Behaviour of TiC Particles on the Co50-Based Coatings by Laser Cladding: Morphological Characteristics and Growth Mechanism

H13 steel surfaces are covered by coatings of Co-based alloy with 0, 10, 20, and 30 wt. % TiC using the laser cladding (LC) method. emorphological characteristics, growthmechanism, and themechanical properties of TiC on themicrostructure of the coatings were studied. e results show that TiC in the TiC/Co50 composite coating is composed of two parts: incompletely melted TiC and in situ TiC. TiC content has a great effect on the morphology of TiC, and it exists in different shapes: original TiC, fine-particle TiC, segregated TiC, petal-shaped TiC, and branch-shaped TiC. Additionally, the morphology of TiC in different areas of the coating is different, while TiC size gradually increases from bonding zone to surface. In the 10% TiC+Co50 coating, TiC mainly appears as undermelted, fine particles, precipitates, and having shapes of polygons and petals. From the bottom of this coating, the number of petal-shaped TiC has increased, and the particle size is also enlarged. In the 20% TiC+Co50 coating, the TiC in the coating mainly presents as undermelted, fine particles, and dendritic morphology. From the bottom of this coating to the surface, the particle size of the undermelted TiC shows a clear gradient change. Finally, the 30% TiC+Co50 coating does not have in situ TiC, and there is no obvious gradient change in the particle size of undermelted TiC. After coating by the LD method, the surface hardness is strongly enhanced. e average hardness of Co50 alloy, Co+10% TiC, and Co+20% TiC composite coatings is 499 HV0.2, 552 HV0.2, 590 HV0.2, and 824 HV0.2, respectively. ese values are 2.4–4.0 times harder than that of the H13 substrate. e wear resistance of Co50 alloy, Co+10% TiC, and Co+20% TiC composite coatings is greatly higher than that of H13 steel, showing excellent wear characteristics. e friction coefficient of the coatings which have TiC is very stable. erefore, the coatings can satisfy the requirement of tool steels applications. Additionally, the wear mechanism of the coating at room temperature is mainly brittle spalling, adhesive, and ploughing. At 700°C, the wear mechanism is mainly oxidation and fatigue.


Introduction
e surface of alloy tool steels and hot-working steels require high-temperature resistance, high strength, and high toughness. Particularly, these kinds of steel need high ability of abrasive resistance and thermal fatigue at high temperatures. After some heat treatment processes such as quenching and tempering, the hardness and the strength of the steel are enhanced greatly. However, the critical working conditions at high temperate could cause damage, fatigue failure, and creep on the steel surface. erefore, the working ability of the tools is reduced and the product quality also suffers a decrease [1,2].
In recent years, laser cladding (LC) is one of the advance surface modification methods that could improve the surface quality of the materials by creating a functional coating on the substrate surface. is method is rapidly developed and applied to repairing and recovering tool steel surfaces, especially at large surface tools like pressing mold, drawing mold, and rolling axis [3][4][5][6][7][8][9][10]. In LC technology, ceramic particle-reinforced metal-based composite coatings have become a hotspot in recent years due to their excellent wear resistance, corrosion resistance, and high-temperature oxidation resistance [11][12][13][14]. Among some feeding materials for the LC technique, Co-based alloy coating material can strongly increase the antioxidation and abrasive abilities for the coated surface. But when suffering high friction force, the hardness and the abrasive characteristic of this type of coating still need further improvement. erefore, various carbides, nitrides, and silicides particles are often used as composite reinforcement components.
