Compositepro... lots of folks get HT concepts WRONG.
NOTE. See Aluminum Association spec AA H31.1 and/or SAE AS1900 for a basic discussion of aluminum alloy tempers.
Annealing is a process where a metallurgical structure [aluminum, ferrous, nickel, titanium, copper, etc alloys] is taken to its most ductile and hence most deformable, but long-term-stable, state. For most metals annealing is accomplished by heating the alloy to a specified temperature for a specified soak time... Then cooling SLOWLY... back to room temp. Aluminum alloys are typically cooled in still air on a rack; steel and other alloys highly prone to oxidation may be cooled in the oven with inert gas to eliminate oxygen, etc]. Most alloys have various stable annealed conditions. For instance 2XXX and 7XXX aluminum alloys can be conventionally to the -O ["Ooo" NOT -0 "zero"] temper... or the specially annealed state called -O1 ["Ooo one"] temper where grain structure is slightly harder/tougher. NOTE: the temperatures for annealing process are typically close-to to solution heat treating temperatures... but not quite the same.
Solution Heat Treating is a process where a metallurgical structure [aluminum, ferrous, nickel, titanium, copper, etc alloys] is taken to certain grain state at that is only stable at the elevated temperature. The alloy is then RAPIDLY cooled [quenched] to room temperature... typically within a matter of seconds... the high temperature grain structure is frozen down to room temperature [below 140F]. This rapid cooling can be accomplished by agitated immersion in water [with mixtures to delay boiling to a higher temperature and minimize in-water oxidation], oil, cold gas, etc. The resultant metallurgy is then either in a an unstable transition state... or in a stable temper state where further transition is feasible/necessary.
For 2XXX, 6XXX and 7XXX heat treatable aluminum alloys the post SHT After-Quench ["AQ"] temper is the "-W" temper. At this point aluminum alloys ACT like they are annealed... for a short period of time... however, there are a LOT of crazy metallurgical process occurring within the alloy. For 2xxx alloys there is a spontaneous transition to the -T42 temper that occurs within ~96-hours. This transition rate-of-reaction can be delayed [freezing] or accelerated [by heating]... typical chemistry 101 stuff. I think the copper within the 2XXX alloys is the driving factor here. NOTE: 6xxx and 7XXX alloys typically have to be pushed by heat from the -W temper to a more useful strength temper.
Interesting note. When an 2xxx or 6xxx aluminum alloy is deformed in the -O temper "the-grain-remembers-the-strain" and the grain typically grows proportional to the strain. When SHT/Quenched/Tempered [heat-aged-hardened] the grain grow is still evident in the heat treated part [-TX] and MAY be detrimental to overall strength/toughness. Hence the -T42 and -T62 tempers were developed to describe/quantify these less than ideal temper states.
However, when alloys are strained in the unstable -W temper [within a certain critical period of time, AQ], then "the-grain-forgives-the-strain" due to the unstable metallurgy. EVERY MATERIAL SPEC [AMS] for heat treated raw sheet/plate, extruded shapes or drawn bar have a basic temper [-T3, -T6, -T7, -T8] allows for the beneficial effects of strain that occurred AQ [in the -W temper state]... and the last digits of the temper number -Txx50, -Txx51 -Txx510, -Txx511, etc are added indicating the type of strain, AQ etc.
UH OH, my brain hurts... this quick reply has gotten more complicated than I expected... gotta go back to work.
Regards, Wil Taylor
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