PRODUCT DESCRIPTION

AMS 5872 is a specification of Nickel Nimonic 263 nickel-chromium-cobalt-molybdenum alloy. Available as plate, sheet or strip, the AMS 5872 specification offers excellent ductility and excellent fabrication characteristics. For sheets, the annealing process lasts 15 minutes at a temperature range of 1922-2012°F (1050-1100°C), followed by rapid cooling. Besides, fluidized bed quenching can be used for sheets.
This specification can be fabricated using hot working in the temperature range of 1742-2102°F (950-1150°C), or cold working for 0.5-1.2 mm thick strips using annealing technique of 3 minutes at 1190°C by fluidized bed quenching.
Nimonic 263 nickel alloy is a nickel-chromium-cobalt-molybdenum alloy specially meant for use in high temperature and high strength applications. Alloy 263 can be precipitation-hardened. Due to its properties, this alloy is mostly used in high temperature and high strength applications, such as the hot section of gas turbines, both in aircraft and land-based applications.

Chemical Composition

ElementContent (%)
Nickel, Ni49
Cobalt, Co19-21
Chromium, Cr19-21
Molybdenum, Mo5.60-6.10
Titanium, Ti1.90-2.40
Iron, Fe0.70
Manganese, Mn0.60
Aluminum, Al0.60
Silicon, Si0.40
Copper, Cu0.20
Carbon, C0.040 - 0.080
Boron, B0.0050
Sulfur, S0.0070

Typical Mechanical Properties

MaterialTemp °CYield Strength (Mpa)Tensile Strength (Mpa)Elongation
%
Hardness HRC
Nimonic 263 Sheet
Solution Treated (AMS 5872 / BS HR206)
RT---22.5 max
Nimonic 263 Sheet
Heat Treated (AMS 5872 / BS HR206)
RT580 (typical)973 (typical)39 -
Nimonic 263 Sheet
Heat Treated (AMS 5872 / BS HR206)
780403 (min)541 (min)9-

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