Recent reports focus on adding some type of carbide particles such as WC, B 4 C, SiC, and Cr 2 C 3 to the Co-based alloy coating to increase the abrasive and mechanical properties at the high-temperature environment of the working surface [15][16][17][18]. Among these reinforcement phases, TiC with high hardness, high melting point, stability at the high-temperature environment, and easiness to disperse is an excellent wear-resistant ceramic strengthening phase. In the field of wear resistance and high-temperature resistance, it has received considerable attention from the material science community. However, when combined with Co-based alloy, thermal stress, voids, and microcracks can appear due to the relatively large thermal expansion coefficient difference between TiC and Co metal. e mechanical properties of ceramic reinforced composites depend on the morphology, particle size, content, crystal integrity, and distribution of particles in the composite phases [19][20][21]. To achieve a perfect coating of Co-based alloy mixed with the TiC particle, the size of the particle is one of the most important factors. e smaller the particle size, the fewer the defects, while the smaller the average free path of the bonding phase, the higher the bending strength and hardness can be maintained. Moreover, the clearer its strengthening effect, the less unfavourable the toughness and plasticity. e larger the particle size, the worse the strengthening effect, therefore, this effect can disappear, the greater the degree of disadvantage to toughness and plasticity [22][23][24].
However, there are few reports on the formation mechanism under the conditions of overequilibrium rapid solidification [25][26][27]. For that reason, it is particularly important to study the morphology of TiC in coatings. is paper used Co50 alloy and TiC mixed powder as raw materials and applied LC technology. By rationally adjusting the ratio of the two powders in the cladding layer and optimizing the cladding process parameters, a TiC reinforced Co-based composite coating is prepared on the surface of the H13 steel layer. e morphological characteristics and growth mechanism of TiC in the coating are analysed. e paper provides a theoretical and technological basis for the promotion and application of laser cladding technology in strengthening wear-resistant surfaces. Friction abrasion is a complex process, influenced by many factors such as hardness, surface morphology, temperature, and pressure [28][29][30][31][32][33]. Recently, the friction and wear properties of cladding layers have been widely studied at room temperature. However, there are not many researches focusing on friction and wear properties and its microstructure at high temperatures. Particularly, the effect of adding TiC in laser cladding coating has not been reported yet. is paper considers the wear resistance and hardness of Co-based alloy coatings and TiC/Co-based composite coatings. rough analyzing the wear characteristics, the mechanisms of friction and wear resistance were indicated to provide useful knowledge for practical applications.

Materials and Methods
ASTM H13 hot-working steel is chosen to be the substrate; the sample size is 100 mm length × 30 mm width × 10 mm thickness. e chemical composition of H13 steel sample is presented in Table 1, indicating a high-quality steel. e steel samples are initially ground by sandpapers and then cleaned by alcohol and acetone, following a drying step by an oven. Self-melting Co50 powder with the particle size of about 53 μm is prepared; its chemical composition is shown in Table 2. e particle size of TiC is about 10 μm; the purity of TiC is 99.5%. e mixtures of Co powder with 0%, 10%, 20%, and 30% TiC are created and scattered along the substrate surface with 1 mm thickness, as shown in Figure 1. After that, these samples are dried in an oven for 8 hours. Finally, the dried samples are melted by using the LC method. e LC process is made by laser cladding machine GS-TFL 6000 CO 2 at Kunming University of Technology. Some basic technical parameters are laser beam power 3.3-3.6 kW, scanning speed 350-500 mm/min, the distance of the laser head to the substrate surface 50 mm, and inert gas argon flow rate 8 l/h, as shown in Table 3.
e coated samples are cut by a laser-cutting machine in a direction that is perpendicular to the scanning direction.
en, the S0 sample is etched by aqua regia solution (1HCl + 3HNO 3 ) in 15 seconds, while S1, S2, and S3 are etched by saturated FeCl 3 in HCl solution for 2 minutes. After cleaning and drying, the etched samples are observed by a scanning electron microscope (SEM). e SEM type XL30ESEM-TMP (the Netherlands) has in situ accessories such as phoenix, OIM, and Energy Dispersive X-Ray Spectroscopy (EDS) for analyzing the microstructure and chemical composition of the coating. An X-ray diffraction (XRD) machine type D/MAX-3B (Japan) is used to study the crystal structure and phases of the samples. e microhardness testing is employed on the HMV-WIN machine, with the loading weight being 1.961 N (HV 0.2 ), and the loading time is 15 seconds. e interface between the coating and the substrate is chosen to be the zero origin coordinate, in which the upper coating layer has a positive value, while the lower substrate layer has a negative value.
