Aluminum is an important commercial
metal possessing some very unique properties. It is very light
(density about 2.7) and some of its alloys are very strong, so its
strength-weight ratio makes it very attractive for aeronautical uses
and other applications in which weight saving is important.
Aluminum, especially in the pure form,
has very high electrical and thermal conductivities and is used as an
electrical conductor in heat exchangers, etc. Aluminum has good
corrosion resistance, is nontoxic, and has a pleasing silvery-white
color; these properties make it attractive for applications in the
food and container industry, architectural, and general structural
fields.
Aluminum is very ductile and easily
formed by casting and mechanical forming methods. Aluminum owes its
good resistance to atmospheric corrosion to the formation of a tough,
tenacious, highly insulating, thin oxide film, in spite of the fact
that the metal itself is very anodic to other metals.
In moist atmospheres, this protective
oxide may not form, and some caution must be taken to maintain this
film protection. Although aluminum can be joined by all welding
processes, this same oxide film can interfere with the formation of
good bonds during both fusion and resistance welding, and\ special
fluxing and cleaning must accompany welding operations.
Commercially pure aluminum (99+%) is
very weak and ductile: tensile strength of 90 Mpa (13,000 lb/in2),
yield strength of 34.5 MPa (5000 lb/in2), and shearing strength of 62
MPa (9500 lb/in2). Extrapure grades (electrical conductor grade) are
99.7+% pure, and are even weaker, but have better conductivity.
Heat Treatment of Aluminum Alloys.
Alloys of the 1000, 3000, and 5000
series cannot be hardened by heat treatment. They can be hardened by
cold working and are available in annealed (recrystallized) and
cold-worked tempers.
The 5000 series alloys are the
strongest non-heat-treatable alloys and are frequently used where
welding is to be employed, since welding will generally destroy the
effects of hardening heat treatment. The remaining wrought alloys can
be hardened by controlled precipitation of alloy phases.
The precipitation is accomplished by
first heating the alloy to dissolve the alloying elements, followed
by quenching to retain the alloy in supersaturation. The alloys are
then “aged” to develop a controlled size and distribution of
precipitate that produces the desired level of hardening. Some alloys
naturally age at room temperature; others must be artificially aged
at elevated temperatures.
