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Thermit welding of chromium- vanadium rail steel - Vanitec

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<strong>Thermit</strong> <strong>welding</strong> <strong>of</strong> <strong>chromium</strong>-<strong>vanadium</strong> <strong>rail</strong> <strong>steel</strong><strong>Thermit</strong> <strong>welding</strong> <strong>of</strong> <strong>chromium</strong><strong>vanadium</strong><strong>rail</strong> <strong>steel</strong>H. D. Fricke (U.S. <strong>Thermit</strong> Inc.)<strong>Thermit</strong> <strong>welding</strong> techniques are' discussed withparticular reference to short preheat cycles and itssuitability to the <strong>welding</strong> <strong>of</strong> high-strength <strong>chromium</strong><strong>vanadium</strong><strong>rail</strong>s. The composition <strong>of</strong> the <strong>Thermit</strong> <strong>steel</strong>used is adjusted to match the phase-transformationcharacteristics <strong>of</strong> <strong>chromium</strong>-<strong>vanadium</strong> <strong>steel</strong>s. Toavoid a martensitic or bainitic structure in the finishedweld, the cooling cycle must be controlled.1. INTRODUCTION<strong>Thermit</strong> <strong>welding</strong> has been applied as a regular <strong>welding</strong>process since 1898, when the aluminothermic reaction betweena metal-oxide and aluminum was discovered by HansGoldschmidt. This type <strong>of</strong> reaction is characterized by itsexothermic nature. Due to the difference <strong>of</strong> free energybetween a metal-oxide and aluminum-oxide, sufficient heatis generated to produce liquid <strong>steel</strong> or any other metal andalloy without applying energy from outside. All componentsfor the aluminothermic process are used as granules orpowders. Once the reaction is initiated by an external heatsource, the aluminum reduces the oxygen from the metaloxide,which will result in a liquid superheated metal andaluminum-oxide (AI203)' Since these two components aredifferent in density, they separate automatically and theliquid metal can be utilized for different <strong>welding</strong> applications,or just for the production <strong>of</strong> special metals or alloys.<strong>Thermit</strong> <strong>welding</strong> had its most important large-scaletechnical application during the early parl<strong>of</strong>this century as aprocess for joining heavy cross-sections for machinery,millhousings, rudderstocks, stern frames and pinions, but the<strong>welding</strong> <strong>of</strong> <strong>rail</strong> sections has become more and more importantwith the widespread installation <strong>of</strong> continuous welded<strong>rail</strong>. While the majority <strong>of</strong> <strong>rail</strong> <strong>steel</strong> is still rolled according tothe AREA or VIC specifications, the continuing developmenttowards faster speeds, higher axle loads and increasedtrain frequencies has led to increased requirements for <strong>rail</strong><strong>steel</strong>s with improved mechanical properties. The commoncarbon-manganese <strong>rail</strong> <strong>steel</strong>s do not satisfactorily withstandthese parameters and show gross plastic deformation andabrasive wear after relatively short periods <strong>of</strong> time. This hasled to the development <strong>of</strong> special alloyed <strong>rail</strong> <strong>steel</strong>s withhigher yield and tensile strength.During the course <strong>of</strong> development <strong>of</strong> these alloyed <strong>rail</strong><strong>steel</strong>s, one major demand has always been taken intoconsideration, that is weldability by both the in-plant<strong>welding</strong> as well as field <strong>welding</strong> processes such as <strong>Thermit</strong><strong>welding</strong>.2. RAILSTEELTYPESSince the time the first alloyed <strong>rail</strong> sections were rolledby various <strong>steel</strong> mills, extensive research has been done in ourmetallurgical laboratories to develop <strong>Thermit</strong> portions forthis new type <strong>of</strong> <strong>rail</strong>. The <strong>welding</strong> parameters had to bechanged in order to avoid critical cooling rates in the weld, aswell as the adjacent heat-affected <strong>rail</strong> sections, since, generallyspeaking, alloyed <strong>rail</strong> <strong>steel</strong> has different transformationtemperature characteristics which will result inembrittled bainitic or martensitic microstructures where theTable I. Chemistry <strong>of</strong> various alloyed <strong>rail</strong> <strong>steel</strong>sChemical CompositionManufacturer C,% Si,% Mn,% Cr,% Mo,% V,% P,% S,%0.55 Max. 0.80 0.80 Max. Max. Max.A to 0.70 to to - 0.30 0.03 0.030.75 1.30 1.30Max. Max. Max. Max.B 0.65 0.50 1.00 1.00 0.15 0.20 0.03 0.030.65 0.30 0.80 0.70 Max. Max.C to to to to - - 0.03 0.030.80 0.90 1.30 1.200.68 Max. 1.10 1.00 Max. Max.D to 0.35 to to - - 0.04 0.030.78 1.40 1.30E 0.76 0.84 0.37 1.49 - - 0.02 0.0263


