BS EN 2119 is a metallic material standard that serves technical specifications for the Aerospace series: Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) wires that enhance safety and performance in high-temperature conditions.
BS EN 2119 specifies the requirements relating to Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) wires for rivets. BS EN 2119 sets the delivery and use conditions as solution treated and precipitation treated.
BS EN 2119 sets a limit dimension range of 2 mm ≤ D ≤ 10 mm and tensile strength of Rm ≥ 960 MPa for aerospace applications.
BS EN 2119 on Aerospace series: Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) wires applies to:
Heat-resistant alloys are the recommended material for usage in hot sections of aircraft engines. They provide high strength and the ability to work at high temperatures. They are the main components of aerospace alloys used for engine blocks and other components. At high temperatures, these alloys have a strong creep resistance and strength.
BS EN 2119 provides you guidance on chemical composition, method of melting, form, method of production, limit dimension and technical specifications that allows you to ensure corrosion resistance and heat resistance in aerospace applications.
BS EN 2119 provides you guidance on delivery condition, heat treatment, delivery condition code, use condition and heat treatment that facilitates transportation condition, storage and usability for heat-resisting alloys.
The adoption of BS EN 2119 enables users to develop and assess heat-resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) wires that ensure safe operability, longevity and performance in high-temperature conditions.
EN 2119:2017