BS EN 4632-006 is an international standard that discusses the weldability and brazeability of materials used in aerospace constructions.
BS EN 4632-006 defines degrees of weldability and brazeability for materials or families of materials used in aerospace applications.
BS EN 4632-006 comprises a series of sheets, by materials or by material family, which:
BS EN 4632-006 on homogeneous assemblies of titanium alloys for aerospace series is relevant to:
Titanium alloys contain traces of aluminium, zirconium, manganese, iron, chromium, cobalt, nickel, and copper.
BS EN 4632-006 contains the index of material sheets, classified by family based on the main element used in the chemical composition and on the alloy structure.
BS EN 4632-006 provides you with the degree of weldability or brazeability, advising you to select the thermal states that give the lowest degree in the operating cycle.
BS EN 4632-006 gives you the list of titanium alloys sheets, that assists with the characteristic features of the alloys. It covers all the requirements for homogeneous assemblies of titanium alloys.
BS EN 4632-006 creates a standardized approach for manufacturers of titanium alloys to adhere to if they supply their metallic materials for use by the aerospace and defence industry.
By adopting BS EN 4632-006, manufacturers can demonstrate the reliability of titanium alloys and build trust for their use throughout the aerospace supply chain.
EN 4632-006:2013