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Nimonic Alloy 90 (Nimonic 90) is a precipitation hardenable nickel-chromium-cobalt alloy strengthened by the addition of Titanium and Aluminium. Alloy 90 has a high stress rupture strength and creep-resistant at temperature to about 950°C(1740°F). Alloy 90 is typically used on such things as turbine blades, hot working tools and high-temperature springs.

Nimonic 90 is a super alloy of nickel-chromium-cobalt, known for both its strength and its ability to withstand extremely high temperature. Typically used in temperature ranging from 100 degrees Celsius to +650 degrees Celsius, Nimonic 90 is a popular alloy in the aerospace and aircraft industries. It is widely used in such applications as valves in turbo motors and blades and discs in gas turbines.

Alloy Wire International Ltd. is a U.K. wire manufacturer specialising in the production of high performance alloys, mainly Nickel Alloys, but including Cobalt and Titanium Alloys. These alloys might be used in any environment that requires resistance to heat and corrosion but where the mechanical properties of the metal must be retained.

Specification: UNS N07090, Werkstoff Nr. 2.4632, AMS 5829 Welding Wire, BS 3075, NA 19, HR2, HR202, HR402, HR501, HR502, HR503. MSRR 7016 and MSRR 7087, AFNOR NCK 20D AECMA Pr EN 2295, EN 2296, EN 2297, EN 2298, EN 2299, EN 2400, EN 2401, EN 2412, EN 2669 and EN 2670 Tradenames: Nimonic® 90, Udimet 90 (tm), VAT90.



Chemical Composition

Weight % Ni Cr Co Ti Al C Si Cu Fe Mn B S Zr Pb
Alloy 90

Balance

18.0 - 21.0

15.0 - 21.0

2.0 - 3.0 1.0 - 2.0 0.2 max 1.0 max 0.2 max 1.5 max 1.0 max 0.02 max 0.015 max 0.15 max 0.0020 max

Typical Mechanical Properties
Temperature PSI MPa
700°C / 1290°F 52,000 360
750°C / 1380°F 35,000 240
800°C / 1470°F 22,000 150
850°C / 1560°F 11,000 75
Rupture Strength 1000h



Typical Properties> of Nimonic 90
Typical properties of Nimonic 90 are covered in the following table.
Property Metric Imperial
Density 8.18 g/cm3 0.296 lb/in3
Melting point 1370 °C 2500 °F
Co-Efficient of Expansion 12.7 μm/m.°C (20-100 °C) 7.1x10-6 in/in.°F (70-212 °F)
Modulus of rigidity 82.5 kN/mm2 11966 ksi
Modulus of elasticity *213 kN/mm2 30894 ksi
**227 / 240 kN/mm2 32924 / 34810 ksi
* Solution Annealed + Aged **Spring Temper and Aged

Properties of Supplied Materials and Heat Treated Materials
Condition of Supply Heat Treatment (After Forming)
Solution Annealed Age Harden at 750°C (1380°F) for 4 hours and air cool.
Spring Temper Age Harden at 650°C (1200°F) for 4 hours and air cool.
Spring Temper Age Harden at 600°C (1110°F) for 16 hours and air cool.
Condition Approx Tensile Strength Approx Service Temp.
Solution Annealed 800 - 1000 N/mm2 116 - 145 ksi
Solution Annealed + aged 1300 - 1400 N/mm2 189 - 203 ksi up to 550°C up to 1020°F
Spring Temper 1300 - 1500 N/mm2 189 - 218 ksi
Spring Temper + aged 1500 - 1800 N/mm2 218 - 261 ksi up to 350°C up to 660°F



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