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ATI Allvac® Nickelvac® X-750 Nickel Superalloy, Heat Treatment: 982°C (1800°F) + Age
Categories: Metal; Nonferrous Metal; Nickel Alloy; Superalloy

Material Notes: Data provided by Allvac.

Applications: Turbine, engine components. Blades, vanes, fasteners, springs, bellows. Extrusion dies, nuclear, heat treating, forming tools.

Key Words: Allvac, an Allegheny Teledyne Company, UNS N07750; AMS 5667, 5668, 5669, 5670, 5671. MIL-N-24114, ASTM B 637
Vendors: Visit metalmen for your metals needs. Products include special chemistry, tight tolerances, custom tempers, odd dimensions/forms, and small quantities. Phone 1-800-767-9494.

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Physical PropertiesOriginal ValueComments
Density 8.30 g/cc
 
Mechanical PropertiesOriginal ValueComments
Hardness, Brinell 326Estimated from Rockwell C value for Brinell test with 3000 kg load/10 mm diameter ball
Hardness, Knoop 354Estimated from Rockwell C value.
Hardness, Rockwell C 35
Hardness, Vickers 341Estimated from Rockwell C value.
Tensile Strength, Ultimate 1207 MPa
Tensile Strength, Yield 793 MPa
@Strain 0.2 %
Elongation at Break 20 %
Reduction of Area 20 %
 
Component Elements PropertiesOriginal ValueComments
Aluminum, Al 0.70 %
Carbon, C 0.040 %
Chromium, Cr 15.5 %
Iron, Fe 7.0 %
Nickel, Ni >= 70 %as balance
Niobium, Nb (Columbium, Cb) 0.95 %
Titanium, Ti 2.5 %

Some of the values displayed above may have been converted from their original units and/or rounded in order to display the information in a consistent format. Users requiring more precise data for scientific or engineering calculations can click on the property value to see the original value as well as raw conversions to equivalent units. We advise that you only use the original value or one of its raw conversions in your calculations to minimize rounding error. We also ask that you refer to MatWeb's terms of use regarding this information. Click here to go back to viewing the property data in MatWeb's normal format.

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NALL10 / 14778

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