Descripción
High temperature alloy Inconel 718, designed to operate at temperatures up to 980 ° C, one of the most common alloys in the Inconel family.
The alloy was initially used as a cladding material for supersonic aircraft. The hardening of the alloy is achieved due to the slow precipitation of the intermetallic compound of nickel with titanium and niobium. The alloy is easy to pressurize and weld well.
The alloy is used for the manufacture of compressor blades for aircraft engines, as well as other parts.
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