13. Special Processes
Transcription
13. Special Processes
13. Special Processes 13. Special Processes 183 Apart from the welding processes explained earlier there is also a multitude of special welding processes. One of them is stud welding. Figure 13.1 depicts different stud shapes. Depending on the application, the studs are equipped with either internal or external screw threads; also studs with pointed tips or with corrugated shanks are used. In arc stud welding, a distinction is basically made between three variations. process Figure 13.2. depicts the three variations – the differences lie in the kind of arc ignition and in the cycle of motions during rammed flange the welding process. br-er13-01e.cdr The switching arrangement of an arc stud weldFigure 13.1 ing unit is shown in Figure 13.3. Besides a power drawn-arc stud welding capacitordischarge stud welding with tip ignition drawn-arc stud welding with ferrule ignition source which produces high currents for a shorttime, a control as well as a lifting device are necessary. ceramic ferrule cold-upset tip ignition ignition ring br-er13-02e.cdr Figure 13.2 2005 13. Special Processes 184 In drawn-arc stud welding the stud is first mounted onto the plate, Figure 13.4. The arc is ignited by lifting the stud and melts the entire stud diameter in a short time. When stud and base plate are fused, the stud is dipped into the molten weld pool while the ceramic ferrule is forming the weld. After the solidification of the liquid weld pool the ceramic ferrule is knocked off. Figure 13.5 illustrates tip ignition stud welding. lifting device The tip melts away imme- control device diately after touching the plate and allows the arc to stud holding device welding time adjustment be ignited. The lifting of the stud stud is dispensed with. When the stud base is molpower source ten, the stud is positioned onto the partly ceramic ferrule V workpiece A molten br-er13-03e.cdr workpiece. Studs with diameters of up Figure 13.3 to 22 mm can be used. Welding currents of more start 3 lifting L dipping > (L + P) 4 L projection P 2 L end current materials, see Figure 13.6. Problematic are the differ- 1 time P ess allows to join different 0 P The arc stud welding proc- stud movement than 1000 A are necessary. ent melting points and the heat dissipation of the individual materials. Aluminium time br-er13-04e.cdr studs, for example, may not be welded onto steel. Figure 13.4 2005 13. Special Processes 185 The relatively high welding currents in the arc stud welding process cause the somewhat troublesome side-effects of the arc blow. Figure 13.7 depicts different arrangements of current contact points and cable runs and illustrates the developing arc deflection (B,C,E). A, D and F show possible countermeasures. a b c d In high-frequency welding of pipes the energy input into the workpiece may be carried out via sliding contacts, as shown in Figure 13.8, or via rollers, as shown in Figure 13.9. Only the high-frequency technique allows a safe current transfer in spite of the scale or oxide layers. Through the skin effect br-er13-05e.cdr © ISF 2002 Phases of Capacitor-Discharge Stud Welding With Tip Ignition the current flows only conditionally at the surface. Therefore no thorough fusion of thickFigure 13.5 wall pipes may be achieved. unalloyed sructural steel S235J0 and/or comparable steels other unalloyed steels stainless steels acc. DIN EN 17440 heat resisting steels acc. SEW 470 aluminium and aluminium alloys unalloyed structural steel S235J0, S355J0 and/or comparable steels (acc. DIN EN 10 025) 1 2 3 2 0 other unalloyed steels 2 2 3 2 0 stainless steels acc. DIN EN 17440 3 3 1 3 0 heat resisting steels acc. SEW 470 2 2 2 2 0 aluminium and aluminium alloys 0 0 0 0 2 stud material base meatl explanation of the weldability classification numbers: 1 = well suitable (transmission of energy) 2 = suitable (transmission of energy possible with restriction) 3 = suitable only up to a point (not for transmission of energy 0 = not possible br-er13-06e.cdr Figure 13.6 2005 13. Special Processes 186 Only welding of