US2005194068A1PendingUtilityA1
Nickel-based superalloy having very high resistance to hot-corrosion for monocrystalline blades of industrial turbines
Priority: Nov 30, 2000Filed: Feb 28, 2005Published: Sep 8, 2005
Est. expiryNov 30, 2020(expired)· nominal 20-yr term from priority
C22C 19/056
50
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Claims
Abstract
Nickel-based superalloy, suitable for monocrystalline solidification, having the following composition by weight: Co: 4.75 to 5.25% Cr: 15.5 to 16.5% Mo: 0.8 to 1.2% W: 3.75 to 4.25% Al: 3.75 to 4.25% Ti: 1.75 to 2.25% Ta: 4.75 to 5.25% C: 0.006 to 0.04% B: ≦0.01% Zr: ≦0.01% Hf: ≦1% Nb: ≦1% Ni and any impurities: complement to 100%.
Claims
exact text as granted — not AI-modified1 . A nickel-based superalloy, suitable for monocrystalline solidification, characterized in that its composition by weight is as follows:
Co:
4.75 to 5.25%
Cr:
15.5 to 16.5%
Mo:
0.8 to 1.2%
W:
3.75 to 4.25%
Al:
3.75 to 4.25%
Ti:
1.75 to 2.25%
Ta:
4.75 to 5.25%
C:
0.006 to 0.04%
B:
≦0.01%
Zr:
≦0.01%
Hf:
≦1%
Nb:
≦1%
Ni and any impurities:
complement to 100%.
2 . Industrial turbine blade produced by monocrystalline solidification of a superalloy according to claim 1.Join the waitlist — get patent alerts
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