Aluminium alloys

Alloys or metallic compositions – Aluminum base – Copper containing

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148417, 148439, C22C 2116

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active

045885532

ABSTRACT:
Aluminium alloys having compositions within the ranges (in wt %) 2 to 2.8 lithium--0.4 to 1 magnesium--1 to 1.5 copper--0 to 0.2 zirconium--0 to 0.5 manganese--0 to 0.5 nickel--0 to 0.5 chromium--balance aluminium. The alloys are precipitation hardenable and exhibit a range of properties, according to heat treatment, which make them suitable for engineering applications where light weight and high strength are required.

REFERENCES:
patent: 2381219 (1945-08-01), Le Baron
patent: 2915390 (1959-12-01), Criner
patent: 2915391 (1959-12-01), Criner
"Aluminium und Aluminiumlegierungen", by Dr. D. Altenpohl, p. 705, 1965.
"Improved Aluminum Alloys for Airframe Applications", by M. W. Hyatt et al., Mar. 1977, pp. 56-59, Metal Progress.
Proceedings "First International Aluminum-Lithium Conference", 19-21 May 1980, Pub. Metallurgical Society of AIME.
American Metal Market/Metal Working News of 29 Dec. 1980.
Lockheed Report No. LMSC-D766966 (Sept. 1980) p. 10.

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