Improving Global Quality of Life
Improving Global Quality of Life
Improving Global Quality of Life
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As another most important item, the prevailing stiffness (restraint intensity) in the repair area due to<br />
surrounding assembly groups and the associated strain constraint are usually much higher than during<br />
fabrication welding and have to be assessed before a repair welding procedure is carried out. For crackresistant<br />
repair welding, knowledge <strong>of</strong> the stresses introduced by welding is <strong>of</strong> major importance, especially<br />
when the repair welding procedure has to be carried out at a high shrinkage restraint. Since the research<br />
efforts in welding have been concentrated on the respective materials and the development <strong>of</strong> new welding<br />
procedures, investigation <strong>of</strong> the design aspects <strong>of</strong> repair welding probably represents a major target for<br />
the near future. This involves correct and quantitative evaluation <strong>of</strong> shrinkage restraints for repair welds,<br />
including the effects <strong>of</strong> the various joint types and reinforcements. With this respect, it has to be anticipated<br />
that the intensity <strong>of</strong> restraint as a quantitative parameter to evaluate structural stiffness in the near and far<br />
field <strong>of</strong> a joint will gain increasing importance. Additionally, a precise knowledge <strong>of</strong> the thermo-mechanical<br />
effects <strong>of</strong> the repair welding procedure on the residual lifetime has to be elaborated.<br />
It is also essential to determine the welding sequences with lowest possible likely stress-strain distribution<br />
during and after the repair <strong>of</strong> steel structures. This will allow it to enlarge the available load spectrum for<br />
later service. In this context, it has to be mentioned that interaction <strong>of</strong> concurrent repair welds has not been<br />
understood up to the present time.<br />
The failure resistance <strong>of</strong> a repair weld is also dependent on the applied filler materials and their transformation<br />
behaviour depending on metallurgical, welding and heat treatment parameters. With respect to the repair<br />
<strong>of</strong> steel structures and components, high-strength filler materials with correspondingly lowered martensite<br />
transformation temperatures have to be developed further to achieve lower residual stresses in the repair<br />
welding at respectively higher strength, i.e. service load capacities.<br />
It has also to be mentioned that a series <strong>of</strong> downstream methods are available for reducing welding-specific<br />
loads in repair joints or even for producing compressive residual stresses at the surface. Such technological<br />
procedures, like stress relieving, shot peening, peening, ultrasonic treatment etc., are generally very timeconsuming<br />
and costly and should be developed further regarding better applicability to repair welding.<br />
It can only be emphasised that repair welding requires decent component weld tests, rational residual<br />
stress evaluation and respective numerical calculations to achieve an actual increase in the life time <strong>of</strong> a<br />
component or structure and to avoid further failure origins in the repaired parts.<br />
4.4 Advanced design and structural integrity rules<br />
Recent advances in joining technologies together with new materials bring increased attention to the damage<br />
tolerance design, long service life and improved structural performance together with the developments in<br />
structural integrity assessment rules (e.g. BS 7910, API 579, R6, FITNET FFS) for the load-bearing structures.<br />
Recently, IIW Commission X has taken the task to develop IIW recommendations for the assessment <strong>of</strong><br />
structural integrity <strong>of</strong> welded structures by taking into account recent developments in this field. IIW FFS<br />
Recommendations for Fracture Assessment <strong>of</strong> Weld Flaws (Doc. X-1637-08/Rev.3, Vol. I Procedure, Vol.<br />
II Annex) document is now in its 3 rd revision and available as a working document.<br />
For example, in the field <strong>of</strong> aircraft manufacturing <strong>of</strong> new welded integral airframe structures, specific “Local<br />
Engineering” considerations in design and fabrication have potential for further improvements in local laser<br />
weld joint properties. Established damage tolerance assessment rules for conventional (riveted) structures<br />
may need to be further developed for welded integral airframe structures. Fatigue and fracture assessments<br />
can be over-conservative with current methods and this in turn may act as a limiting factor for successful<br />
implementation <strong>of</strong> advanced joining technologies in airframe manufacturing. Therefore, R&D efforts for better<br />
understanding <strong>of</strong> failure mechanisms <strong>of</strong> joints, development and validation <strong>of</strong> testing, structural integrity<br />
rules and hence an overall roadmap for LBW and FSW welded integral airframe structures are needed.<br />
30 <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