Iron-nickel superalloy of the type in 706

Alloys or metallic compositions – Containing over 50 per cent metal but no base metal – Iron containing

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4203861, 148442, 148419, 416223R, 416241R, C22C 3000

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058634940

ABSTRACT:
An iron-nickel superalloy of the type IN 706 has an addition of 0.02 to 0.3 percent by weight of boron and/or 0.05 to 1.5 percent by weight of hafnium. By means of this addition, a virtual doubling of the ductility is achieved as compared with an addition-free iron-nickel superalloy of the type IN 706, while the hot strength is reduced only slightly. The alloy is particularly suitable as a material for rotors of large gas turbines. It has a sufficiently high hot strength. When locally acting temperature gradients arise unwanted stresses can occur to only a slight extent because of the high ductility of the alloy.

REFERENCES:
patent: 3705827 (1972-12-01), Muzyka et al.
patent: 3785876 (1974-01-01), Bailey
patent: 5415712 (1995-05-01), Thamboo
"The Microstructure of 706, a new Fe-Ni-Base Superalloy", Moll, et al., Metallurgical Transactions, vol. 2, Aug. 1971, pp. 2143-2151.
"Environmental Damage of a Cast Nickel Base Superalloy", Woodford, Metallurgical Transactions, vol. 12A, Feb. 1981, pp. 299-308.
"Heat Treatment of 706 Alloy for Optimum 1200.degree.F Stress-Rupture Properties", Moll, et al., Metallurgical Transactions, vol. 2, Aug. 1971, pp. 2153-2160.
CA 76: 62338 1971.

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