small wall thicknesses is profitable – as the weld speed must be greatly reduced with in- A creasing wall thicknesses, B Figure 13.10. C D br-er13-07e.cdr Figure 13.7 rotary transformer moving direction of the pipe ~ pressure rollers Isolation copper electrode wheel (water-cooled) sliding contacts (fixed) slot pipe ∼ interstage transformer pressure rollers HF-valve generator br-er13-08e.cdr counterpressure rollers © ISF 2002 br-er13-09e.cdr Rotary Transformer Resistance Welding High-Frequency Welding of Pipes Figure 13.8 © ISF 2002 Figure 13.9 2005 13. Special Processes 187 In induction welding – a process which is 80 4 5 used frequently nowadays – the energy input 6 is received contactless, Figure 13.11. Varying 3 m/min magnetic fields produce eddy currents inside welding speed 2 the workpiece, which again cause resistance heating in the slotted tube. A distinction is 40 made between coil inductors (left) and line 1 inductors (right). 20 Also in case of induction welding flows the 0 0 2 4 6 8 10 wall thickness 12 mm 16 current flows only close to the surface areas of the pipe. Only the current part which 1: 36 kA; 100 kVA; 60 Hz 2: 57 kA; 200 kVA; 60 Hz 3: 75 kA; 300 kVA; 60 Hz 4: 125 kA; 500 kVA; 60 Hz 5: 150 kA; 1200 kVA; 120 Hz 6: 200 kA; 1850 kVA; 120 Hz reaches the joining zone and causes to fill the gap may be utilised. Figure 13.12 illustrates Br-er13-10e.cdr © ISF 2002 Welding Speeds in HF-Resistance Welding two current paths. On the left side: the useful current path, on the right side: the useless current path which does not contribute to the Figure 13.10 Figure 13.13 fusion of the edges. shows the moving direction of the pipe effective depth during the moving direction of the pipe inductive heating for different materials, in dependence on the frequency. As pressure rollers soon as the Curie tempera- pressure rollers ture point is reached, the effective depth for ferritic coil inductor steels increases. line inductor br-er13-11e.cdr Figure 13.11 2005 13. Special Processes 188 The application of the induction l δ2 welding method of more than 100m/min, b b allows high welding speeds δ1 Figure 13.14. δ1 s d δ2 b width of the heating inductor s wall thickness of the pipe δ1 current penetration depth on pipe backside d l current penetration depth at the strip edges outside diameter of the pipe distance inductor- welding point br-er13-12e.cdr Figure 13.12 160 100 corrective factor effective depth δ 20 mm 10 8 6 4 1 m/min 2 3 2 1,0 0,8 0,6 0,4 4 5 120 % 0 6 0 7 50 100 mm 200 pipe diameter 100 high frequency 200 - 450 kW 0,2 weld speed 0,10 0,08 0,06 0,04 0,02 1 4 1 2 3 4 5 6 br-er13-13e.cdr 7 10 frequency f steel (ferritic steel (austenitic) brass aluminium copper brass copper aluminium steel (ferritic) 100 200 kHz 1000 800°C 20....1400°C 800°C 600°C 850°C 20°C 20°C 20°C 20°C 80 60 600 kW 40 450 kW 300 kW 20 200 kW 60 kW 100 kW 150 kW 0 0 © ISF 2002 2 4 8 10 12 14 wall thickness br-er13-14e.cdr Standard Values of the Effective Depths During Inductive Heating Figure 13.13 6 16 mm 20 © ISF 2002 Welding Speeds in Induction Welding Figure 13.14 2005 13. Special Processes 189 Aluminothermic fusion welding or cast welding is mainly used for joining 3FeO + 2Al Al2O3 + 3Fe - 783 kJ railway tracks on site. A crucible is filled with a mix- Fe2O3 + 2Al ture consisting of alumin- Al2O3 + 2Fe - 758 kJ ium powder and iron ox- 3Fe3O4 + 8Al ide. An exothermal reac- 4Al2O3 + 9Fe - 3012 kJ tion is initiated by an igniter – the aluminium oxidises br-er13-15e.cdr and the iron oxide is reduced to iron, Fig- ure 13.15. The molten iron Figure 13.15 flows into a ceramic mould which matches the contour of the track. After the melt has cooled, the mould is knocked off. Figure 13.16 shows the process assembly. Explosion welding or explosion cladding is fre- quently used for joining mould runner gate riser slag mould preheating gas fuel workpiece air riser c b dissimilar materials, as, for example, steel/alloyed cut A-B unalloyed steel, cop- thermit steel steel/aluminium. The materials which are to be joined are pressed together by a A riser thermit bulge weld cross-section b or blow-hole orifice thermit slag thermit crucible slag mould per/aluminium workpiece thickness of the cast b channel between riser and runner gate runner gate blow-hole orifice iron or sand plug B foundry sand riser runner gate workpiece cast-around bulge br-er13-16e.cdr shock wave. Wavy transitions develop in the joining area, Figures 13.17 and Figure 13.16 13.18. 