BS EN 3018 is a metallic material standard that serves technical specifications for the Aerospace series: Heat resisting alloy NI-PH2801 (NiCr16Fe7Ti3Nb1Al1) wires that enhance load-bearing capacity and heat resistance in aerospace applications.
BS EN 3018 specifies the requirements relating to Heat resisting alloy NI-PH2801 (NiCr16Fe7Ti3Nb1Al1) in wire form.
BS EN 3018 specifies a cold drawn method of production and a consumable electrode method as a method of melting. BS EN 3018 sets a limit dimension of D ≤ 3 mm for aerospace applications.
BS EN 3018 on Aerospace series: Heat resisting alloy NI-PH2801 (NiCr16Fe7Ti3Nb1Al1) wires applies to:
Heat resistant alloys provide high strength and the ability to work at high temperatures. They are the main components of aerospace alloys used for engine blocks and many other parts. At high temperatures, these alloys have a strong creep resistance and strength.
BS EN 3018 provides you guidance on chemical composition, method of melting, form, method of production, limit dimension and technical specifications, ensuring corrosion resistance and heat resistance in aerospace applications.
BS EN 3018 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 wires.
Guidance in BS EN 3018 enables you to develop and assess Heat resisting alloy NI-PH2801 (NiCr16Fe7Ti3Nb1Al1) wires that ensure longevity and reliability in thread inserts.
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