Low density, high strength Al-Li alloy having high toughness at

Metal treatment – Process of modifying or maintaining internal physical... – With casting or solidifying from melt

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148693, 148697, 148700, 148417, 148439, 420529, 420532, 420533, 420543, C22F 104

Patent

active

053891651

ABSTRACT:
An aluminum-based alloy useful in aircraft and aerospace structures which has low density, high strength and high fracture toughness consists essentially of the following formula:

REFERENCES:
patent: 5032359 (1991-07-01), Pickens et al.
patent: 5198045 (1993-03-01), Cho et al.
patent: 5211910 (1993-05-01), Pickens et al.
Suresh, S. and Vasudevan, A. K. "Influence of Composition and Aging Treatment on Fracture Toughness of Lithium-Containing Aluminum Alloys", Aluminum Lithium Alloys III, Conference Proceedings, pp. 595-601.
White, J. et al., "Effect of Precipitation on Mechanical Properties of Al-Li-Cu-Mg-Zr", Aluminum Lithium Alloys III, Conference Proceedings, pp. 530-538.
Rinker, Marek and Sanders, Mat. Cir. and Eng. 64, 1984, pp. 207-208.

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