Weldable anti-corrosive aluminium-magnesium alloy containing a high amount of magnesium, especially for use in aviation

The invention relates to a weldable, corrosion-resistant, high-magnesium-content aluminum-magnesium alloy, which contains a ternary aluminum-scandium-zirconium phase as the essential component. Such an alloy is known from U.S. Pat. No. 5,624,632, for example, and is of interest above all for applications in aeronautics due to its low density, high strength and corrosion resistance. Adding rare earth or rare earth-like elements generates dispersoids in the aluminum-magnesium alloy, which produce a higher strength and corrosion resistance according to the above US patent. The above US patent makes no statement as to the weldability of such an alloy.

The object of this invention is to provide a weldable, corrosion-resistant, high-magnesium-content aluminum-magnesium alloy, which is at least as good as the known alloy in terms of strength and corrosion behavior, and exhibits a high recrystalization threshold to go along with a good weldability. This object is achieved by an aluminum-magnesium alloy according to claim 1 .

In comparison to the known alloy, this new alloy exhibits above all a distinctly lower manganese content, wherein an improved corrosion resistance was surprisingly found, primarily in the sensitized state of the parts made out of this alloy, e.g., when cold-formed parts are subjected to an elevated temperature over a prolonged period. It is assumed that these positive properties are determined primarily by the ratio of manganese to scandium. An improved corrosion resistance is observed at a ratio of Mn to Sc<2. Along with acting as a grain growth inhibitor, the titanium content not present in the known alloy helps to increase strength, since titanium can replace the zirconium in the ternary Al—Sc—Zr phase, wherein the solubility of titanium is lower than that of zirconium however.

The addition of Cu and/or Zn increases the strength, which can be traced back to the known high strength of the Al—Cu or Al—Zn phase. The respective upper concentration limits are selected to prevent the Cu from diminishing the weldability, and the Zn from diminishing the corrosion resistance.

A particularly strong and corrosion-resistant alloy contains at least 0.15% w/w scandium. A component from the lanthanide series is preferably added in amounts ranging from 0.05 and 0.35% w/w, wherein this range relates to the total mixture when using a lanthanide mixture. The alloy tolerates silicon contamination of up to 0.1% w/w; primarily the dynamic properties deteriorate above this level.

A particularly strong and corrosion-resistant alloy contains at least 0.15% w/w scandium. Lanthanidene is preferably added in amounts ranging from 0.05 and 0.35% w/w, wherein this range relates to the total mixture when using a lanthanidene mixture. The alloy tolerates silicon contamination of up to 0.1% w/w; primarily the dynamic properties deteriorate at above this level.