Material Name and Equivalent Names: Inconel 713 is called Alloy 713 and aligns with the American standard UNS N07713. It complies with ASTM B637 and GB/T 14992: GH713, with equivalents such as DIN/EN 2.4650, but it does not have British (BS) or AMS designations.
Inconel 713 is a high-strength nickel-based superalloy designed to operate at elevated temperatures. It exhibits outstanding thermal fatigue resistance and maintains its mechanical integrity during prolonged exposure to high temperatures.
Industries such as aerospace, power generation, and energy rely on Inconel 713 for components like turbine blades and vanes. The alloy's ability to withstand extreme heat and resist cyclic thermal fatigue makes it ideal for applications where long service life and minimal degradation are critical.
Alternative materials to Inconel 713 include Inconel 718, Rene 77, and Hastelloy X. Inconel 718 offers enhanced tensile strength but is more suitable for cryogenic conditions and lower operating temperatures. Rene 77 provides superior creep resistance but is more challenging to manufacture. Hastelloy X is ideal for chemical applications due to its oxidation resistance but lacks the high-temperature mechanical strength of Inconel 713.
Each alloy has unique advantages, but Inconel 713 stands out for high-temperature, cyclic applications in aerospace and power generation environments.
Inconel 713 is designed for long-lasting, high-temperature performance in components subject to thermal cycling and mechanical stress. With a nickel content of up to 76%, the alloy provides excellent oxidation resistance, while chromium enhances corrosion resistance at elevated temperatures. Titanium and aluminum improve strength through precipitation hardening, and niobium further stabilizes the microstructure to ensure durability during extended service.
The alloy’s ability to maintain mechanical properties at temperatures up to 982°C makes it suitable for turbine blades and other critical aerospace components.
The carefully balanced elements in Inconel 713 offer exceptional thermal fatigue resistance and mechanical strength, ensuring long-lasting performance in extreme environments.
Element | Composition (%) |
---|---|
Nickel (Ni) | 70.0 – 76.0 |
Chromium (Cr) | 12.0 |
Iron (Fe) | 0.2 |
Niobium (Nb) | 1.4 |
Aluminum (Al) | 0.6 |
Titanium (Ti) | 0.6 |
Inconel 713 offers a high melting point and excellent thermal conductivity, making it ideal for high-performance applications.
Property | Value |
---|---|
Density (g/cm³) | 8.11 |
Melting Point (°C) | 1325 |
Thermal Conductivity (W/(m·K)) | 11.1 |
Modulus of Elasticity (GPa) | 213 |
Inconel 713 features an austenitic, face-centered cubic (FCC) microstructure, which enhances its ductility and mechanical stability at elevated temperatures. The presence of aluminum and titanium facilitates precipitation hardening, forming a gamma prime (γ') phase that improves high-temperature strength and fatigue resistance.
The alloy also resists grain boundary precipitation, minimizing embrittlement during thermal cycling. This stable microstructure ensures Inconel 713 can perform reliably under long-term exposure to extreme heat, making it suitable for critical applications like turbine blades and vanes.
Inconel 713 offers exceptional mechanical strength and thermal fatigue resistance, ensuring reliability in high-stress environments.
Property | Value |
---|---|
Tensile Strength (MPa) | 1240 |
Yield Strength (MPa) | 1035 |
Creep Strength | High at 982°C / 10,000 hours |
Fatigue Strength (MPa) | 400 – 450 |
Hardness (HRC) | Rockwell C35 – 45 |
Elongation (%) | 10 |
Elastic Modulus (GPa) | ~210 |
1. High-Temperature Strength: Inconel 713 offers outstanding mechanical strength at elevated temperatures, which is ideal for components like turbine blades operating in extreme heat. It maintains a tensile strength of 1240 MPa and yield strength of 1035 MPa even under continuous exposure to temperatures up to 982°C.
2. Excellent Thermal Fatigue Resistance: The alloy is highly resistant to thermal fatigue, which ensures durability during cyclic temperature variations. This feature makes Inconel 713 ideal for gas turbines and jet engines, where components are exposed to fluctuating temperatures during operation.
3. Long Creep Life: With strong creep resistance at high temperatures, Inconel 713 offers a creep rupture life of 10,000 hours at 982°C, ensuring reliability in critical applications that require prolonged high-temperature exposure.
4. Oxidation and Corrosion Resistance: The high nickel and chromium content in Inconel 713 provides excellent resistance to oxidation and corrosion. This makes it suitable for harsh aerospace and power generation environments, where components are exposed to extreme heat and corrosive gases.
5. Stability in Cyclic Applications: Inconel 713 performs well in cyclic applications, maintaining mechanical integrity even after repeated thermal cycling. This ensures long-term reliability for components like turbine blades and vanes, reducing maintenance costs and downtime.
Inconel 713 is well-suited for Vacuum Investment Casting. The alloy’s excellent high-temperature strength and stability allow it to be cast with minimal oxidation, producing precise components for the aerospace and energy industries.
Inconel 713 is not ideal for Single Crystal Casting because the alloy’s mechanical properties are optimized for equiaxed grains rather than single-crystal structures required for advanced turbine blades.
Equiaxed Crystal Casting is a preferred process for Inconel 713. This method enhances the alloy’s fatigue resistance by producing uniform grain structures, making it suitable for components like turbine vanes.
The alloy can also be used in Superalloy Directional Casting, where controlled grain orientation improves creep resistance, which is essential for components exposed to prolonged high-temperature service.
Powder Metallurgy Turbine Disc is unsuitable for Inconel 713, as its properties are better retained through casting than powder metallurgy processes.
Superalloy Precision Forging can enhance the alloy’s strength, but Inconel 713 is primarily used in cast forms for components requiring precise high-temperature performance.
Superalloy 3D Printing is not commonly used with Inconel 713 due to challenges in maintaining mechanical properties during additive manufacturing.
Inconel 713 is well-suited for CNC Machining, though advanced tooling is required to manage its hardness and prevent tool wear during machining.
The alloy supports Superalloy Welding, though preheating and post-weld heat treatments are recommended to avoid cracking and maintain mechanical strength.
Hot Isostatic Pressing (HIP) can improve Inconel 713’s density and eliminate internal voids, enhancing fatigue and creep resistance for critical aerospace applications.
In Aerospace and Aviation, Inconel 713 is used for turbine blades, vanes, and exhaust systems due to its ability to withstand extreme temperatures and thermal cycling.
In Power Generation, the alloy is employed in gas turbines and heat exchangers, ensuring reliable performance under continuous high-temperature exposure.
In the Oil and Gas industry, Inconel 713 provides corrosion resistance for components in high-temperature environments, such as downhole tools and exhaust manifolds.
The alloy is essential in the Energy sector and is used in gas turbines and exhaust systems, ensuring high performance under fluctuating temperatures.
For Marine applications, Inconel 713 offers excellent oxidation resistance and durability, making it suitable for components in marine turbines and exhausts.
In Mining, the alloy is used in high-performance pumps and equipment exposed to abrasive and high-temperature environments.
In the automotive industry, the alloy is applied to turbochargers and high-performance exhaust systems where heat resistance is essential.
For Chemical Processing, Inconel 713 is used in reactors and heat exchangers due to its resistance to oxidation and chemical corrosion.
In the Pharmaceutical and Food industries, the alloy is used in valves and heat exchangers to prevent contamination and ensure corrosion resistance.
In Military and Defense, Inconel 713 is employed in missile components and jet engines, providing reliable performance under extreme conditions.
In the Nuclear sector, the alloy’s thermal stability and creep resistance make it ideal for reactors and high-temperature steam systems.
Inconel 713 is ideal for applications requiring exceptional strength and stability at elevated temperatures. Its outstanding thermal fatigue resistance makes it a preferred material for custom superalloy parts in gas turbines, jet engines, and exhaust systems.
The alloy’s ability to maintain mechanical properties at temperatures up to 982°C ensures long-lasting performance, reducing downtime and maintenance. Inconel 713 offers a balance of oxidation resistance and mechanical integrity, making it a versatile option for aerospace, power generation, and chemical processing industries.