BS EN 2387 is a standard that serves technical specifications for Aluminium alloy 2014A T6 tubes for structures ensuring safety, performance, and structural integrity in aerospace applications.
BS EN 2387 specifies the requirements relating to Aluminium alloy 2014A tubes for structures in aerospace applications.
BS EN 2387 specifies delivery condition as T6 and method of melting as drawn tubes. BS EN 2387 sets a limit dimension range of 0.6 mm ≤ a ≤ 12.5 mm for aerospace applications.
BS EN 2387 on Aluminium alloy 2014A T6 tubes for structures applies to:
Aluminium has a long history and variety of applications in the aerospace industry. Aluminium is utilised to create the frames and components of aeroplanes, demonstrating its lightweight, strength, and corrosion resistance. Aluminium alloy is a high-grade alloy with outstanding fatigue resistance and high yield strength.
BS EN 2387 provides you guidance on chemical composition, method of melting, form, method of production, limit dimensions and technical specifications, which allows you to standardize the physical and chemical properties of aluminium alloys for aerospace applications.
BS EN 2387 provides you guidance on delivery conditions, heat treatment, use condition that facilitates transportation condition, storage and usability for aluminium alloy tubes for structures.
BS EN 2387 also provides you guidance on testing, including heat treatment, dimensions, cladding thickness, temperature, proof stress, strength, elongation, hardness, shear strength and bending, ensuring mechanical strength, performance, and longevity of aluminium alloys for aerospace applications.
Guidance in BS EN 2387 enables you to develop and assess Aluminium alloy 2014A T6 tubes for structures that ensure longevity and structural stability in aerospace applications.EN 2387:2018