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Improving Global Quality of Life

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Up-to-date, titanium alloys have been used primarily in high performance fighter aircraft. They are now also<br />

being considered for structural material in new composite wrapped commercial aircraft (e.g A350). Titanium<br />

could replace aluminium, which is known to have a compatibility problem with graphite composites. Many<br />

new approaches to joining are likely to be employed, including riveting, arc and laser welding, and friction<br />

stir welding. Friction stir welding <strong>of</strong> titanium, however, posses a unique problem regarding tool wear,<br />

making it much less attractive than with aluminium. Due to its exceptional corrosion resistance, commercial<br />

grade titanium has been used as a replacement for stainless steel piping in heat exchangers for power<br />

plants. Similarly, beta alloys have been used as a drill pipe for sour oil wells due to their resistance to H 2<br />

S<br />

environments. Such pipe applications typically involve gas-tungsten arc welding. Titanium has also been<br />

given serious consideration for use as armour on military tanks. This would require multi-pass arc welding<br />

<strong>of</strong> thick sections using the gas-metal arc process. Such welding leads to large columnar grains in the weld<br />

metal, continuous from one pass to another, that significantly reduces toughness. These difficulties which<br />

are peculiar to titanium alloys have to be investigated more thoroughly in future. The extent to which Tialloys<br />

will be used in the future, in the applications discussed above, depends to a large part upon the<br />

availability <strong>of</strong> relatively inexpensive grades <strong>of</strong> titanium. One <strong>of</strong> the ways <strong>of</strong> reducing costs is to tolerate<br />

higher impurity levels, such as iron. It has to be investigated, however, how this might affect weldability or<br />

joint properties, including strength and corrosion resistance.<br />

Mg-Alloys<br />

Most magnesium alloys can be welded reasonably well, but present some unique problems with regard<br />

to bead control, spatter and oxidation. Due to a lower density, magnesium weld pools react differently<br />

to the arc, gravity and surface tensions acting on them, resulting in unconventional bead shapes. Due to<br />

magnesium’s high vapour pressure and the small interval between melting and vaporising (600-1100°C),<br />

wire transfer during gas-metal arc welding can result in explosive expulsion <strong>of</strong> material (i.e. spatter). Also,<br />

like aluminium and titanium, magnesium has a high affinity for oxygen. For welds made with arc processes<br />

using electrode negative polarity, surface oxides must be removed prior to welding in order to avoid thick<br />

(crusty) oxides on the weld surface. Use <strong>of</strong> alternating current or variable polarity also helps in this regard.<br />

For gas-metal arc welds made with electrode positive polarity, a thin surface oxide surface layer on the joint<br />

may actually be beneficial for arc stability. Hot and cold cracking are not normally a problem, and porosity<br />

originating from hydrogen contamination is seldom encountered.<br />

Mg-alloys have typically been used in selected automotive and aerospace applications, primarily in the form<br />

<strong>of</strong> die castings. With the recent development <strong>of</strong> rolled sheet, however, there exist many new possibilities<br />

for welded constructions, with the higher strength wrought alloys feeding the need for weight reduction. In<br />

addition, new power supply technology has allowed the gas-metal arc process to operate in the short circuit<br />

mode with reduced spatter. This process shows promise for the welding <strong>of</strong> thin section magnesium, as does<br />

the use <strong>of</strong> laser and friction stir welding processes. Laser beam welding <strong>of</strong> AZ31 sheets with and without<br />

wire additions provides excellent hardness, ductility, fatigue (including crack propagation) and fracture<br />

properties for the butt-joints.<br />

Due to the difficulty in forming HCP magnesium, filler wire <strong>of</strong> good quality is only available from a few<br />

suppliers, and is typically limited to one or two sizes (e.g. 1.2 and 1.6 mm dia.) suitable for gas-metal arc<br />

welding. To solve this task for gas-tungsten arc or laser welding, finer wires have to be developed in the<br />

near future. In addition, there are typically only a few alloys available in wire form: e.g. AZ31 and AZ61. The<br />

question then becomes, what is the desired filler composition so as to optimise joint properties in terms <strong>of</strong><br />

corrosion resistance? Weld metal is <strong>of</strong>ten the weak link in magnesium welds, suggesting that improvements<br />

are possible with filler alloy development. For use <strong>of</strong> welded components in automotive applications, fatigue<br />

and in particular corrosion fatigue <strong>of</strong> welds becomes an important design criterion. When dealing with a<br />

reactive metal like magnesium, corrosion must always be considered when evaluating lifetime behaviour.<br />

While limited data is available for magnesium weld fatigue, little or no information is available for weld<br />

24 <strong>Improving</strong> <strong>Global</strong> <strong>Quality</strong> <strong>of</strong> <strong>Life</strong> Through Optimum Use and Innovation <strong>of</strong> Welding and Joining Technologies

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