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#1
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Aluminum protects itself. When it rusts (aka oxidizes,) which it does
very very quickly, it forms aluminum oxide (duh.) A coating of aluminum oxide is about the hardest, most impervious thing you could put on a piece of metal. The "process" does not "continue on its own." As soon as a microscopically thin layer forms, your aluminum is protected from further degradation. I'm no expert, however my understanding is... 6061 and 2024 are not pure aluminum. In order to obtain the desired strength properties, other metals are added to the aluminum. I believe 2024 has something of the order of a couple percent of copper. The surface will not be pure aluminum oxide, since there are "impurities" within the metal. You are now open to pitting corrosion as well as granular corrosion. The alodine forms a passivated layer, that uniformly protects the whole surface. Being a delicate surface itself (as a previous poster already mentioned), the passivated layer needs to be protected against mechanical abrasion. 6061 is quite immune to most of the above corrosion. It is still a good idea to protect anywhere you will have metal to metal contact though, since you can have moisture trapped between the parts which accelerates the corrosion. I use 2024, so I do the scuff, etch, alodine, 2 part epoxy prime routine. |
#2
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![]() "RV9" wrote I'm no expert, however my understanding is... Obviously your understanding is far above Smitty's I use 2024, so I do the scuff, etch, alodine, 2 part epoxy prime routine. As would any sensible person working aluminum in an aircraft. Strange, isn't it, that the Navy (and I suspect the other armed forces) spend all of that time with the above procedure on their aircraft? They must know something that Smitty does not. -- Jim in NC |
#3
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6061 and 2024 are not pure aluminum. In order to obtain the desired
strength properties, other metals are added to the aluminum. I believe 2024 has something of the order of a couple percent of copper. The surface will not be pure aluminum oxide, since there are "impurities" within the metal. You are now open to pitting corrosion as well as granular corrosion. 2024 Cu 3.8 - 4.9 Mg 1.2 - 1.8 Mn 0.30 - 0.9 Fe = 0.50 Si = 0.50 Zn = 0.25 Zr+Ti = 0.20 Total Other = 0.15 Ti = 0.15 Cr = 0.10 Other Elem = 0.05 Al Remainder 6061 Mg 0.40 - 0.8 Si 0.30 - 0.6 Fe = 0.35 Cu = 0.25 Cr = 0.20 Mn 0.05 -0.20 Total Other = 0.15 Zn = 0.15 Ti = 0.10 Other Elem = 0.05 Al Remainder All compositions in wt%. "alclad" sheets have a thin layer of pure aluminium on the surface to improve corrosion resistance. see http://aluminium.matter.org.uk/aluse...ion_browse.asp for corrosion and anodizing properties. -- Geoff the sea hawk at wow way d0t com remove spaces and make the obvious substitutions to reply by mail Spell checking is left as an excercise for the reader. |
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