is research uses wear-by-friction testing machine at high-temperature type MMU-5G to study the wear resistance of coatings at room temperature and at 700°C with pinon-disc wear of friction pairs. Some main technical indicators are as follows: the working range of the axial test force is 10-5000 N; the relative error of the test force indication value is 1%; the maximum friction torque is 5 N·m; the relative error of the friction torque indication is ±2%; singlestage transmission system 0.1-2000 r·min −1 ; spindle speed error is ±1%; and the temperature of the cylindrical heating furnace is 1100°C, using 2 K-type thermocouples. Figure 2 represents the XRD spectrum of S0, S1, S2, and S3 samples. e results show that S0 coating consists mainly of 2

Analyzing the Coating Phases by XRD Spectrum.
Advances in Materials Science and Engineering the c-Co phase, which has the highest peak, and Cr 1 . 12 Ni 2 .88 phase. e lattice structure of c-Co is face center cubic (FCC). Normally, at a temperature higher than 417°C, pure Co has an FCC structure; however, at a lower temperature, Co lattice transforms into hexagonal close-packed (HCP) ε-Co style. Otherwise, the XRD diagram illustrates an FCC structure of c-Co rather than an HCP structure of ε-Co as the existence of the Ni, W, and Fe elements on the Co50 powder. ese elements tend to stabilize the FCC structure. Besides, the LC method generates a superrapid cooling rate of the molten powder when creating a coating; thereby, the c-Co structure does not have time to transfer into ε-Co.
ese are the reasons why the coating structure consists mainly of c-Co. Besides Co element, the solid solution of c-Co dissolves some other elements [1,20]. Cr 1.12 Ni 2.88 phase is generated by the crystallization rate and cooling rate that are extremely fast in the LC method. is phase can also dissolve a small amount of other elements. Figure 2 also indicates that the coating of S1 sample is formed of TiC, TiCo 3 , Cr 2 Ni 3 , and Cr-Ni-Fe-C phases. TiCo 3 phase is created by a reaction between Co elements in Co powder and Ti elements split up from TiC by LC heat, while Cr 2 Ni 3 phase is formed by a reaction between Cr and Ni under the high power of a laser beam. On the other hand, Cr-Ni-Fe-C phase in S1 sample is generated by the elements in Co50 powder, Ti elements split up from TiC, and some elements diffused from the steel substrate. e coating of S2 sample is made of TiC, Cr 2 Ni 3 , and c-Co, while S3 sample coating consists mainly of TiC and c-Co.
In summary, the solid solution c-Co exists in the coating of S0, S2, and S3 samples but does not exist in the coating of S1 sample. In the coatings of S1, S2, and S3 samples that are having TiC on the mixture powder, increasing the TiC percentage results in decreasing the percentage of Cr 2 Ni 3 . Cr 2 Ni 3 phase exists in the coatings of S1 and S2 samples, but cannot be found on the S3 sample. Figure 3 demonstrates the microstructure of S0, S1, S2, and S3 coatings. It can also be seen that from the top of S0, S1, and S2 samples, the microstructure includes bonding zone (BZ), cladding zone (CZ), heat-affected zone (HAZ), and steel substrate. e microstructure of the S0 sample has a good microdensity and a good metallurgical bond that is formed between the coating and the substrate, with the thickness of the coating being low. e microstructure of the S2 sample indicates a better structure, and the coating thickness is larger than that of the S1 sample. e coating thickness of the S3 sample is the largest, but the coating and substrate are not well combined.
ere are no bonding regions caused by the high TiC content in the coating, so the quality of this S3 coating is not good enough.
