INCONEL ALLOYS

INCONEL 718 A precipitation-hardenable nickel-chromium alloy that combines High Strength and Corrosion resistance with an excellent creep-rupture strength.
Langley Alloys Standard 718 material is Double Vacuum melted with restricted (Ta-Nb) to eliminate Delta phase within the alloy and supplied in the Hot Worked and Aged condition to meet Oil industry requirement of API6a 718
Alloy 625 (INCONEL) A nickel-chromium-molybdenum alloy with an addition of niobium that acts with the molybdenum to stiffen the alloy’s matrix and thereby provide strength without an ageing heat treatment. The alloy resists a wide range of severely corrosive environments and is especially resistant to pitting and crevice corrosion. Used in chemical processing, aerospace, offshore and marine engineering.

Alloy	Common Name	Related Specifications			Tensile Strength	Proof Stress	Elongation
Alloy	Common Name	British	European	United States	Tensile Strength	Proof Stress	Elongation
Alloy 718	INCONEL 718			ASTM B637 N07718, API 6A 718	1034 [150]	862 [125]	20
Alloy 625	INCONEL 625	BS 3076 NA21		ASTM B564, B446 N06625	758 [110]	344 [49.9]	60

LANGALLOY^® is a registered Trade Mark of Langley Alloys Ltd; MONEL^® and INCONEL^® are registered Trade Marks of Special Metals Corporation

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