<strong>Thermit</strong> <strong>welding</strong> <strong>of</strong> <strong>chromium</strong>-<strong>vanadium</strong><strong>rail</strong> <strong>steel</strong>frequency <strong>of</strong> 5.5 cycles/sec. Welds were tested up to 2.0million cycles and in case <strong>of</strong> no failure, discontinued.Figure 1 shows the Woehler curve which resulted fromtests made with SKY welds on <strong>chromium</strong>-<strong>vanadium</strong> <strong>steel</strong> <strong>rail</strong>sections, pr<strong>of</strong>ile S54.Slow bend tests showed increased fracture loads <strong>of</strong>about 10% higher in comparison to carbon-manganese <strong>steel</strong>welds, but as anticipated somewhat lower deflection. As inthe case <strong>of</strong> welds made with heat-treated carbon-manganese<strong>rail</strong> <strong>steel</strong>, the AREA specifications calling for 25.4 mm (1 in)deflection in the commonly known AREA test arrangement,cannot always be met. This can be attributed to the fact thatelements such as <strong>chromium</strong>-<strong>vanadium</strong> and molybdenum willincrease the strength by refinement <strong>of</strong> the interlamellarspacing, as well as the precipitation <strong>of</strong> carbides, but will alsoresult at the same time in a decrease <strong>of</strong> ductility.Figure 2 shows the correlation between carbon contentand deflection <strong>of</strong> welds made with <strong>chromium</strong>-alloyed <strong>rail</strong><strong>steel</strong>.4. TRANSFORMATION CHARACTERISTICSFigure 3 shows the typical chemistry <strong>of</strong> a <strong>Thermit</strong> <strong>steel</strong>and its corresponding CCT diagram. The <strong>steel</strong> was austenitizedfor 30 min at 950°C (1742°F) resulting in a grain size <strong>of</strong>ASTM No. 3, which is comparable to the grain size in the1000800°uw'a::>I-600«a:w f--Cl.~ 400I-200.....Act = 720°CAi-- MsRail Steel U.S.A.132 Ib/yd (66 kg/m) -18321472u..°w'1.00IC:M'Va:1001112. ~ «a:100l(9100\\It -1\wCl., IP", \ItCompleteferrite/pearlitetransformation 2I'752 w !-Iat 2i\ "nd 20sec\r-,.\\392M \\ '\\ \"1 sec 10102 103 1041 min 10 102TIMEFig.4 CCT diagram for carbon-manganese (AREA) <strong>rail</strong><strong>steel</strong>. (Composition: C, 0.79%; I\1n, 0.88%; Si, 0.11%.Tensile strength: 900 N/mmz (130 ksj)) (Taken fromW. Ahlert, ETR, 18 (1969), pp. 468-520)1000800u0wa:~ 600«a:wCl.~ I-400200II-=Act'" 725°CIIiA.--1.""',"\\.Cr-Mn Alloyed Rail (Steel <strong>of</strong> Special Grade 1" fi "100..Complete Ferrite/PealTransformation1 sec 10 102 103104Pat 580° C and 220 sec'\ \"CommendableB-Cooling CurveMs 40'\""MIro..\.18321472u..0wrlite ~1112 !;ta:wCl.2752 ~392II1 min 10TIMEFig.5 CCT diagram for 1% <strong>chromium</strong> <strong>steel</strong>. (Composition:C, 0.77%; Cr, 1.07%; Mn, 1.06%; Si, 0.39%. Tensilestrength: 1080 N/mm2 (157 ksi)) (Taken from W.Ahlert, ETR, 18 (1969), pp. 468-520)10265


Vanadium in Rail Steels<strong>Thermit</strong> <strong>steel</strong> adjacent to the <strong>rail</strong>. Even though the maximumtemperature in a weld is significantly higher, the total timeinterval during which the weld will remain in this hightemperature range is considerably shorter, consequentlyresulting in the same grain size.A time/temperature curve, taken at the fusion linebetween the <strong>Thermit</strong> and the <strong>rail</strong> <strong>steel</strong> is plotted in the CCTdiagram. It demonstrates that in the area with the highestcooling rate, the microstructure transforms fully into pearlite.This time/temperature curve, shown in Fig. 3, was takenin a weld made with the SKY <strong>Thermit</strong> <strong>welding</strong> process, wherethe <strong>rail</strong> ends were preheated for 2 min. Welds made with theSoW <strong>Thermit</strong> <strong>welding</strong> process, which requires a longerpreheating time <strong>of</strong> up to 10 min, naturally resulted in slower,even less critical cooling rates. The time/temperature curve <strong>of</strong>a weld made with the self-preheat (SPH) <strong>Thermit</strong> processwith no external preheat, is almost identical to the onemeasured with the SKY process. This process is accomplishedthrough a different weld design as well as a differentflow and larger amount <strong>of</strong> the liquid <strong>steel</strong>, where one-third <strong>of</strong>it is used only for the purpose <strong>of</strong> preheating and washing the<strong>rail</strong> ends. Furthermore, it should be mentioned that thechemical analysis <strong>of</strong> welds made with the SPH process isdifferent, with higher silicon and lower manganese content.This higher Si content <strong>of</strong> up