In the superrapid melting process, the energy intrusion amount of the laser beam into the steel substrate is dramatically small. at is the reason why the sensitivity HAZs are ultrathin, with 788 μm for S0, 722 μm for S1, and 590 μm for S2. e thinner the HAZ, the better the quality of the sample. In addition, the martensite grain size of HAZ is bigger than the martensite grain in substrate. Because the substrate is affected by the huge heat energy of the laser beam, some grains grow larger as they merge with the neighbor grain. But in the LC process, this heat-affected zone happens in an extremely short time. e growing grain does not have enough time to grow too large; therefore, the mechanical properties of the HAZ remain in good condition.
is is the impressive advantage of LC method. e LC technical parameters are important factors that strongly affect the quality of the coating. When the technical parameters are well controlled, the microstructure of the LC coatings can prevent heat stress, residual stress, and microcracks. Figure 4 illustrates the microstructure of the cross section of S1, S2, and S3 coating samples. It can be seen from Figures 4(a)-4(c) that the coating and the substrate interface show a clear "white bright band," showing that the coating and the H13 steel substrate can achieve a good metallurgical bond. In laser cladding, the "white bright band" is extremely thin (2∼5 μm). e molten powder is cooled down at the highest rate at this interface, generating a fine grain structure with uniaxial orientation. ese grains can quickly grow to form a dendritic crystal. e dendrite with the main branch grows parallel and in reverse direction to the heat flux (perpendicular to the substrate) at a high speed. Other dendrites with the main branch which are not perpendicular to the substrate cannot grow because they are surrounded by other crystals. Consequently, the crystal with the highest growing speed will form the morphology of the solid-liquid interface and leads to the formation of the columnar grains. eir columnar grains have a flat boundary and grow in the reverse direction to the heat flux. ey are the white bonding lines. It means that S1 and S2 coatings construct a strong bonding with the H13 steel substrate. Above these white lines, the TiC particles with black color appear. e density and size of the black TiC particles increase as the increase in the ratio of the TiC in the mixture powder. In S3 coating, there are too many TiC particles that result in a limitation in a good bonding zone.
In S0 coating, the "bright band" is a quite flat-growth tissue. Because the laser energy is transmitted downward from the top of the cladding layer, and the tissue solidifies from bottom to top, the heat action time at the bottom of the cladding layer is short, and the tissue growth rate is slow. erefore, flat interface grows. is "bright band" is substantially perpendicular to the plane and cell crystals growing at the interface. To the middle of the molten pool, multidirectionally grown dendrites and dendrites are transformed.
e near-surface is a fine dendrite region  Advances in Materials Science and Engineering that grows parallel to the direction of the laser scanning speed. is is because the temperature of the substrate is low and heat is dissipated fastest in a direction perpendicular to the cladding layer. In addition, the dendrite structure of the coating gradually disappeared from the bottom to the surface, and it turned into a large number of dense fine structures near the coating surface. e edge of the bonding zone of the S0 coating has obvious growth characteristics of columnar dendrites and equiaxed crystals and solidifies and develops towards the coating surface perpendicular to the bonding zone. Zhang's research shows that there is an equiaxed crystal chill layer near the base in the cladding layer of Co-based alloy, therefore producing a large degree of subcooling [14]. Compared with the S0 coating, a "white bright band" of the S1 and S2 coatings is wider, which will help increase the bonding strength between the coating and the substrate. It can be seen that the structure of the S1 coating is composed of bright white dendrites, eutectics between the dendrites, and black TiC particles, and the TiC particles are diffusely distributed, which can play a good hardening role. e morphology of TiC in the S1 coating structure is different due to its different parts in the molten pool; its composition, temperature distribution, and cooling rate are different. TiC in the middle and the surface of the coating is a large block structure, while the bottom of the coating has a low temperature and insufficient melting, and the more rapid the heat transfer effect of the cold matrix, the larger the cooling rate, and the TiC grains are too late to grow. It has stopped growing when it is large, so a fine granular structure is formed. In addition, compared with the microstructure of the S0 coating, the structure of the S1 coating is no longer composed of neat columnar dendrites, and there is no obvious direction of dendrite growth. Many interdendritic eutectic structures exist. In S2 coating with 20% TiC, the "white bright band" contains a large amount of black TiC particles. With the increase of the amount of TiC in the preset layer, the content of the TiC reinforcing phase and the phase structure of the coating evolve accordingly, while the size of the TiC particles in the structure increases and the number decreases slightly. e resulting TiC is evenly distributed in the coating. It can also be seen from the figure that the structure of the coating is composed of bright white dendrites, eutectics between the dendrites, and black TiC particles, and the TiC particles are dispersedly distributed, which can play a greatly hardening role.

