High fracture toughness aluminum-copper-lithium sheet or light-gauge plates suitable for fuselage panels

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United States of America Patent

PATENT NO 8771441
APP PUB NO 20070181229A1
SERIAL NO

11612131

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Abstract

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An aluminum alloy comprising 2.1 to 2.8 wt. % Cu, 1.1 to 1.7 wt. % Li, 0.1 to 0.8 wt. % Ag, 0.2 to 0.6 wt. % Mg, 0.2 to 0.6 wt. % Mn, a content of Fe and Si less or equal to 0.1 wt. % each, and a content of unavoidable impurities less than or equal to 0.05 wt. % each and 0.15 wt. % total, and the alloy being substantially zirconium free.

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Patent Owner(s)

Patent OwnerAddress
CONSTELLIUM ISSOIRE63500 ISSOIRE

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Bes, Bernard Seyssins, FR 31 189
Ribes, Herve Clermont Ferrand, FR 11 105
Sigli, Christophe Grenoble, FR 19 182
Warner, Timothy Voreppe, FR 45 531

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