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Views: 2 Author: Site Editor Publish Time: 2025-07-09 Origin: Site
JN Company supplies premium Inconel 718 superalloy in versatile forms including sheet, plate, bar, round bar, tube, pipe, wire, fasteners, and pipe fittings. We guarantee material quality compliant with AMS 5662/5663 standards, backed by full traceability and precision heat treatment. Enjoy competitive pricing with volume discounts on raw stock and engineered components. Our services feature low MOQs, rapid prototyping, and global logistics support. Trust JN for reliable Inconel 718 solutions tailored for aerospace, oil & gas, and high-stress applications.
Inconel 718 is a nickel-chromium superalloy renowned for its exceptional strength, corrosion resistance, and versatility in extreme environments. Also called 718 Inconel, it retains mechanical properties at temperatures up to 700°C, making it ideal for aerospace, oil and gas, and chemical industries. This overview covers its composition, properties, forms, pricing, and applications.
Inconel 718 primarily composed of Nickel and Chromium, it forms a solid foundation. Chromium provides excellent oxidation and corrosion resistance. Crucially, significant additions of Niobium and smaller amounts of Molybdenum, Titanium, and Aluminum enable a powerful strengthening mechanism called precipitation hardening. Fe is also balance, making it a more cost-effective than some purer nickel alloys. Understanding the Inconel 718 composition or 718 Inconel composition is key before you buy:
Inconel 718 (UNS N07718) | |||||||
C | Si | Mn | P | S | Cr | Ni | Mo |
≤0.08 | ≤0.35 | ≤0.35 | ≤0.015 | ≤0.015 | 17-21 | 50-55 | 2.8-3.3 |
Co | Nb | Al | Ti | B | Mg | Cu | Fe |
≤1.0 | 4.75-5.5 | 0.2-0.8 | 0.65-1.15 | ≤0.006 | - | ≤0.30 | Remain |
Inconel 718 Density: The density of Inconel 718 is approximately 0.297 lb/in³ (8.19 g/cm³). This Inconel 718 density or 718 Inconel density is a fundamental physical constant for the alloy, important for weight calculations.
Inconel 718 Melting Point: The melting point of Inconel 718 ranges between 2300°F - 2460°F (1260°C - 1350°C). This Inconel 718 melting point or melting point Inconel 718 defines its upper processing limits and resistance to heat. Its melting temperature is exceptionally high.
Inconel 718 Thermal Conductivity: Thermal conductivity is relatively low, around 6.5 - 11.7 W/m·K depending on temperature. This means heat doesn't flow through it easily, which can be an advantage (insulation) or disadvantage (heat buildup during machining).
Inconel 718 Hardness: Hardness varies significantly depending on heat treatment. In the annealed condition, it's typically around Rockwell B 85-95. After full aging (precipitation hardening), it achieves impressive hardness, often Rockwell C 35-45 (Inconel 718 hardness, 718 Inconel hardness). This directly impacts wear resistance and machinability.
Inconel 718 Yield Strength: This is a critical measure of its load-bearing capacity. The yield strength of aged Inconel 718 is exceptionally high, typically ≥ 120 ksi (825 MPa) at room temperature, and remains strong even at elevated temperatures (yield strength Inconel 718).
Tensile Strength: Typically ≥ 150 ksi (1035 MPa) at room temperature after aging.
Elongation: Around 12-20% in the aged condition, indicating good ductility for a high-strength alloy.
JN supplies premium Inconel 718 superalloy in versatile forms including sheet, plate, bar, round bar, tube, pipe, wire, fasteners, and pipe fittings. Enjoy competitive pricing with volume discounts on raw stock and engineered components. Request a quote today at Info@jnalloy.com.
Excellent Strength
Alloy 718 provides strength and reliability at extremely high temperatures, maintaining good structural properties at temperatures up to 1600 degrees Fahrenheit. It is precisely because of its excellent high temperature resistance that Inconel 718 is very suitable for use in aircraft, especially in engine positions.
Oxidation and Corrosion Resistance
Inconel 718 alloy has excellent resistance to extremely high pressure environments, such as pressure vessels, rocket engines, gas turbines, etc. Inconel 718 alloy can also be precipitation hardened with aluminum or titanium, so it can withstand high oxidation and corrosion, which is common in many parts of aircraft.
Low Expansion Properties
Inconel 718 has an extremely low coefficient of thermal expansion at 260°C, which allows the alloy to always maintain its shape and strength. Common applications include as a manufacturing tool for composites in the aerospace industry, and pipelines for storing and transporting liquefied gases.
Creep resistance
Inconel 718 nickel alloy has very good creep resistance. It can remain tough under high stress and at temperatures up to 850°C, making it extremely useful for the manufacture of turbine rotors in aircraft engines and exhaust valves for internal combustion engines.
