Nickel Alloy 86 / Nimonic 86


Technical Data Sheet

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.

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

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

Customer Reviews - What Customers Say About Us!

"I would like to extend my gratitude to the entire staff at Aircraft Materials. It is a true pleasure to work with professionals in the aerospace industry. Keep up the great work!"
"Thank you very much, everything seems perfect. The quality of your cutting is superb."
"Could not fault your service."
"The service was perfect you had stock and same day collection"
"Item was very well packed"
  CLICK HERE TO VIEW OUR BROCHURE  

 

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.