Metal treatment – Compositions – Heat treating
Patent
1977-11-07
1979-02-20
Dean, R.
Metal treatment
Compositions
Heat treating
75171, 148 325, C22C 1905
Patent
active
041405552
ABSTRACT:
A nickel-base casting superalloy consisting essentially (by weight of the alloy) of 7% to 25% chromium, 02.% to 7% aluminum, 0.2% to 6% titanium, 0.01% to 0.25% carbon, up to 0.2% zirconium, up to 0.15% boron, up to 3% hafnium, at least 5% of a matrix-strengthening element selected from the group consisting of 0 to 25% cobalt, 0 to 10% molybdenum, 0 to 13% tungsten to 6% tantalum, 0 to 5% columbium, and 0 to 1.5% vanadium, a carbide shape controller selected from 0.022% to 0.15% magnesium, 0.005% to 0.1% calcium, or mixtures thereof, and the balance nickel except for impurties, said alloy in the as-cast condition having a fine grain macrostructure in thick as well as thin sections, exhibiting a microstructure having precipitated carbide particles which are substantially equi-axed in shape and well-distributed through the alloy with a substantial portion of the magnesium and/or calcium content of the alloy concentrated in such particles and at grain boundaries, and displaying in its thick sections a tensile strength and elongation substantially higher than a corresponding thick-section alloy having a microstructure exhibiting script-like carbide particles substantially free internally and at grain boundaries of said carbide shape controller.
REFERENCES:
patent: 2570193 (1951-10-01), Bieber et al.
patent: 3512963 (1970-05-01), Schramm et al.
patent: 3575734 (1971-04-01), Muzyka et al.
patent: 3723108 (1973-03-01), Twigg et al.
Butzer Jerry A.
Garcia Willard
Hulit Gerald W.
Mihalisin John R.
Dean R.
Howmet Corporation
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