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The specification of X10CrNiMoTi1810 steel is as follows:
1. Chemical Composition:
– Carbon (C): 0.08%
– Silicon (Si): 1.00%
– Manganese (Mn): 2.00%
– Phosphorous (P): 0.045%
– Sulfur (S): 0.030%
– Chromium (Cr): 16.00 – 18.00%
– Nickel (Ni): 11.00 – 14.00%
– Molybdenum (Mo): 2.00 – 3.00%
– Titanium (Ti): 0.70 – 1.00%
2. Mechanical Properties:
– Tensile Strength: 690 – 890 MPa
– Yield Strength: 590 MPa
– Elongation: 22%
– Hardness: 24 HRC (Rockwell hardness)
X10CrNiMoTi1810 steel is an indispensable material in the aerospace industry due to its excellent combination of mechanical properties and chemical composition. It offers high tensile strength, good yield strength, and superior elongation, making it suitable for various applications in aircraft components, such as structural parts, landing gears, engine components, and fasteners.
The chemical composition of X10CrNiMoTi1810 steel plays a crucial role in its performance. The presence of Chromium provides corrosion resistance, Nickel enhances the material’s strength and toughness, and Molybdenum improves the steel’s high-temperature strength and resistance to pitting and crevice corrosion. Additionally, the inclusion of Titanium aids in stabilizing the steel’s structure and enhancing its oxidation resistance.
Overall, X10CrNiMoTi1810 steel is highly sought after in the aerospace industry due to its exceptional mechanical properties and chemical composition, making it an indispensable material for critical applications.
X10CrNiMoTi1810 Steel grade
1698807132