Inconel 718 alloy
Inconel 718 is a high-strength, corrosion-resistant nickel-chromium alloy known for its excellent mechanical properties at elevated temperatures. It is commonly used in aerospace, oil and gas, and other high-stress applications.
What is the difference between Inconel X750 and 718 springs?
nconel X750 and Inconel 718 are both nickel-based superalloys, but they have different compositions and properties that make them suitable for different applications. Here’s a comparison of the two, particularly in the context of spring materials:
1. Composition:
Inconel 718: Contains nickel (50-55%), chromium (17-21%), iron (up to 19%), molybdenum (2.8-3.3%), and niobium (4.75-5.5%). It also has small amounts of other elements like titanium and aluminum.
Inconel X750: Contains nickel (70-75%), chromium (14-17%), iron (5-9%), and significant amounts of titanium (1-2.5%) and aluminum (0.2-0.6%). It is primarily used in high-temperature applications.
2. Mechanical Properties:
Inconel 718: Known for its high strength, excellent fatigue resistance, and good ductility, particularly at elevated temperatures. It can be heat-treated to enhance its properties.
Inconel X750: Offers high strength and oxidation resistance at elevated temperatures, but it has lower ductility compared to Inconel 718. It is often used in applications that require stability under high-temperature conditions.
3. Corrosion Resistance:
Inconel 718: Excellent corrosion resistance, particularly in acidic and saline environments, making it suitable for aerospace and oil and gas applications.
Inconel X750: Also offers good corrosion resistance but is more focused on high-temperature oxidation resistance rather than resistance to acidic environments.
4. Applications:
Inconel 718: Commonly used in aerospace components, gas turbines, and springs that operate in high-stress and corrosive environments.
Inconel X750: Primarily used in gas turbine engines, nuclear reactors, and other high-temperature applications where stability and strength are critical.
5. Heat Treatment:
Inconel 718: Can be age-hardened to improve strength and hardness through specific heat treatment processes.
Inconel X750: Typically used in the solution-annealed condition; aging is less common as it is designed for stability rather than hardening.
Chemical Properties of Inconel 718
Nickel (plus Cobalt) .......................................................50.00-55.00
Chromium......................................................................17.00-21.00
Iron .....................................................................................Balance
Niobium (plus Tantalum)....................................................4.75-5.50
Molybdenum .....................................................................2.80-3.30
Titanium.............................................................................0.65-1.15
Aluminum ..........................................................................0.20-0.80
Cobalt ...............................................................................1.00 max.
Carbon..............................................................................0.08 max.
Manganese .......................................................................0.35 max.
Silicon ...............................................................................0.35 max.
Phosphorus.....................................................................0.015 max.
Sulfur...............................................................................0.015 max.
Boron ..............................................................................0.006 max.
Copper..............................................................................0.30 max
Density | 8.19g/cm³ | 0.296 lb/in³ |
Melting point | 1260-1336 | 2437°F |
Inconel series
Customize size as below
Shape | Size(mm) |
WIre | 0.5-7.5 |
Rod/Bar | 8.0-200 |
Strip | (0.5-2.5)*(5-180) |
Tube | custom made |
Plate | custom made |
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