BS EN 2465 is a metallic material standard that covers technical specifications for steel X2CrNi18-9 (1.4307) bars for machining in aerospace applications that ensure quality, performance and longevity at variable temperatures and stresses.
BS EN 2465 specifies the requirements relating to Steel X2CrNi18-9 (1.4307) bars for machining. It is softened steel with a tensile strength range of 450 MPa ≤ Rm ≤ 680 MPa and a limit dimension of 4 mm ≤ De ≤ 100 mm for aerospace applications.
BS EN 2465 on steel X2CrNi18-9 (1.4307) bars for machining in aerospace applications 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 which make it a reliable option for use in aerospace industry.
BS EN 2465 provides you guidance on chemical composition, method of melting, form, method of production, limit dimensions, and technical specifications which enables standardization of steel bars that enhances performance, corrosion resistance and mechanical properties.
BS EN 2465 provides you guidance on delivery condition, heat treatment, delivery condition code, use condition and heat treatment that facilitates transportation condition, storage and application for steel bars.
BS EN 2465 also provides you guidance on testing which includes heat treatment, dimensions, thickness of cladding, temperature, proof stress, strength, elongation, hardness, shear strength and bending that ensures mechanical strength and operability of steel bars for the purpose of machining.
Guidance in BS EN 2465 allows you to develop and assess steel X2CrNi18-9 (1.4307) bars for machining in aerospace applications which ensures the operational safety and performance in aerospace components.
BS EN 2465:2019 supersedes BS EN 2465:2007, which is now withdrawn.
EN 2465