Inconel 718 Mechanical Properties

Inconel 718 Mechanical Properties

Inconel 718 is a nickel-chromium-molybdenum alloy known for its excellent mechanical properties, especially at high temperatures. Below are its main mechanical properties:
Element Content Range Function
Nickel (Ni) Approximately 50% - 55% It is the main matrix element of Inconel 718. Nickel can improve the strength, toughness, and corrosion resistance of the alloy, and endow the alloy with good high-temperature performance.
Chromium (Cr) Generally 17% - 21% Chromium can form a dense oxide film on the surface of the alloy, improving the oxidation resistance and corrosion resistance of the alloy, and enhancing the stability of the alloy in high-temperature and harsh environments.
Iron (Fe) About 18% - 21% Iron is an important constituent element of the alloy, which helps to improve the strength and toughness of the alloy, and at the same time reduces the cost.
Niobium (Nb) Usually 4.75% - 5.50% Niobium can form stable carbides with carbon, improving the strength and creep resistance of the alloy. Especially at high temperatures, it can effectively prevent grain growth and enhance the high-temperature mechanical properties of the alloy.
Molybdenum (Mo) Approximately 2.8% - 3.3% Molybdenum can improve the strength, hardness, and corrosion resistance of the alloy, especially having a significant effect on pitting corrosion and crevice corrosion resistance. It also helps to improve the high-temperature strength and toughness of the alloy.
Titanium (Ti) Between 0.65% - 1.15% Titanium can form a strengthening phase with nickel, improving the strength and hardness of the alloy. At the same time, it can also improve the welding performance of the alloy.
Aluminum (Al) Generally 0.20% - 0.80% Similar to titanium, aluminum can form a strengthening phase with nickel, improving the high-temperature strength and hardness of the alloy and enhancing the oxidation resistance of the alloy.

 

Inconel 718 is a nickel-chromium-molybdenum alloy known for its excellent mechanical properties, especially at high temperatures. Below are its main mechanical properties:

Mechanical Property Details
High-Temperature Strength Room Temperature:
Tensile Strength: Approximately 1270 - 1370 MPa
Yield Strength: Around 1000 - 1070 MPa
At 650°C:
Tensile Strength: Exceeds 900 MPa
Yield Strength: About 750 MPa
Fatigue Resistance Excellent fatigue resistance, can endure a large number of stress cycles without failure, suitable for components with cyclic loading (e.g., turbine blades, engine parts)
Creep Resistance Good creep resistance, low creep rate at 650°C under a given stress level, maintains dimensional stability and mechanical performance during long-term high-temperature service
Hardness After heat treatment, hardness can reach HRC 38 - 42, providing good wear resistance and surface strength
Toughness Good toughness, can absorb energy and resist cracking or brittle fracture under impact and other loading conditions, crucial for component reliability and safety

 

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