UDK 621.73:519.876.5 Original scientific article/lzvirni znanstveni članek ISSN 1580-2949 MTAEC9, 48(6)855(2014) THERMOMECHANlCAL PROCESSING OF MlCRO-ALLOYED STEEL TERMOMEHANSKA PREDELAVA MlKROLEGlRANEGA JEKLA Pavel Podany, Petr Martinek COMTES FHT lnc., Prumyslova 995, 334 41 Dobrany, Czech Republic ppodany@comtesfht.cz Prejem rokopisa - received: 2013-10-01; sprejem za objavo - accepted for publication: 2014-01-09 The paper deals with the thermomechanical processing of low-carbon micro-alloyed steel processed by means of a physical simulation on a unique device for simulating a real forging process. The main goal of the experiment was to assess the mechanical and microstructural properties of steel after additions of various amounts of micro-alloying elements. Heats with additions of V, Nb, Ti and Zr were prepared. Different austenitization temperatures and different deformations were applied. Their influence on the microstructure and mechanical properties was evaluated. Keywords: micro-alloyed steel, thermomechanical processing Članek obravnava termomehansko predelavo maloogljičnega mikrolegiranega jekla s fizikalno simulacijo na napravi za simulacijo realnega postopka kovanja. Glavni namen eksperimenta je bil ugotoviti mehanske lastnosti in mikrostrukturne značilnosti po dodatku različne količine mikrolegirnih elementov. Pripravljene so bile taline z dodatkom V, Nb, Ti in Zr. Uporabljene so bile različne temperature avstenitizacije in različne deformacije. Ocenjen je bil njihov vpliv na mikrostrukturo in mehanske lastnosti. Ključne besede: mikrolegirano jeklo, termomehanska predelava 1 INTRODUCTION High-strength low-alloy (HSLA) steels, or micro-alloyed steels, are designed to provide better mechanical properties and/or a greater resistance to atmospheric corrosion than conventional carbon steels. They are not considered to be alloy steels in the usual sense because they are designed to have specific mechanical properties rather than a specific chemical composition. ln order to realize the full strengthening potential of micro-alloying additions, it is necessary to use a soaking temperature prior to forging that is high enough to dissolve all the vanadium-bearing precipitates1. A soaking temperature above 1100 °C is preferred. For the Nb-Ti micro-alloyed steel a single-step austenite reheating temperature of 1150 °C provided better auste-nite conditioning than a higher reheating temperature of 1240 °C.2 According to34 a complete dissolution of carbonitride precipitates based on Nb occurs at 1140 °C in the interval of 1100-1200 °C.5 A further processing after the austenitization should consist of two-phase forging. A higher amount of deformation at an elevated temperature (about 1100 °C) facilitates a dynamic recrystallization. At this stage a critical amount of strain is required for the austenite grain refinement through repeated recrystallization. The second stage should be carried out below 900 °C, i.e., below the recrystallization temperature (TR) in order to make the austenite grain pancaked and to introduce interfacial defects into hot austenite. These interfacial defects in turn lead to an increase in the effective grain-boundary areas, enhancing the nucleation potency of ferrite. Subsequently, the micro-alloying elements come out of the solution with a decrease in the temperature, inhibiting the austenite grain growth by forming micro-alloying carbides or carboni-trides at these interfacial defects. Controlled cooling after the forging leads to the desired microstructure. A subsequent tempering could bring another strengthening due to the precipitation of micro-alloying elements. A tempering temperature of 600 °C and a dwell time of 4 hours are used in this experiment to meet the customer requirements. 