Abstract:
The ternary Al-Cu-Mg system 2xxx series aluminium alloys were examined as construction
materials for armour system applications based upon comparable ballistic properties to the
currently employed Al-7xxx series alloys. Utilising MIG welding solidification cracking was
evident when welding constrained Al-2024 candidate base material using Al-2319 filler, the
only available consumable wire for this series. A previously developed thermodynamic
model suggested that an incompatible weld chemistry resulted when welding with this filler
which would result in hot cracking due to a wide weld pool freezing range and a low volume
fraction of eutectic liquid. As this filler wire was the only commercially available Al-2xxx
filler this was seen as the principal limiting factor for exploiting this alloy series. The solution
was to vary and control weld chemistry. Two approaches were taken. Firstly advanced arc
welding was used to control weld dilution with the base material. A clad layer exhibiting a
less crack susceptible composition was deposited using the Cold Metal Transfer process and
the binary Al-2319 filler wire. Onto this layer the same filler could then be deposited to
provide a structural joint. Although not fully validated, by limiting weld dilution with the
base material this technique showed potential as an alternative method for suppressing
solidification cracking. The second approach, which forms the core of this work, adapted the
conventional tandem MIG welding process to mix different series consumable fillers in a
single weld pool to control weld composition. A range of ternary weld mixtures were
produced which resulted in the development of a robust thermodynamic model. Validation
using this system resulted in weld cracking being eradicated. The concept was then further
developed to weld using three filler wires; this expanded the mixing range and allowed
further model validation. A range of crack free compositions were produced with differing
mechanical properties. An optimum weld composition was determined that was then used for
characterisation of the weldment. By varying heat input, base material HAZ softening was
controlled with joint failure confined to the weld / base material interface. This was attributed
to grain boundary liquation due to the welding temperatures involved resulting in solute rich
grain boundaries. These areas did not deform easily under tensile loading initiating fracture of
the joint. Acceptable joint strengths were realised however ductility was reduced due to the
identified failure mode. Although not tested to military specifications, acceptable mechanical
test values were recorded which were closely compliant with the minimum requirements for
armour system specifications. As a consequence a filler wire composition was recommended
for future prototype development.