to 1.5%is due to the different rawmaterials used for the manufacture <strong>of</strong>the molds, where the Siis absorbed by the liquid <strong>Thermit</strong> <strong>steel</strong> from the mold.Figures 4 and 5 show the CCT diagram for a regularAREA carbon-manganese <strong>steel</strong> and for a 1% <strong>chromium</strong> <strong>rail</strong><strong>steel</strong>. Other diagrams for the different variations as shown inTable I, have been published in several papers. The CCTdiagram for a 1% <strong>chromium</strong> <strong>steel</strong> demonstrates that for atemperature range from 800°C (1472°F) to 500°C (932°F), atleast 200 sec are required for fully pearlitic transformations,whereas the same temperature interval for a regular carbonmanganese"<strong>steel</strong>,according to AREA specifications, might becrossed within 50 sec.w I-1400? 1000w 0::::>I-


--- -------<strong>Thermit</strong> <strong>welding</strong> <strong>of</strong> <strong>chromium</strong>-<strong>vanadium</strong><strong>rail</strong> <strong>steel</strong>A comparison between Figs. 3 and 5 shows that control<strong>of</strong>the cooling rate is most important in the heat-affected zone<strong>of</strong> the <strong>rail</strong> <strong>steel</strong> where precautionary steps have to be taken inorder to avoid embrittled microstructures. This is mostimportant with the preheated types <strong>of</strong> <strong>Thermit</strong> welds, wherethe excess weld metal, the so-called riser on top <strong>of</strong> the <strong>rail</strong>Fig- 8 Macroetched cross-section <strong>of</strong> a SPH weldhead will be removed either by hot chiselling or shearing aftersolidification <strong>of</strong> the weld. Immediately thereafter, the sheared<strong>of</strong>f upper part <strong>of</strong> the mold containing hot <strong>steel</strong> and slagshould either be placed back on to the top <strong>of</strong> the weld or theweld, as well as the adjacent <strong>rail</strong> sections, should be coveredwith an insulating blanket. Furthermore, head and base <strong>of</strong>the <strong>rail</strong> on both sides <strong>of</strong> the mold-half should be evenlypost heated for approximately 2 min.Figure 6 shows three thermal cycles <strong>of</strong> SKV welds,cooled by different methods. Optimum results are accomplishedby wrapping the weld with an insulating blanket afterthe excess metal has been removed. If the SPH process isapplied for <strong>Thermit</strong> <strong>welding</strong>, the head riser does not have tobe removed until the weld cools to approximately lOO°C(2lO°F) or less. Until that time the mold remains in place andwill protect the weld and heat-affected zone from cooling to<strong>of</strong>ast. Insulating blankets are not required, as the wide moldhalves overlap the weld and <strong>rail</strong> section on both sides by 9.5cm (3.74 in). However, in order to build up a heat wall andprevent the <strong>rail</strong> sections from cooling too fast, a postheatingtreatment should be applied in the same manner as thatrecommended for the SKV and SoW processes.Figure 7 shows the cooling curve <strong>of</strong> a <strong>Thermit</strong> weldmade with the SPH process, where the molds remained inposition for the entire cooling period.~. THERMALTRANSFORMATION OF THE RAILSTEELDepending upon the gap size between the two <strong>rail</strong>sections to be welded as well as the total preheating time, thewidth <strong>of</strong> the heat-affected zone is developed differently.Figures 8, 9 and lO show some macro-etched cross-sectionswhich are characteristic for each process. The total width <strong>of</strong>the heat-affected zone is bordered by the two light verticallines, where pearlite has been spheroidized but not as yetaustenitized- Figure 11 shows the microstructure in thetransition zone from the weld to the heat-affected <strong>rail</strong> <strong>steel</strong>.Fig.9 Macroetched cross-section<strong>of</strong> a SKV weld67


<strong>Thermit</strong> <strong>welding</strong> <strong>of</strong> <strong>chromium</strong>-<strong>vanadium</strong><strong>rail</strong> <strong>steel</strong>metallurgical standpoint is to be considered as a casting, thisdifference in hardness will balance itself out as soon as the <strong>rail</strong>is exposed to regular train service, and the <strong>rail</strong> and the<strong>Thermit</strong> <strong>steel</strong> will eventually have the same end hardness.The most heat-affected zone <strong>of</strong> the <strong>rail</strong>, next to the fusion linewith the weld, having a maximum grain growth <strong>of</strong> theaustenite, shows the highest peak in hardness, whereas thespheroidized pearlite results in the area <strong>of</strong> lowest hardness.7. SPECIAL PRECAUTION WHEN WELDINGALLOYED RAIL STEELDespite the