INCONEL 901

A nickel-iron-chromium alloy containing titanium and aluminum for precipitation hardening and molybdenum for solid-solution strengthening.

The alloy has high yield strength and creep resistance at temperatures to about 1110°F (600°C). A substantial iron content enables the alloy to combine high strength with good forging characteristics. Used in gas turbines for discs and shafts. Standard products form is round.

SPECIFICATION

• Specifications ASTM B333 / ASME SB333
• Width 1000mm / 1219mm /1250mm / 1500mm / 2000mm
• Length 2000 mm / 2440 mm / 2500 mm / 3000 mm / 6000 mm
• Thickness 0.1mm to 12 mm Thk
• Hardness Soft, Hard, Half Hard, Quarter Hard, Spring Hard etc.
  

Finish Hot rolled plate (HR), Cold rolled sheet (CR).
Form Coils, Foils, Rolls, Plain Sheet, Strip, Flats, Blank (Circle), Ring (Flange) etc. NICKEL ALLOYS INCONEL

Chemical composition

C 0.10 max%      Si 0.60 max%       Mn 1.00 max%      P 0.030max%       S 0.030max%      Al 0.35 max%     

Cr 12.50 min%      Cu %      Ni 43.0 min%       Mo 6.00 max%       Nb %      Ti 2.90 min%       V Co 1.0 max%