Advances in Materials Science and Engineering
When the TiC content in the preset layer was increased to 30%, the S3 coating did not achieve a good combination with the substrate, as shown in Figures 3(d) and 4(d). e reason is that the thermal expansion coefficients of TiC powders and Co-based alloy powders are quite dissimilar. Consequently, when the temperature gradient increases, the thermal stress and the formation of cracks generated by expansion increase. In addition, the required laser power density is related to the melting point; when the absorption rate is high, the required laser power density is greater. Studies by Si et al. [17,18] found that if the content of added carbide reinforcing phase is too high, the brittleness of the coating will experience a significant increase. is is because the formation of a large amount of carbides, leading to the coating being prone to cracks and spalling during working operation. Figure 5 shows the microstructure with different types of shapes of TiC on S1 coating. It can be seen that the coating structure is mainly composed of dendrites, eutectic structures between dendrites, and TiC particles. Besides the original TiC particles (black) that are not fully melted, there are also primary TiC particles (white) that are precipitated in situ from the liquid phase during solidification. Observing the morphology of TiC, it can be found that from the bottom to the surface layer, the morphology of incompletely melted TiC is mainly spherical, while TiC precipitated in situ exists in different forms. Figure 5(a) demonstrates that in the bonding zone, TiC particles have a white color with extremely fine size. Prior reports indicated that these fine TiC particles have a hexagonal shape and only appear near the white bonding lines, while most of the dense TiC particles near the bonding interface are randomly distributed, and the small TiC particles only appear at the bottom of the coating; away from the bonding interface, a large amount of fine TiC precipitates [2,3]. e growing mechanism of these particles is independent growth as the nuclei of TiC formed by the "floating" principle. e floating principles are caused by concentration, structure, and energy. ese principles are helpful for the microstructure arrangement; for instance, TiC in liquid phase existing on the atomic cluster will gradually pile up to grow bigger to become a super fine TiC. According to the analysis, the reason that TiC is not fully melted is mainly due to the fact that when laser-cladding TiC/Co-based composite coatings, the composite material melts by absorbing the energy of the laser beam. e absorptivity of a material to a laser depends on the resistivity of the material, the scanning speed, and the wavelength of the laser [12].
Figures 5(b) and 5(c) show that a large amount of TiC particles gather together to form a blocky rosette, with two or three particles in a rosette [4]. From the bottom to the top of the coating, the number of TiC petals increases, and the particle size becomes larger. e orientation of different TiC particles in the petal-like morphology is disordered, showing random bonding and no obvious orientation characteristics. e different morphologies of TiC in different regions are caused by different cooling rates. On the other hand, the growth morphology of TiC is related to the solidification speed of the coating and the carbon concentration in the laser molten pool. e nucleus of these TiC particles are constructed by the incomplete molten TiC particle in the powder. It can be seen that TiC's growth mechanism in the middle zone of the coating is mainly in the form of a "bridge" [2]. Some TiC particles that are close to each other play roles as the central particles, and then they support each other and develop. On the top of the coating, TiC particles gather together to form clusters. In general, the number and the size of TiC clusters increase as they increase the distance from the bonding zone to the upper surface. is effect shows that, before the "capturing" phenomenon, the TiC clusters in the molten area were always moving. After that, they link together to generate bigger TiC clusters [3]. It can be explained that in the melting zone, parts of TiC particles resolve, assemble, and link with each other; each petal represents a TiC. Figure 5  Advances in Materials Science and Engineering also indicates that a section of TiC can be observed as needleshaped, a similar result as Pei's report [5]. is is because when the temperature decreases, Ti and C atoms in the saturated c-Co phase will separate and accumulate. e accumulation will form extremely fine TiC particles, and this phenomenon is called phase segregation. e phase segregation happens as a result of defects on c-Co, therefore, forming vacancies. Karantzalis et al. [7] proved that the segregated TiC particles appear in many shapes: Chinese script shape, elongated precipitates shape, and fine-sized cuboid precipitates shape. Meanwhile, Pei [6] shows that the scanning speed of the laser beam seriously affects the shape of segregated TiC particles. e segregated TiC particles and recombinant TiC particles appear almost throughout the coating. e recombinant TiC particles grow in the direction that is parallel to the laser beam or they stack together. In summary, the diversity of the TiC particle shapes is caused by the effect of the close relationships between the TiC shape, the cooling rate, and the concentration of C in the melting region.