fact that all types <strong>of</strong> alloyed <strong>rail</strong> <strong>steel</strong> withchemistries such as those indicated in Table I show very goodweldability characteristics for the different <strong>Thermit</strong> <strong>welding</strong>processes, there are some points that require specialattention.7.1 Hot shearingIf the excess metal on top <strong>of</strong> the head is removed byshearing, the waiting time between the pouring <strong>of</strong> the<strong>Thermit</strong> into the mold and the start <strong>of</strong> the shearing operation,should be longer than normal if a single blade type shear isused. If the waiting time is not long enough, it will result inhot tearing in the center <strong>of</strong> the weld (Fig. 13).This can beeliminated by applying the double blade shear in which twoblades shear the weld from opposite sides. Furthermore, testshave shown that the tendency for hot tearing will be lessenedwith shorter preheating periods.Fig.136. HARDNESSHot tearing after shearing <strong>Thermit</strong> <strong>steel</strong> too earlyThe heat pattern as shown in Figs. 8 to 10 is reflected inthe hardness pr<strong>of</strong>iles taken in the head parallel to the runningsurface, see Fig. 12.The hardness <strong>of</strong> the weld is slightly higherthan that <strong>of</strong> the unaffected <strong>rail</strong> <strong>steel</strong>. As the rolled <strong>steel</strong> has atendency to work-harden more than the weld, which from a7.2 Torch cuttingIf torch cutting is necessary, which will be the casewhenever no abrasive saw is available, and the <strong>rail</strong> ends haveto be cut for preparation <strong>of</strong> the gap for <strong>Thermit</strong> <strong>welding</strong>, the<strong>rail</strong> ends must be preheated according to the instructions <strong>of</strong>the different <strong>rail</strong> manufacturers. The preheating temperatureshould be 500°-600°C (930°-111OaF)for at least 0.2 cm (0.08in) on both sides <strong>of</strong> the projected torch cut, and approximately50°C (120°F) at a distance 1.0 m (approx. 3 ft) onboth sides. If the <strong>Thermit</strong> weld is not to be made immediately,the <strong>rail</strong> sections have to be preheated for another 5 min at atemperature <strong>of</strong> approximately 500°C (930°F). Arc <strong>welding</strong>cannot be performed without preheating to 5000~600°C(930°-11 10°F), and this temperature should be maintainedduring the whole <strong>welding</strong> operation.DISCUSSION ON<strong>Thermit</strong> <strong>welding</strong> <strong>of</strong> <strong>chromium</strong><strong>vanadium</strong><strong>rail</strong> <strong>steel</strong>H. D. FrickeF. B. FLETCHER (Climax Molybdenum) I would like totake issue with one statement you made in your presentation:You attribute the smaller deflections you observe in alloy<strong>steel</strong>s to a decrease in ductility <strong>of</strong>the <strong>steel</strong> due to alloying. Wefind that, in general, one cannot conclude that the addition <strong>of</strong><strong>chromium</strong>, <strong>vanadium</strong>, and molybdenum decreases the ductility.In fact, the tensile ductility <strong>of</strong> <strong>steel</strong> is not necessarilyadversely affected by the addition <strong>of</strong> these alloying elements.The explanation for the apparent decrease in deflection youobserve for alloy <strong>steel</strong>s lies in the fact that there is ameasurably greater degree <strong>of</strong> local deformation under theloading points in the s<strong>of</strong>ter unalloyed <strong>steel</strong>s. The alloy <strong>steel</strong>sdo not deform under the loading points as much as thecarbon manganese <strong>steel</strong>s, so they appear to give smallerdeflections.H. D. FRICKEEven though the weld is called a weld, it isbasically a casting, and that should also make a contributionto the ductility we measured.S. MARICH (BHP Melbourne Research Labs) Is there anoptimum hardness <strong>of</strong> the weld metal relative to that <strong>of</strong> the<strong>rail</strong>?H. D. FRICKE Our experience has been that the <strong>rail</strong> <strong>steel</strong>work hardens faster than the weld metal and eventually, aftera certain gross tonnage has passed over the joint, we end upwith the same hardness in the <strong>rail</strong> as in the weld. To take thisinto account, the weld should, as a general rule, be about 20points Brinell harder than the <strong>rail</strong> initially. I must emphasize,though, that this experience is based on carbon-manganese<strong>rail</strong>s. The same situation may not hold in alloy <strong>rail</strong>s andwelds, where contributions <strong>of</strong> the various alloying elementsmake the situation much more complex.69


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