BS EN 4376 is a standard that serves technical specifications for Heat resisting alloy NiCr19Fe19Nb5Mo3 (2.4668) that enhance safety and performance in high-temperature conditions.
BS EN 4376 specifies the requirements relating to Heat resisting alloy NiCr19Fe19Nb5Mo3 (2.4668) bars and sections for aerospace applications. BS EN 4376 specifies delivery and use conditions as solution treated and precipitation treated.
BS EN 4376 sets the limit dimension range of De ≤ 200 mm for aerospace applications.
BS EN 4376 on Heat resisting alloy NiCr19Fe19Nb5Mo3 (2.4668) 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 4376 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 4376 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 alloy bars and sections.
The adoption of BS EN 4376 allows users to develop and assess heat-resisting alloy NiCr19Fe19Nb5Mo3 (2.4668) bars and sections that ensure safe operability, longevity and performance in high-temperature conditions.EN 4376:2016