Abstract
Despite the undisputed dominance of composite materials in the construction of lightweight aircraft, steel structures still find use - especially for engine mounts. Weight reduction of the structure is achieved through the use of tubular trusses, usually made of structural steel for tempering. An increasing number of requirements for this type of construction and the development of steel metallurgy provide the basis for the introduction of new steel grades. This paper presents the testing results of a welded truss made of advanced 15CDV6 steel as a potential replacement for 30HGSA steel. The microstructure and hardness of characteristic zones of TIG-welded joints are discussed, as well as the results of static tensile testing of the parent material and welded joints.
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