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Nickel Alloy 86 / Nimonic 86


Technical Data Sheet

 

Chemical Composition Limits
Weight% Ni Cr Mo Ce C
Alloy 86 65 25.0 10.0 0.03 0.05 max

Alloy 86 is a nickel-chromium-molybdenum alloy. Alloy 86 has good formability and weldability with exceptional resistance to oxidation and scaling to 1050°C (1920°F). Alloy 86 is quite rare due to its "Cerium" addition although it is widely used in afterburners and heat treating furnaces.

Typical Mechanical Properties


Material Treatment Temperature °C UltimateTensile Strength MPa Yield Strength (0.2% Offset) MPa Elongation on 5.65 √ 50(%)
Alloy 86 Bar Heat Treatment 4h/1150°C/ AC 300 251 692 49
Allloy 86 Bar Heat Treatment 4h/1150°C/ AC 500 243 661 54
Allloy 86 Bar Heat Treatment 4h/1150°C/ AC 700 239 557 56
Allloy 86 Bar Heat Treatment 4h/1150°C/ AC 850 173 319 69

Availability
Alloy 86 is available in Round Bar and Sheet. For all stock availability contact Sales.

Specifications
MSRR 7152 Sheet
MSRR 7141 Bar
Tradename's: NIMONIC 86

Services
At Aircraft Materials we specialise in the rapid turn-around of orders, with most stock items ready for shipping out the same day to anywhere in the world. For time-critical orders, such as AOGs use our AOG service desk (aog@aircraftmaterials.com), the team are dedicated to processing and dispatching orders on the same day, even for cutting orders on bar and sheet products.

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Disclaimer
Every effort is made to ensure that technical specifications are accurate. However, technical specifications included herein should be used as a guideline only. All specifications are subject to change without notice.