High strength alloy tailored for high temperature...

C - Chemistry – Metallurgy – 22 – C

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C22C 19/05 (2006.01)

Patent

CA 2352822

A high strength nickel-base alloy consisting essentially of, by weight percent, 50 to 60 nickel, 19 to 23 chromium, 18 to 22 iron, 3 to 4.4 aluminum, 0 to 0.4 titanium, 0.05 to 0.5 carbon, 0 to 0.1 cerium, 0 to 0.3 yttrium, 0.002 to 0.4 total cerium plus yttrium, 0.0005 to 0.4 zirconium, 0 to 2 niobium, 0 to 2 manganese, 0 to 1.5 silicon, 0 to 0.1 nitrogen, 0 to 0.5 calcium and magnesium, 0 to 0.1 boron and incidental impurities. The alloy forms 1 to 5 mole percent Cr7C3 after 24 hours at a temperature between 950 and 1150 ~C for high temperature strength.

Cette invention se rapporte à un alliage à base de nickel haute résistance comprenant essentiellement, en pourcentage en poids, 50 à 60 % de nickel, 19 à 23 % de chrome, 18 à 22 % de fer, 3 à 4,4 % d'aluminium, 0 à 0,4 % de titane, 0,05 à 0,5 % de carbone, 0 à 0,1 % de cérium, 0 à 0,3 % d'yttrium, 0,002 à 0,4 % au total de cérium plus yttrium, 0,0005 à 0,4 % de zirconium, 0 à 2 % de niobium, 0 à 2 % de manganèse, 0 à 1,5 % de silicium, 0 à 0,1 % d'azote, 0 à 0,5 % de calcium et magnésium, 0 à 0,1 % de bore, et des impuretés accidentelles. Cet alliage forme 1 à 5 % molaire de Cr¿7?C¿3? après 24 heures à une température comprise entre 950 et 1150 ·C pour une résistance hautes températures.

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