Because TiC powder absorbs laser energy much more than Co50 alloy, the resistivity of TiC is significantly higher than that of Co50 alloy. Hence, during the laser irradiation process, TiC preferentially absorbs heat and is rapidly heated to a very high temperature and then conducts heat to surrounding materials (heating matrix Co50 alloy). is heating mechanism makes the temperature of TiC and its nearby matrix Co much higher than the average temperature of the molten pool, which easily causes interfacial reactions.
is indicates that the TiC particles were not completely melted during the laser cladding process, but mainly the surface melt-solidification process (black TiC particles that were not fully melted). It means that the nucleation of TiC mainly uses a large number of incompletely dissolved original TiC particles in the molten pool as the crystalline core, or it can grow independently. e existence of undermelted TiC and the precipitation of a large number of primary carbides make the structure of the cladding coating very fine. e reason for TiC in situ precipitation is mainly because of the partial dissolution of TiC powder under the action of the laser. During laser irradiation operation, particles with residual deformation and distortion defects or TiC at the coating surface with higher cladding temperature may be completely dissolved, and large TiC particles also partially dissolve at their edges or raised parts [5]. At the same time, the melting point of the Co50 alloy is much lower than that of TiC, so during the heat transfer process, Co50 in the mixed powder dissolves first, and TiC subsequently dissolves, causing the Co50 alloy melt to contain a large amount of supersaturated Ti and C atoms, forming a C-rich region around it. e solid C particles quickly diffuse into the laser melt pool and are surrounded by Ti liquid. As the laser beam moves, the temperature of the molten pool drops rapidly, and these supersaturated Ti and C will reprecipitate from the melt. Because Ti atoms have a good affinity for C atoms, they preferentially combine to form TiC. Under the laser beam effect, some TiC particles are resolved into Ti and C. Solid C particles rapidly diffuse into the melting region and surrounded by liquid Ti. e process of forming TiC consists of three stages. First, the contact surface between the liquid-solid phase of Ti and C directly reacts to form TiC x [2,5,8]. Second, the liquid Ti continues to diffuse through TiC x layer to react with the remaining C in the core. e diffusion will continue until reaching the corresponding TiC concentration, forming molten TiC in the liquid phase. e solidification process happens at an extremely rapid rate, and the TiC separated from the liquid will segregate and grow. In addition, under the tremendously fast heating rate of the LC method, the separation rate in the melting zone of TiC is greater than Co due to a higher energy absorption of the TiC. A small number of TiC particles have high internal energy due to the appearance of residual stress or defects created in TiC powder making. For this reason, during the melting process, these particles are completely melted. e bigger TiC particles are also melted in the protruding part or at the edge. During the cooling process, some Ti and C atoms from the liquid phase recombine to form a new TiC. At the end of the coating, besides the partly molten TiC, the microstructure also consists of new forming TiC and TiC segregated from c-Co.
