced composition of Inconel 718C ensures excellent mechanical properties, corrosion resistance, and thermal 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 718C offers outstanding thermal conductivity, strength, and density, enabling it to maintain mechanical integrity under harsh conditions.
Property | Value |
---|---|
Density (g/cm³) | 8.19 |
Melting Point (°C) | 1260 |
Thermal Conductivity (W/(m·K)) | 11.4 |
Modulus of Elasticity (GPa) | 205 |
Inconel 718C has a stable austenitic structure, strengthened through precipitation hardening. The formation of gamma prime (γ') and gamma double prime (γ'') phases enhances the alloy's resistance to creep and thermal fatigue. These phases prevent grain boundary sliding, ensuring the alloy retains its mechanical properties at high temperatures.
The microstructure of Inconel 718C remains stable during long-term exposure to elevated temperatures, providing high fatigue resistance. The alloy’s niobium and titanium content ensures excellent precipitation hardening, contributing to its ability to withstand continuous thermal and mechanical stress.
Inconel 718C offers high tensile strength, fatigue resistance, and excellent creep rupture life, ensuring durability under extreme conditions.
Property | Value |
---|---|
Tensile Strength (MPa) | 1280 |
Yield Strength (MPa) | 1100 |
Creep Strength | Effective at 700°C |
Fatigue Strength (MPa) | 450 |
Hardness (HRC) | Rockwell C40 – 45 |
Elongation (%) | 15 – 20 |
Elastic Modulus (GPa) | ~210 |
1. High-Temperature Strength: Inconel 718C retains exceptional tensile strength and mechanical integrity at temperatures up to 800°C, making it ideal for gas turbines and jet engines.
2. Superior Fatigue Resistance: The alloy offers outstanding fatigue resistance, ensuring reliable performance under cyclic thermal loads in critical aerospace and power generation applications.
3. Long Creep Rupture Life: With a creep rupture life of over 20,000 hours at 700°C, Inconel 718C provides long-term durability, reducing the need for frequent maintenance.
4. Excellent Corrosion and Oxidation Resistance: The high chromium content offers superior corrosion resistance, making the alloy suitable for marine and chemical environments.
5. Ease of Fabrication and Weldability: Inconel 718C can be easily machined and welded, providing flexibility in manufacturing complex components for aerospace and industrial use.
Inconel 718C is an excellent candidate for Vacuum Investment Casting. Its superior strength and corrosion resistance make it suitable for precision parts requiring minimal defects and high performance, such as turbine components.
However, Single Crystal Casting is not typically used for Inconel 718C. The alloy’s precipitation-hardening characteristics make it more effective with grain structures rather than single-crystal designs.
In Equiaxed Crystal Casting, Inconel 718C’s uniform grain structure offers excellent fatigue resistance, ensuring high reliability for critical aerospace and power generation components.
Superalloy Directional Casting is an appropriate process for Inconel 718C, providing enhanced creep resistance and durability for components operating at high temperatures.
Inconel 718C is not commonly used for Powder Metallurgy Turbine Disc manufacturing, as traditional casting and forging methods generally offer better mechanical properties.
The alloy is highly effective in Superalloy Precision Forging, enhancing its mechanical strength, creep resistance, and fatigue performance under high stress.
While Inconel 718C is not widely employed in Superalloy 3D Printing, advances in additive manufacturing may expand its potential.
In CNC Machining, Inconel 718C performs well with proper tooling and coolant management, ensuring precision and preventing work hardening during machining.
The alloy offers excellent weldability in Superalloy Welding, with minimal cracking or distortion, making it ideal for aerospace and industrial applications.
In Hot Isostatic Pressing (HIP), Inconel 718C achieves enhanced mechanical properties by eliminating porosity and improving fatigue life, which is critical for high-performance industries.
In Aerospace and Aviation, Inconel 718C is widely used for jet engine parts, turbine blades, and exhaust systems, delivering excellent fatigue resistance and thermal stability.
In Power Generation, the alloy’s strength at elevated temperatures makes it ideal for gas turbines and heat exchangers, ensuring efficient and long-lasting performance.
In the Oil and Gas industry, Inconel 718C is used for flow control equipment and downhole tools, offering excellent corrosion resistance under harsh conditions.
In Energy applications, Inconel 718C ensures reliable operation in reactors and turbines, reducing downtime and maintenance costs.
In the Marine sector, the alloy’s resistance to seawater corrosion makes it suitable for exhaust systems, pumps, and valves exposed to marine environments.
In Mining, the alloy offers durability and strength for critical components such as valves and pump housings subjected to wear and high temperatures.
In the Automotive industry, Inconel 718C is used for turbochargers and exhaust systems, providing heat resistance and durability for high-performance vehicles.
In Chemical Processing, the alloy’s corrosion resistance makes it ideal for reactors, heat exchangers, and piping systems handling aggressive chemicals.
In Pharmaceutical and Food industries, Inconel 718C ensures clean processing environments by resisting corrosion and contamination.
In Military and Defense, the alloy provides strength and reliability in missile systems, jet engines, and military equipment exposed to high stress.
In the Nuclear industry, Inconel 718C is used for reactor components, offering long-term stability under radiation and thermal exposure.
Inconel 718C is ideal for applications requiring superior mechanical strength, fatigue resistance, and corrosion protection at elevated temperatures. It is especially suitable for custom superalloy parts in aerospace engines, turbines, and energy systems, where consistent performance and reliability are critical.
The alloy excels in environments that involve thermal cycling, high mechanical stress, and exposure to corrosive elements. Whether in jet engines, nuclear reactors, or marine applications, Inconel 718C offers the durability and strength required to ensure long service life and reduced downtime, making it a preferred material across multiple industries.