A magnesium alloy consists essentially of the formula Mg.sub.bal Al.sub.a Zn.sub.b X.sub.c, wherein X is at least one element selected from the group consisting of manganese, cerium, neodymium, praseodymium, and yttrium, "a" ranges from about 0 to 15 atom percent, "b" ranges from about 0 to 4 atom percent, and "c" ranges from about 0.2 to 3 atom percent, the balance being magnesium and incidental impurities, with the proviso that the sum of aluminum and zinc present ranges from about 2 to 15 atom percent. Second phase particles contained by the alloy are less susceptible to corrosion attack. Articles produced from the alloy have superior corrosion resistance and mechanical properties comparable to those made from commercial magnesium alloys. Such articles are suitable for application as structural members in helicopters, air frames, such as gear box housings, where good corrosion resistance in combination with low density and good strength are required.
2007-06-01 10:08:33
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answer #1
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answered by gatorbait 7
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It would probably work very well for the housing because it's strong and lightweight, but the gears themselves may have some problems. Gears are usually made of hard metals (steel). Aluminum alloys are relatively soft which would cause them to wear quickly. As always, it depends on the application.
2007-06-01 17:27:17
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answer #2
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answered by Dan 2
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