According to the second law of thermodynamics, the reaction process always proceeds in the direction of the reduction of the free energy of the system. In other words, during the rapid solidification process, the synthesis of TiC is roughly divided into three stages. Initially, Ti and C at the solid-liquid bonding interface react directly to form TiC x , as presented in Figure 6(b). en, the liquid Ti diffuses and passes through the TiC x layer reacts with the remaining C until the concentration of C in TiC x reaches the concentration of C in TiC, and the resulting TiC is dissolved in the liquid phase, as illustrated in Figure 6(c). Finally, TiC precipitates from the solution and grows [9,10]. is shows that TiC in situ can grow outside the original TiC particles along the edges or grow sideways with facet steps.
Comparing of in situ precipitation TiC and incompletely melted TiC, incompletely melted TiC particles have some kind of defects such as burnout, interface pollution, and melting phase decomposition of enhanced phase during laser cladding, while TiC in situ precipitated particles are produced by in situ reaction. In this way, the thermal stability and interface problems of the enhanced phase are solved, and the coating performance is further improved. In addition, the incompletely melted TiC and TiC in situ properties are greatly different, while the incompletely melted TiC's particle size and TiC in situ morphology have a great impact on the performance of TiC/Co-based coatings.
To provide more details about the composition of TiC particles, energy-dispersive X-ray spectroscopy (EDS) is used to analyze the particles in S1 sample, as shown in Figure 7. e results reveal that the black particles (point 1) and white particles (points 2 and 3) are composed mainly of Ti and C. In point 1, the atomic components of Ti and C are 36.32% and 49.39%, respectively, and the atomic ratio Ti:C is 0.74. In point 3, the atomic components of Ti and C are 25.31% and 27.38%, respectively, and the atomic ratio is 0.92. From these numbers, it can be withdrawn that the atomic ratio between Ti and C is almost 1 : 1. is proves that the black and white particles in the microstructure of S1 are TiC. e black particles are nonmolten TiC or partially melting TiC, while the tiny white particles are the newly formed TiC.
ese new particles have a much smaller size compared to the black TiC particles. In point 2, the atomic percentages of Ti and C are 28.77% and 16.37%, respectively, and the atomic ratio Ti:C is 1.76. At this point, the TiC x appears with a large amount of C. e atomic percentage of point 4 is 35.15% and 39.06%, and the atomic percentage of point 5 is 28.49% and 34.04%, respectively. e atomic ratios of Ti and C in the particles are close to 1 : 1. Combined with the Ti-C phase diagram as demonstrated in Figure 7(f ), it can be concluded that both black and white blocks are TiC. Among them, the black blocks are uncompleted melting TiC, and the white blocks are in situ TiC. e size of the particles is much smaller than that of the undermelted TiC particles. Notably, the atomic percentages at point 2 are 28.77% and 16.37%, respectively, and the C/Ti atomic ratio is 1.76, which indicates that TiC x still presents at point 2, and a large amount of C still remains. e precipitation of TiC mostly uses the defects in the Cr-Ni-Fe-C solid solution as a nucleation substrate. When the cooling process happens below the solidification temperature, the supersaturated Ti and C atoms in the Cr-Ni-Fe-C solid solution precipitate. A fine-dispersed TiC precipitate is created and spread throughout the coating [13]. Pei's research [6] shows that the growth mechanism of tiny TiC particles is independent nucleation; that is, the independent nucleation of TiC in the liquid phase is based on the microlocation of favorable concentration fluctuations, structural fluctuations, and energy fluctuations, and then they stepwise stacking grow up and finally exist in the form of polyhedra in the form of close-packed atoms. TiC precipitates out because the supersaturated Ti in the c-Co phase gradually precipitates when the solidification temperature continues to cool, forming small dispersed TiC particles.
