Heat-treated zirconium alloy product
AssigneeAtomic Energy of Canada Limited
InventorsErland M. Schulson, Donald J. Cameron
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AssigneeAtomic Energy of Canada Limited
InventorsErland M. Schulson, Donald J. Cameron
Estimating the term…
High tensile strength, creep and corrosion resistant zirconium alloys containing 7.0-10.0 wt % aluminum, 0-3 wt % in total of one or more elements selected from the group consisting of magnesium, tin, chromium, iron, carbon, silicon, yttrium, niobium, molybdenum and beryllium, the balance zirconium and incidental impurities, are produced by annealing cast alloys at a temperature below about 992.degree. C. for a period of time sufficient to produce alloys having a substantially continuous matrix of the ordered intermetallic compound Zr.sub.3 Al. The alloys may initially be hot worked at temperatures about 1000.degree. C., while in the .beta.Zr-Zr.sub.2 Al two phase region, prior to annealing. Preferred alloys contain 7.5-9.5 wt % aluminum, the balance zirconium and incidental impurities.
A heat-treated, high tensile strength creep and corrosion resistant zirconium alloy containing 7.0-10.0 wt% aluminum, and 0-3.0 wt% of one or more elements selected from the group comprising magnesium, tin, chromium, iron, carbon, silicon, yttrium, niobium, molybdenum and beryllium, balance, zirconium and incidental impurities, having a substantially continuous matrix of the intermetallic compound Zr.sub.3 Al.
A corrosion resistant, structural element fabricated from an alloy containing 7.0-10.0 wt% Al, and 0-3.0 wt% of one or more elements selected from the group comprising magnesium, tin, chromium, iron, carbon, silicon, yttrium, niobium, molybdenum and beryllium, balance zirconium and incidental impurities, heat treated in the range from 700.degree. C.-950.degree. C. for a sufficient time to ensure a substantially continuous matrix of the intermetallic compound Zr.sub.3 Al.
Dependencies are inferred from the claim text.