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ATI Allvac® 718Plus™ Nickel Superalloy
Categories: Metal; Nonferrous Metal; Nickel Alloy; Superalloy

Material Notes: Allvac 718Plus alloy (UNS N07818) is a precipitation hardened nickel-base material that exhibits high temperature tensile strength and stress rupture performance. This alloy is designed to have the high temperature capability and thermal stability of Waspaloy ally while retaining the processing characteristics of 718 alloy. It is double vacuum melted (VIM/ESR/VAR). This VIM/VAR process ensures excellent microcleanliness and tight compositional control. Triple melting, with electroslag remelting between the VIM and VAR operations, minimizes the possibility of macrosegregation, increases microcleanliness, and is preferred for premium quality jet engine rotating component applications. 718Plus alloy has at least a 100°F (55°C) operating temperature advantage over 718 alloy. 718Plus alloy also has advantages over Waspaloy and other higher temperature capable, nickel-base alloys due to its higher strength, superior formability, better wear resistance, and a resistance to weld cracking. 718Plus alloy is a lower cost option than Waspaloy or Rene 41 alloy due to its lower intrinsic raw materials cost and improved hot workability which provides higher material yields, resulting in a lower cost finished part. 718Plus alloy is available in all product forms: ingot, billet, block, forged round bar, hot-rolled shapes and rectangles, bar, rod, wire, plate, sheet, strip, and castings.

Information provided by Allegheny Technologies

Key Words: UNS N07818
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 8.25 g/cc
 
Mechanical PropertiesOriginal ValueComments
Hardness, Rockwell C 25 - 35solution heat treated depending on quench rate
 42 - 48fully aged condition
Tensile Strength, Ultimate 215000 psi
 200000 psi
@Temperature 427 °C
 210000 psi
@Temperature 204 °C
Tensile Strength, Yield 170000 psi
 150000 psi
@Temperature 427 °C
 160000 psi
@Temperature 204 °C
Elongation at Break 25 %
 
Thermal PropertiesOriginal ValueComments
CTE, linear 6.85 µin/in-°F
@Temperature 100 °C
 7.30 µin/in-°F
@Temperature 250 °C
 13.86 µm/m-°C
@Temperature 500 °C
 16.74 µm/m-°C
@Temperature 900 °C
Specific Heat Capacity 0.520 J/g-°C
@Temperature 260 °C
 0.700 J/g-°C
@Temperature 538 °C
 0.725 J/g-°C
@Temperature 399 °C
 0.900 J/g-°C
@Temperature 468 °C
Thermal Conductivity 95.0 BTU-in/hr-ft²-°F
@Temperature 260 °C
 125 BTU-in/hr-ft²-°F
@Temperature 538 °C
 165 BTU-in/hr-ft²-°F
@Temperature 816 °C
 185 BTU-in/hr-ft²-°F
@Temperature 1090 °C
Melting Point 1260 - 1343 °C
Solidus 1260 °C
Liquidus 1343 °C
 
Component Elements PropertiesOriginal ValueComments
Aluminum, Al 1.2 - 1.8 %
Boron, B <= 0.0080 %
Carbon, C <= 0.060 %
Chromium, Cr 17 - 21 %
Cobalt, Co 8.0 - 10 %
Iron, Fe 8.0 - 10 %
Manganese, Mn <= 0.35 %
Molybdenum, Mo 2.5 - 3.1 %
Nickel, Ni 45.002 - 57.55 %
Niobium, Nb (Columbium, Cb) 4.75 - 5.8 %
Phosphorus, P <= 0.020 %
Silicon, Si <= 0.35 %
Sulfur, S <= 0.010 %
Titanium, Ti 0.50 - 1.0 %
Tungsten, W 0.50 - 1.5 %

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NALL08A / 14776

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