2 EXPERIMENT The first part of the experiment was focused on a numerical simulation in the DEFORM 3D software. lt consists of a simulation of the controlled last step of the forging from the 500 mm bar diameter to the 460 (440) mm bar diameter (Figure 1). The forging takes place in the interval range of 940-800 °C. Numerical modelling allows accurate computing of a precise deformation and temperature distribution in every location of the real forged product according to choice. One location 40 mm below the bar surface was chosen for a further experiment - a physical simulation. lt is the location used for making the samples for mechanical testing. The second part of the experiment - the physical simulation - was focused on the samples with various micro-alloying additions. A physical simulator is a unique device with the possibilities of temperature and deformation control. The testing cell is set up on a modified MTS servo-hydraulic tensile-test machine. Figure 1: Distribution of the temperature for one-step open-die forging - numerical simulation in DEFORM 3D. Diagram in the upper left-hand corner shows the temperature distribution from the surface to the core. Slika 1: Razporeditev temperature pri enostopenjskem prostem kovanju - numericna simulacija z DEFORM 3D. Diagram levo zgoraj prikazuje razporeditev temperature od površine do sredine. It allows simulating the conditions of a location of the real piece with respect to the tem^perature/deforma-tion of the small specimen (Figure 2). The specimen shape is similar to the tensile-test sample (Figure 3) and it is resistive heated and loaded with tension and compression. A numerical simulation of the temperature distribution in the specimen was also done to make the simulation model more precise (Figure 4). The device parameters are: the maximum force of 250 kN, the heating rate of up to 150 °C/s, the cooling Figure 3: Specimen for the physical simulator Slika 3: Vzorec za fizikalni simulator rate of up to 150 °C/s, the maximum frequency of the cyclic loading of 30 Hz and the maximum forming velocity of 600 mm/s. The cooling rate of the physical simulator allows a simulation of cooling in various environments. It is possible to simulate cooling in the air, quenching in oil and water. Simulation of cooling in the water was chosen to be the best for this task. For a producer, cooling the whole bar in the water is also the simplest way of cooling. Various deformation processes were applied to the specimens in the simulator (see the example on Figure 5). Two samples (base heat B and V1) underwent a physical simulation of forging in the range of 980-840 °C. Other samples were processed in the range of 940-800 °C. Also, the applied deformation was doubled on some specimens and the austenitization temperature prior to the deformation varied from 1000 °C to 1150 °C. All the samples were annealed at 600 °C after the forging. The chemical compositions of the experimental heats with different micro-alloying additions and parameters of the physical simulation are summarized in Table 1. We prepared the samples for tensile and mini-Charpy (notch toughness) tests after the physical simula- Figure 2: Specimen in the physical simulator during thermomecha-nical processing Slika 2: Vzorec v fizikalnem simulatorju med termomehansko predelavo Figure 4: Numerical simulation of temperature distribution in the specimen during physical simulation Slika 4: Numericna simulacija razporeditve temperature v vzorcu med fizikalno simulacijo Figure 5: Example of temperature and deformation parameters of the physical-simulation process Slika 5: Primer temperature in deformacijskih parametrov pri fizikalni simulaciji tion and the subsequent heat treatment. The microstruc-ture was observed by means of a light microscope Nikon Epiphot 200 with the quantitative-image-analysis software NIS Elements 3.2. A detailed observation with the EDX measurement was done using a scanning electron microscope JEOL 6380. The last experiment was focused on the real experimental forging with a hydraulic press. One heat with no micro-alloys and one heat with Ti, Nb, V were subjected to identical forging processes. The aim was to compare the microstructures and mechanical properties of the non-micro-alloyed and micro-alloyed heats. 