Inconel x750

Description

Designed for high-temperature strength and oxidation resistance, this nickel-chromium alloy contains titanium and aluminum for precipitation hardening. Inconel X-750 maintains strength up to 700°C and is used in turbines, rocket engines, and other high-stress systems.

Application:

Jet engine components
Control rods
Turbocharger components
Heat exchangers
Springs
Aerospace components

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Product Specification

Chemistry Composition

Carbon	0.08 max
Manganese	1.00 max
Sulfur	0.01 max
Silicon	0.50 max
Chromium	14.00 – 17.00
Niobium + Tantalum	0.70 – 1.20
Titanium	2.25 – 2.75
Aluminum	0.40 – 1.00
Iron	5.00 – 9.00
Cobalt	1.00 max
Copper	0.50 max
Nickel	70.00 min