While strong in the annealed state, Inconel 718 achieves its maximum capabilities through a specific heat treatment process known as precipitation hardening or aging:
Solution Annealing: Typically performed around 1700-1850°F, followed by rapid cooling. This dissolves the strengthening phases and softens the alloy for fabrication.
Aging: A two-step process is standard:
Hold at 1325°F ±25°F for 8 hours.
Furnace cool to 1150°F ±25°F.
Hold at 1150°F ±25°F for a total aging time of 18 hours including cool-down time.
Air cool.
This aging sequence precipitates fine γ' and gamma double γ'' phases within the matrix, dramatically increasing strength and hardness while maintaining good toughness. Precise control of the heat treatment is paramount for achieving the desired Inconel 718 material properties.
Composition Comparison
Inconel 718 Composition: Higher Fe, Nb, Ti, Al. Forms the γ'' (Ni₃Nb) phase during heat treatment, enabling exceptional precipitation hardening. This gives it superior yield strength and tensile strength.
Inconel 625 Composition: Higher Ni and Mo, with some Nb. Achieves strength primarily through solution strengthening. It is typically used in the annealed condition and does not require aging for corrosion resistance.
Mechanical Properties Comparison
Strength: Inconel 718 has significantly higher yield strength up to 1100 MPa / 160 ksi at RT and tensile strength than Inconel 625.
Creep and Fatigue: Inconel 625 offers superior creep resistance and fatigue strength at temperatures above 700°C due to its high Mo content and solution-strengthened structure. Inconel 718 excels in creep and fatigue below 650°C but loses significant strength above this as the γ'' phase dissolves.
Hardness: Aged Inconel 718 hardness 35-47 HRC is higher than annealed Inconel 625 hardness.
Corrosion Resistance Comparison
Inconel 625 is generally superior, particularly for seawater, brine, and acidic chloride environments. Oxidation resistance at very high temperatures.
Inconel 718 offers very good resistance to:
High-temperature oxidation and sulfidation.
Acidic environments.
Stress-corrosion cracking in chloride solutions.
Fabrication Comparison
Machining: Machining Inconel 718 is very difficult. It requires rigid setups, sharp carbide tools, low speeds, high feeds, and ample coolant. Machining Inconel 625 is easier due to less work hardening.
Welding: Inconel 718 has excellent weldability without post-weld heat treatment cracking, a major advantage over many other high-strength superalloys. Inconel 625 is also readily weldable but can be more susceptible to microfissuring in highly restrained joints.
Heat Treatment: Inconel 718 requires a specific solution annealing and aging heat treatment to achieve its peak strength. Inconel 625 is typically used in the solution-annealed condition; aging is not standard method and can reduce ductility.
High Temperature Performance Comparison
For high yield and fatigue strength up to 650-700°C, Inconel 718 is ideal.
For corrosion/oxidation resistance or moderate strength from above 700°C up to 980°C, Inconel 625 performs better.
Both alloys perform well at low temperatures.
The price of Inconel 718 is significantly higher than that of ordinary stainless steel. Its price changes are mainly related to raw material costs, product form, size, and purchase quantity.
Inconel 718 price per kg or Inconel 718 price per pound are common queries. While exact current prices require supplier quotes, expect costs to be several times higher than 304 stainless steel. The following is a price list of different 718 products from JN Alloys:
Form | Price per kg | Price per Pound | Key Influencing Factors |
Inconel 718 Billet/Ingot | 35–35–50 USD | 16–16–23 USD | Nickel market volatility, order volume |
Inconel 718 Bar/Round Bar | 40–40–65 USD | 18–18–30 USD | Diameter, tolerance, surface finish |
Inconel 718 Sheet/Plate | 45–45–70 USD | 20–20–32 USD | Thickness (thin sheet costs more) |
Inconel 718 Tube/Tubing | 55–55–85 USD | 25–25–39 USD | Wall thickness, OD precision |
Inconel 718 Wire | 60–60–90 USD | 27–27–41 USD | Diameter, spool size |
Inconel 718 Fasteners | 70–70–120 USD | 32–32–55 USD | Complexity (e.g., bolts vs. custom nuts) |
Inconel 718 Custom Stamped Parts | 90–90–200+ USD | 41–41–90+ USD | Design complexity, tooling, lot size |
Note: The above prices are for reference only. Please contact our sales team for the actual prices.
JN supplies premium Inconel 718 superalloy in versatile forms including sheet, plate, bar, round bar, tube, tubing, wire, fasteners, and pipe fittings. Enjoy competitive pricing with volume discounts on raw stock and engineered components. Request a quote today at Info@jnalloy.com.