3 RESULTS AND DISCUSSION 3.1 Physical simulation Tensile tests were executed at room temperature. Prior to the testing, the specimen dimensions were measured and the original gauge length needed for determining elongation A was marked on each specimen. Some specimens were tested in the "mini-tensile" shape. This allowed preparing three specimens from one specimen after the physical simulation (Figure 6). Impact tests were performed on the instrumented Charpy pendulum with the impact energy of 15 J. Dimensions of the tested samples were 3 mm x 4 mm x 27 mm. The tests were executed at minus 46 °C. The minimum required values for the mechanical properties were as follows: Rpo.2 = 415 MPa; Rm = 530 MPa; A = 20 %; RVm^n. (-46 °c) = 2 J. Table 1: Chemical compositions of the analysed heats in mass fractions, w/% Tabela 1: Kemijska sestava analiziranih talin v masnih deležih, w/% Heat C Mn Si S Cr Ni P Cu Mo Ti V Nb Zr Applied deformation T/°C of deformation T/°C of austeniti-zation B 0.10 1.47 0.14 0.001 0.15 0.09 0.004 0.11 0.04 - - - - 1 980-840 1000 V1 0.10 1.43 0.09 0.001 0.15 0.09 0.004 0.12 0.04 - 0.060 0.045 - 1 980-840 1000 V2 0.11 1.55 0.15 0.001 0.14 0.09 0.004 0.12 0.04 — 0.090 0.047 — 2 940-800 1000 V3 0.10 1.36 0.1 0.001 0.14 0.09 0.004 0.11 0.04 - 0.170 0.047 - 2 940-800 1150 V4 0.10 1.29 0.1 0.001 0.14 0.09 0.004 0.11 0.04 - 0.130 0.042 - 2 940-800 1000 14 0.11 1.57 0.16 0.001 0.14 0.09 0.004 0.11 0.04 - 0.130 0.052 0.140 2 940-800 1150 15 0.10 1.49 0.13 0.001 0.14 0.09 0.004 0.11 0.04 — 0.130 0.050 0.195 2 940-800 1000 19 0.10 1.47 0.14 0.001 0.15 0.09 0.004 0.11 0.04 0.17 0.110 0.045 - 1 940-800 1000 23 0.10 1.40 0.12 0.001 0.15 0.09 0.004 0.11 0.04 0.20 0.200 0.050 - 2 940-800 1100 26 0.11 1.51 0.18 0.001 0.14 0.09 0.044 0.11 0.04 - - - - 2 940-800 1000 29 0.11 1.43 0.12 0.001 0.14 0.91 0.004 0.11 0.04 — — — — 2 940-800 1000 33 0.07 0.50 0.03 0.001 0.11 0.09 0.004 0.11 0.48 - - - - 2 940-800 1000 Table 2: Results of mechanical testing of thermomechanically processed specimens (with the physical simulator) Tabela 2: Rezultati mehanskih preizkusov na termomehansko predelanih vzorcih (na fizikalnem simulatorju) Specimen Rp0.2/MPa Rm/MPa KVmini (-46 °C)/J Taust/°C Def Tdef/°C B (no microalloys) 365 606 6.9 1000 1 980-840 V. Nb V1 415 543 6.2 1000 1 980-840 V2 480 624 9.3 1000 2 940-800 V3 600 732 2.2 1150 2 940-800 V4 481 593 8.0 1000 2 940-800 V. Nb. Zr Zr1 474 710 0.6 1150 2 940-800 Zr2 482 625 3.3 1000 2 940-800 Ti. V. Nb Ti1 422 547 10.0 1000 1 940-800 Ti2 622 699 1.0 1100 2 940-800 P P 412 486 9.5 1000 2 940-800 Ni Ni 459 533 2.7 1000 2 940-800 Mo Mo 349 443 8.4 1000 2 940-800 Figure 6: Mini-tensile test samples Slika 6: Natezni minipreizku{anci The highest values of the mechanical properties (YS and TS) were reached for samples V3, Zr1 and Ti2 (Table 2). They were austenitized before the thermo-mechanical processing on the simulator at 1100 °C and 1150 °C, respectively. The microstructures of all the heats consist of fine-grained ferrite, tempered bainite/ martensite and pearlite. The reason for higher yield and tensile strengths after a decrease in the deformation temperature is a decrease in the grain size due to a higher deformation ratio (the change in the grain size from 10.5 to 11.5) (Figure 7). A higher austenitization temperature (1100-1150 °C) allowed a complete dissolution of carbonitrides before the thermomechanical processing and thus led to an increase in the tensile strength up to 730 MPa. But the notch toughness of these specimens was low. The lowest value of notch toughness in the case of heat Zr1 was caused by coarse undissolved ZrCN particles, which were also visible on the fracture surfaces and in the microstructures of the mini Charpy samples (Figure 8). Figure 8: ZrCN particles on the fracture surface of heat 15 (SEM) Slika 8: Delci ZrCN na povr{ini preloma taline 15 (SEM) Vanadium-based carbides/carbonitrides were observed in the microstructure of all the samples marked as Vx, Zrx and Tix. The strengthening mechanism did not occur on specimens P, Ni and Mo, which were not micro-alloyed at all. The lowest values of mechanical properties were reached for the heat marked as Mo due to the reduction of manganese and carbon amounts. The main mechanism for increasing the yield and tensile strengths of the micro-alloyed specimens consisted of grain refinement (due to a decrease in the forming temperature) and precipitation strengthening. The grain size Figure 7: Decreased grain size due to a higher deformation: a) specimen Ti1, b) specimen V2 Slika 7: Zmanj{anje velikosti zrn z večanjem deformacije: a) vzorec Ti1, b) vzorec V2 Figure 9: Three-dimensional model of an ingot and a numerical simulation of forging in DEFORM 