DIN EN 4632-004
Aerospace series - Weldability and brazeability of materials in aerospace constructions - Part 004: Welding and brazing of homogeneous assemblies of high alloyed steels; German version EN 4632-004:2012
Luft- und Raumfahrt - Schweißbarkeit und Lötbarkeit von Werkstoffen im Luft- und Raumfahrzeugbau - Teil 004: Schweißen und Löten gleichartiger Verbindungen aus hochlegierten Stählen; Deutsche Fassung EN 4632-004:2012
Overview
This standard specifies the degree of weldability and brazeability of materials or material families used in the aerospace industry. It comprises a series of sheets, classified by materials or material family, which: - indicate the main titles, the typical chemical composition and the main characteristics; - contain recommendations for welding and brazing; - indicate a degree of weldability or brazeability for a given process under defined conditions; - indicate a value for the welded joint mechanical resistance coefficient for each welding process when extracted from relevant bibliographical references. Joint coefficient is the ratio of stress resistance transversally to welded joint over tensile strength of parent alloy. It recommends ISO/TR 17671-3 and EN 1011-3 for pre-heating conditions specially for the welding of martensitic steels. These conditions depend on the line energy of welding, thickness, arc welding process and of hydrogen rate in filler metal. It applies unreservedly to the manufacturing of new parts or for repair. The committee responsible for this standard is NA 092-00-17 AA "Schweißen im Luft- und Raumfahrzeugbau (DVS AG A 9)" ("Welding in aerospace (DVS AG A 9)") at DIN.
Document: references other documents
Document: referenced in other documents
Responsible national committee
NA 092-00-17 AA - Welding in aerospace (DVS AG A 9)