2005 13. Special Processes 190 The determined cladding adhered to during a) explosive charge buffer flyer plate igniter the parent plate anvil vd t welding speed is too low, vd vP B α A' A vF K If the welding speed is A' β B' K vK t β B vP B' vF A vK B 90 - β + α /2 exceeded, the develop- v ment of the waves in the joining zone is erratic. explosive charge buffer flyer plate igniter parent plate anvil Amboß welding process. If the lack of fusion is the result. b) d speed must be strictly F vP β K vK vF 90 - α /2 B' K β vK = vD B vP B' br-er13-17e.cdr Figure 13.19 shows the critical cladding speeds for different material com- Figure 13.17 binations. Figure 13.20 shows a diagrammatic representation of a diffusion welding unit. Diffusion welding, like ultrasonic welding, is welding in the solid state. The surfaces which are to be joined are cleaned, polished and then joined in a vacuum with pressure and temperature. After a certain time (minutes, right up to several days) joining is achieved by diffusion processes. The advantage of this costly welding method lies in the possibility of joining dissimilar materials without taking the risk of structural transformation due to the heat input. Figure 13.21 shows several possible material combinations. The joining of two extremely different materials, as, e.g. austenite and a zirconium alloy, may be obtained by several interBr-er13-18e.cdr mediate layers. Figure 13.18 2005 13. Special Processes 191 measuring amplifier -1 critical speed [m s ] materials flyer plate/ parent plate working pressure 1,33 mPa vk1 vk2 vk3 600 1000 >4000 copper/ copper 1200 1600 >3600 steel/ steel 2100 2700 >3900 copper/ aluminium 1000 1400 aluminium/ steel 1200 1600 cooper/ steel 1400 2400 aluminium/ zinc 500 1000 3000 copper/ zinc 800 1400 3300 hydraulic aggregate unit P aluminium/ aluminium workpieces HFgenerator pumping station recorder p,T = f(t) br-er13-19e.cdr loading device © ISF 2002 br-er13-20e.cdr Schematic Representation of a Diffusion Welding Unit Critical Cladding Speeds in Explosive Cladding tantalum niobium zirconium Figure 13.22 shows the structure of a joint tungsten molybdenum titanium nickel copper aluminium stainless steel tool steel Figure 13.20 structural steel cast iron Figure 13.19 material © ISF 2002 tantalum where nickel, copper and vanadium had been used as intermediate layers. As the diffusion of the individual components takes place only niobium zirconium in the region close to the surface, very thin tungsten molybdenum layers may be realised. titanium nickel copper aluminium stainless steel tool steel very good weld quality structural steel cast iron good weld quality bad weld quality not tested/ results not reported br-er13-21e.cdr © ISF 2002 Possible Material Combinations for Diffusion Welding Figure 13.21 2005 13. Special Processes 192 In cold pressure welding in contrast to diffusion welding - a deformation is produced by the high contact pressure in the bonding X10CrNiTi18 9 Ni Cu V Zr2Sn plane, Figure 13.23. The joint surfaces are moved very close towards each other, i.e., to the atomic distance. Through transpobr-er13-22e.cdr sition processes as well as through adhesion forces can joining of similar and Figure 13.22 dissimilar materials be realised. Ultrasonic welding is used as a microwelding method. The process principle is shown in Figure 13.24. The surface layers of overlap arranged plates are destroyed by applying mechanical vibrator energy. At this instance are joining surfaces deformed by very short localised warming up and point-interspersed connected. The joining members are welded under pressure, where one part small amplitudes (up to 50 µm) relative to the other is moved with with