3D Slika 9: Tridimenzijski model ingota in numerična simulacija kovanja z DEFORM 3D Figure 10: Microstructure of the specimens after conventional open-die forging: a) no micro-alloys, b) micro-alloyed with Ti, V and Nb Slika 10: Mikrostruktura vzorcev po navadnem prostem kovanju: a) brez mikrolegiranja, b) mikrolegirano s Ti, V in Nb Table 3: Mechanical properties of forged ingots (without micro-alloys and micro-alloyed with Ti, V and Nb) Tabela 3: Mehanske lastnosti kovanih ingotov (brez mikrolegiranja in mikrolegirano s Ti, V in Nb) Specimen Rp0.2/ MPa Rm/ MPa A5/ % Ky(_46°C)/ J Grain size/G Base heat 326 480 34 179 9.5 Heat with Ti, Nb and V 433 534 32 155 11.0 of the specimen before thermomechanical processing was 6.5 and it decreased to the average value of 11.0 (ASTM E 112) after thermomechanical processing. 3.2 Fogging experiment The forging on the hydraulic press was performed according to the numerical-simulation calculation of deformation in the location of the real forged bar. The forging model and the specimen after forging are shown in Figure 9. The forging of experimental ingots was done by means of a hydraulic press, Zeulenroda (PYE 40). The ingots were put in a Heraus atmospheric furnace and heated up to 1150 °C. Then they were being forged to the final dimensions for about 1 min and 10 s. The final temperature on the ingot surfaces was measured with a thermocouple, and it reached about 750 °C. The ingots were then cooled on air with no subsequent annealing. The microstructure of the ingots after forging shows substantial differences, especially in the grain size (Figure 10). The yield and tensile strengths of an ingot with micro-alloys are considerably higher and the grain size is also different (Table 3). The yield strength increased by more than 100 MPa thanks to micro-alloying strengthening. 4 CONCLUSION A new technological process of forging steel for the oil industry was designed by means of a numerical simulation in the DEFORM 3D software. This process was applied to the samples during the experiment with a physical simulation. The samples were made from various heats micro-alloyed with a combination of Ti, Nb, V and Zr. The main mechanism for increasing the values of YsS and TS consists of grain refinement and precipitation strengthening. A grain refinement was achieved thanks to a decrease in the final forging temperature below the temperature of austenite recrystallization. Also, good notch toughness at lowered temperatures was maintained. The best values of the yield strength and tensile strength were reached by micro-alloying with vanadium and niobium and, especially, with the samples preheated before the thermomechanical processing at higher auste-nitization temperatures. This process led to a complete dissolution of all the micro-alloying additions during austenitization; therefore, good yield and tensile strengths were reached after thermomechanical processing. The forging experiment with real forging on the hydraulic press confirms the efficiency of the designed technological process. In the case of micro-alloying, the yield strength was by about 25 % higher than for the heat with no micro-alloys. The grain refinement of the micro-structure is also clearly visible. Acknowledgments The research presented in this paper was supported by project West-Bohemian Centre of Materials and Metallurgy CZ.1.05/2.1.00/03.0077, and co-funded by the European Regional Development Fund. 5 REFERENCES 1 ASM, Alloying - Understanding the basics, 1st edition, Materials Park, Ohio, USA 2001, 647 2 J. Zrnik, Effect of thermomechanical processing on the microstructure and mechanical properties of Nb-Ti microalloyed steel, Materials Science & Engineering A - Structural materials: properties, microstructure and processing, 319 (2001) 21, 321-325 3 S. K. Mishra (Pathak), Investigation on precipitation characteristics in high strength low alloy (HSLA) steel, Scripta Materialia, 39 (1998) 2, 253-259 4 A. Pandit, Strain induced precipitation of complex carbonitrides in Nb V and Ti V microalloyed steels, Scripta Materialia, 53 (2005) 11, 1309-1314 5 K. Hulka, Characteristic Feature of Titanium, Vanadium and Niobium as Microalloy Additions to Steel [online]. [cit. 2010-03-12]. Available online: