Process for preparation of near-alpha titanium alloys

Metal treatment – Compositions – Heat treating

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148 325, C22F 118

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043092268

ABSTRACT:
Process for improving the creep strength of near-alpha titanium alloys by a specific heat treatment schedule which include solution heat treatment prior to conventional aging.

REFERENCES:
patent: 3833363 (1974-09-01), Bomberger et al.
patent: 3901743 (1975-08-01), Sprague et al.
Mendritta et al., Metallurgical Transaction, vol. 5, pp. 1949-1951, Aug. 1974.
Rosenberg et al., Technical Report No. 17, Project No. 48-8 Titanium Metals Corporation of America, Henderson, Neva, Jan. 31, 1966.
Sparks, Report No. RD66-108, M.D. & E. No. 193, Wyman-Gordon Company, Worcester, MA, Feb. 1966.
Sparks, Report No. Rd67-130, M.D. & E. No. 250, Wyman-Gordon Company, Worcester, MA, 1967.
Shannon, Code 3718, Aerospace Structural Metals Handbook, vol. II, AFML-TR-68-115, Mar., 1968.
Wood et al., Titanium Alloys Handbook, Metals and Ceramics Information Center, pp. 1-6:72-1-6:72-13, Dec. 1972.

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