Page 52 - Welding of Aluminium and its Alloys
P. 52

44     The welding of aluminium and its alloys

              treatment and ageing after welding, not often possible in a fully fabricated
              structure. The less weldable alloy 2014 (AlZnMgCu) may also be heat
              treated to recover some tensile strength but the improvement is not as
              great as in 2219 (AlCu6) and may exhibit an even greater reduction in
              ductility.
                Filler metals of similar composition such as 2319 (AlCu6) are available
              and weld metal strengths can therefore be matched with the properties in
              the HAZ.


              3.4.2.2 Aluminium–magnesium–silicon alloys (6XXX series)
              The hardening constituent in 6XXX series alloys is magnesium silicide
              Mg 2Si. These alloys contain small amounts of silicon and magnesium, typi-
              cally less than 1% each, and may be further alloyed with equally small
              amounts of manganese, copper, zinc and chromium.The alloys are sensitive
              to weld metal cracking, particularly when the weld metal is rich in parent
              metal such as in the root pass of the weld. Fortunately the cracking can be
              readily prevented by the use of filler metals containing higher proportions
              of silicon such as 4043 or, with a slightly increased risk of hot cracking, the
              higher magnesium alloys such as 5356.
                With these heat-treatable alloys the changes in the structure and mechani-
              cal properties, briefly discussed in Chapter 2, are complex and strongly
              dependent on the welding conditions employed. Welding without filler
              metal or with filler metal of parent metal composition is rarely practised
              because of the risk of weld metal hot cracking. A weld metal with a com-
              position close to that of the parent metal may age-harden naturally or may
              be artificially aged to achieve a strength approaching, but never matching,
              that of the aged parent metal.
                In the overheated zone in the HAZ closest to the fusion line, partial
              melting of the grain boundaries will have taken place. Temperatures have
              been high enough and cooling rates sufficiently fast that solution treatment
              has taken place, enabling some ageing to occur after welding. Adjacent to
              this is the partially solution-treated zone where some of the precipitates
              have been taken into solution, enabling some post-weld hardening to occur,
              but those not dissolved will have been coarsened. Outside this will be the
              overaged zone where precipitate coarsening has taken place and there has
              been a large drop in strength.
                The strength losses in the 6000 alloys are less in the naturally aged metal
              than in the artificially aged alloys.The strength of the weld and HAZ in the
              artificially aged condition generally drop to match that of the naturally aged
              alloy with a narrow solution-treated zone either side of the weld and an
              overaged zone beyond this, which is weaker than the T6 condition.With
              controlled low-heat input welding procedures the strength of the weldment
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