ultrasonic frequency. dies d1 As far as metals are concerned, the vibratory vector is in the joining zone, in specimen A contrast to ultrasonic weld- guide and buffer ing of plastics. The ultra- specimen B d2 sonics which have been produced by a magne- tostrictive transducer and br-er13-23e.cdr transmitted by a sonotrode lie in the frequency range of 20 up to 60 Hz. Figure 13.23 2005 13. Special Processes 193 Figure 13.25 shows possible material combinations for ultrasonic welding. Further microwelding processes are methods which HFgenerator are also called heated ele- process observation optics ment welding methods, as, pressure force for sonotrode example, nailhead bonding and wedge bond- sonotrode tip ing. These methods are workpiece applied in the electronics anvil industry for joining very fine ultrasonic vibrator wires, as, for example, gold br-er13-24e.cdr wires from microchips with aluminium strip conductors. Figure 13.24 In wedge bonding a wire is positioned onto the contact point via a feeding nozzle. The welding wedge is lowered and the wire is welded with the aluminium thin foil, Figure 13.26. The wire is cut with a cutting aluminium+alloy beryllium+alloy copper, Cu-Zn-alloy germanium gold iron magnesium+alloy molybdenum+alloy nickel+alloy palladium+alloy platin+alloy silicon silver+alloy tantalium+alloy tin titanium+alloy tungsten+alloy zirconium+alloy tool. In nailhead bonding, the wire which emerges from the feeding nozzle may have diameters from 12 to 100 µm. By a reducing hydrogen flame its end is molten to a globule, Figure 13.27. The nozzle then presses this globule onto the part aimed at and shapes it into a nail head. Figure 13.28 depicts this type of weld. aluminium+alloy beryllium+alloy copper, Cu-Zn-alloy germanium gold iron magnesium+alloy molybdenum+alloy nickel+alloy palladium+alloy platin+alloy silicon silver+alloy tantalium+alloy tin titanium+alloy tungsten+alloy zirconium+alloy A further method related to welding is soldering. The process principle of soldering is briefly explained in Figure 13.29. br-er13-25e.cdr © ISF 2002 Possible Material Combinations for Ultrasonic Welding Figure 13.25 2005 13. Special Processes 194 heated wedge (tungsten-carbide) 5-50 µm gold wire wedge bonding Al-strip conductor cutting tool br-er13-26e.cdr Figure 13.26 heated wedge (tungsten-carbide) H2-flame 5-50 mm gold wire wedge bonding Al-strip conductor nailhead br-er13-27e.cdr Figure 13.27 br-er13-28e.cdr Figure 13.28 2005 13. Special Processes 195 The individual soldering methods are classified into different mechanisms depending on the type of heating, Figure 13.30. There are two basic distinctions: soft soldering (melting temperature of the solder is approx. up to 450°C) and brazing (melting temperature of the brazing solder is approx. up to 1100°C. For high-temperature soldering solders with high melting points (melting temperature is approx. up to 1200°C) are used. This process is frequently subject to automation. In soldering, atomar forces of attraction are effective. Similar and dissimilar metals are joined by addition of a solder with a low melting point. In the boundary area classification according to the type of heating: transposition processes occur between solder and base metal. This is called a “two-dimensional”diffusion. In the subsequent diffusion glowing phase - flame brazing (high-temperature soldering) the solder may be - iron soldering completely absorbed by the base metal. - block brazing A distinction is made between soft soldering (melting - furnace soldering temperature of the solder is below 450°C) and brazing - salt bath brazing (melting temperature of the solder is 450°C up to 1100°C) as well as high-temperature soldering (melting - dip soldering temperature of the solder is up to 1200°C). Heating of - wave soldering the component for melting the solder may be effected in - resistance soldering various ways. - induction brazing br-er13-29e.cdr © ISF 2002 br-er13-30e.cdr Classification of Soldering Methods Soldering - Definition and Process Principle Figure 13.29 © ISF 2002 Figure 13.30 2005