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High temperature nickel alloy powder IN718

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High temperature nickel alloy powder IN718

High-temperature nickel alloy 718, produced in accordance with UNS N07718, AMS5662, AMS5664, W.Nr 2.4668 and DIN Nicr19Fe19NbMo3 standards, is a precipitation hardened nickel-chromium alloy that retai
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High-temperature nickel alloy 718, produced in accordance with UNS N07718, AMS5662, AMS5664, W.Nr 2.4668 and DIN Nicr19Fe19NbMo3 standards, is a precipitation hardened nickel-chromium alloy that retains good tensile strength, fatigue strength, creep at 700 ° C Strength and crack strength, good corrosion resistance, suitable for the manufacture of high temperature conditions used in various parts, such as gas turbine components, instrumentation components, energy industrial components, the material also has strong resistance to low temperature performance, can be used for a variety of Low temperature function

Industrial Specifications: UNS N07718, AMS5662, AMS5664, W.Nr 2.4668 and DIN Nicr19Fe19NbMo3

Chemical composition (wt%): Chromium 17.0-21.0; Manganese 0.35max; Molybdenum 2.8-3.3; Silicon 0.35max; Titanium 0.65-1.15; Phosphorus 0.015max; Aluminum 0.2-0.8; Sulfur 0.015max; Cobalt 1max; Boron 0.006max; Carbon 0.08max; copper 0.3max; nickel 50-55; niobium + tantalum 4.75-5.50; balance iron.

Applicable equipment: EOS, Renishaw, Concept Laser, SLM Solutions, Arcarm and other domestic equipment.

Features:

● heat.

● anti-corrosion.

● In the high temperature up to 700 degrees, to maintain good tensile strength, fatigue resistance, creep strength and crack strength.

● The method of precipitation hardening heat treatment can achieve post-hardening. Can be cutting, discharging, welding, forging, polishing and coating processing.

Uses:

● Functional model.

● Mass production of parts.

● aerospace.

● High-temperature turbine components.

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