“…In Table 1 the best AISI joint welding parameters are reported as reference values; the optimum configuration resulted with two successive discharges under a force of 17 kN, established on the basis of visible weld morphology and static resistance results [6][7][8][9]. Table 1 The best welded AISI mock-up…”
Section: Welding For Mock-ups In Aeronautical Materialsmentioning
confidence: 99%
“…3) bears electro-magnetic forces and components deformations; a hydraulic system ensures compressive forces to perfectly hold the parts during welding. Large batteries (8320 µF with 3000 V circuits) are connected to the discharging lines through pulse transformers for the secondary welding circuit working at 10-15 V [6][7][8].…”
Section: The Multipoint Cdw Techniquementioning
confidence: 99%
“…This work is part of a European research program involving the authors and aeronautical industries, aimed to use CDW methods for repair applications [6][7][8][9][10][11][12][13][14][15][16].…”
Section: Introductionmentioning
confidence: 99%
“…CDW technology has been applied so far to realize circular butt welds up to 6 mm in diameter [3][4][5]; the authors recently explored the possibility of joining larger surfaces up to 12 mm in diameter in AISI 304 steel [6][7][8][9], Ti 6 Al 4 V, and Inconel 718 materials [10][11][12].…”
Section: Introductionmentioning
confidence: 99%
“…In this article, welded joints in the form of shaped mock-ups are presented; the welds are achieved with different combinations of welding parameters, on the basis of previous experimentations [6][7][8][9][10][11][12]. The chosen materials are the α/β titanium alloy Ti 6 Al 4 V and Inconel 718 nickel super-alloy, widely used for aeronautical compressors and turbine blades [17].…”
Capacitor discharge welding (CDW) is analysed to repair aeronautical components made with Inconel 718 and Ti 6 Al 4 V alloys, currently used for compressor and turbine applications.The CDW process is a resistance welding technology; it makes use of high-intensity current pulses, discharged by large capacitors. The use of multipoint contact features allows us to reduce stress concentration effects at the weld toe, obtaining thin weld beads, and achieve good material continuity.Base material and as-welded specimens with the same heat treatment were welded, using different parameters, and mechanically tested; the weld bead extension and the microstructural aspect of the welds were finally analysed.The development of advanced technologies for aeronautical components repair is of particular interest and the structural performances at room and working temperatures for capacitor discharge welds have to be carefully studied.
“…In Table 1 the best AISI joint welding parameters are reported as reference values; the optimum configuration resulted with two successive discharges under a force of 17 kN, established on the basis of visible weld morphology and static resistance results [6][7][8][9]. Table 1 The best welded AISI mock-up…”
Section: Welding For Mock-ups In Aeronautical Materialsmentioning
confidence: 99%
“…3) bears electro-magnetic forces and components deformations; a hydraulic system ensures compressive forces to perfectly hold the parts during welding. Large batteries (8320 µF with 3000 V circuits) are connected to the discharging lines through pulse transformers for the secondary welding circuit working at 10-15 V [6][7][8].…”
Section: The Multipoint Cdw Techniquementioning
confidence: 99%
“…This work is part of a European research program involving the authors and aeronautical industries, aimed to use CDW methods for repair applications [6][7][8][9][10][11][12][13][14][15][16].…”
Section: Introductionmentioning
confidence: 99%
“…CDW technology has been applied so far to realize circular butt welds up to 6 mm in diameter [3][4][5]; the authors recently explored the possibility of joining larger surfaces up to 12 mm in diameter in AISI 304 steel [6][7][8][9], Ti 6 Al 4 V, and Inconel 718 materials [10][11][12].…”
Section: Introductionmentioning
confidence: 99%
“…In this article, welded joints in the form of shaped mock-ups are presented; the welds are achieved with different combinations of welding parameters, on the basis of previous experimentations [6][7][8][9][10][11][12]. The chosen materials are the α/β titanium alloy Ti 6 Al 4 V and Inconel 718 nickel super-alloy, widely used for aeronautical compressors and turbine blades [17].…”
Capacitor discharge welding (CDW) is analysed to repair aeronautical components made with Inconel 718 and Ti 6 Al 4 V alloys, currently used for compressor and turbine applications.The CDW process is a resistance welding technology; it makes use of high-intensity current pulses, discharged by large capacitors. The use of multipoint contact features allows us to reduce stress concentration effects at the weld toe, obtaining thin weld beads, and achieve good material continuity.Base material and as-welded specimens with the same heat treatment were welded, using different parameters, and mechanically tested; the weld bead extension and the microstructural aspect of the welds were finally analysed.The development of advanced technologies for aeronautical components repair is of particular interest and the structural performances at room and working temperatures for capacitor discharge welds have to be carefully studied.
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