BS EN 2475 is a standard that serves technical specifications for Aerospace series: Steel 30CrNiMo8 (1.6580) bar for machining that ensures structural durability, hardness and corrosion resistance in aerospace applications.
BS EN 2475 specifies the requirements relating to Steel 30CrNiMo8 (1.6580) bar for machining for aerospace applications.
BS EN 2475 specifies the method of melting as air melted and delivery condition as hardened and tempered. BS EN 2475 also defines a tensile strength range of 1100 MPa ≤ Rm ≤ 1300 MPa and limit dimension (De) ≤ 100 mm for aerospace applications.
BS EN 2475 on Aerospace series: Steel 30CrNiMo8 (1.6580) bar for machining applies to:
Stainless steel is one of the most commonly used metals in aerospace equipment. Steel has mechanical properties such as corrosion resistance, strength, and toughness, making it a reliable option for use in the aerospace industry.
BS EN 2475 provides you guidance on chemical composition, method of melting, form, method of production, limit dimension and technical specifications, which allows you to ensure corrosion resistance and heat resistance in aerospace applications.
BS EN 2475 provides you guidance on delivery condition, heat treatment, delivery condition code, use condition and heat treatment that facilitates transportation condition, storage, and usability of steel bar for machining.
BS EN 2475 provides you guidance on testing, including heat treatment, dimensions, temperature, proof stress, strength, elongation, hardness, shear strength and bending, ensuring mechanical strength and operability and longevity in aerospace applications.
Guidance in BS EN 2475 enables you to develop and assess Steel 30CrNiMo8 (1.6580) bar for machining that ensures operation stability and structural integrity in aerospace applications.EN 2475:2018