is precipitation mainly uses defects in the c-Co solid solution as the nucleation site, and the dislocation lines firmly pin the precipitate. Zhang et al. [8] have confirmed that the TiC precipitates appear in the shape of Chinese characters, slender, and slender cubes. Pei et al. [5] also found that when the growth rate of the solid solution interface is greater than the critical speed of particle  e lotus petal-shaped nucleus mainly grows and connects with several incompletely melted original TiC particles close to each other as crystalline cores. erefore, this morphological feature is a result of the in situ precipitation and aggregation of TiC particles, and each petal represents a TiC particle. Figure 8 shows the microstructure with different types of shapes of TiC on S2 coating. From Figure 8(a), it can be seen that, like the S1 coating, small TiC particles precipitated in situ near the bonding interface of the S2 coating, and the small TiC particles only appear at the bottom of the coating. A magnified observation at ×16000 showed that the surface of the small TiC particles was smooth, approximately spherical, and no obvious edges and corners. Figure 8(b) indicates a large amount of TiC in the form of cross petals [5] and twigs [7,10]. Around the bonding zone, the temperature is lower than the cladding zone, causing an incomplete melting. Moreover, the low temperature of the substrate leads to a rapid cooling rate. e growing time of the TiC is short, so it tends to keep the original shape or exist in any shape rather than growing bigger. Around the bonding zone, the shape petals are very symmetrical; this phenomenon is closely related to the crystal structure of TiC. TiC lattice has an FCC structure, with both Ti and C atoms having symmetrical structural centers. ereafter, when forming TiC, the structure of TiC will tend to be symmetrical.
In Figures 8(c) and 8(d), TiC mostly exists in a spherical shape. In Figures 8(b)-8(d), TiC behaves in two ways in the alloy melt: one is that TiC has been completely dissolved and presents a large, densely distributed and developed dendritic morphology. Moreover, the developed dendrites are mostly cross-shaped and the orientation tends to be consistent; the second is that the TiC particles in the added powder are not completely dissolved and mainly exist as spherical structures, as displayed in Figures 8(c) and 8(d). Particularly, in the coatings, both dendrite and eutectic have a relatively uniform size, but the size of TiC varies greatly: from the bonding zone to the surface of the coating, the size of TiC gradually increases.
is phenomenon is very clear and continuous. Chen and Wang [9] show that the shape of TiC is determined by the difference in position, composition, temperature distribution, and cooling rate in the coating. e reason for the formation of the developed dendritic crystals of TiC is that part of the TiC in the coating is dissolved, and the Ti and C produced after the dissolution are solid-dissolved in the alloy melt. When cooling, a large number of polygonal lumps and primary TiC with other elements are solid-dissolved. A diffusion zone with high Ti and C content is formed around the unmelted TiC particles. During the solidification process, radial primary massive TiCs with unmelted TiC as the center appear, and then further cooling, so between the unmelted TiC and the primary TiC, they are formed. e fine c-Co dendrites and their eutectic structure were introduced. Due to the lower temperature and insufficient melting at the bottom of the coating, combining with the rapid heat transfer of the surrounding cold substrate, the cooling rate is extremely high, so the growth time of the precipitated TiC is dramatically shortened. It is too late to grow and maintain the initial state of the precipitation. During the nonequilibrium solidification process of laser cladding, primary TiC will appear when the C content in the liquid reaches a certain value. Since the space occupied by the ball is the smallest in the same volume, the primary TiC should exist in a spherical form, but it looks like the spherical TiC is actually a polyhedron, and the corners of the polyhedron have a small radius of curvature, a large concentration gradient of the solute, and a fast diffusion rate. erefore, the crystals at the corners grow faster than the planes, making the polyhedron gradually grow into a dendritic shape [27]. Figure 9 shows the morphology of TiC in different areas of the S3 sample coating. e figure points out that TiC exists like a large number of diffusely distributed spherical structures. Unlike S2 coating, TiC particle size in S3 coating has no clear gradient change. is is because the TiC content is higher in the S3 coating, and the thermal expansion Advances in Materials Science and Engineering 11 coefficients between TiC powder and Co-based alloy powder are very different. is will cause a large temperature gradient in the molten pool area, and the increase of the temperature gradient is inevitable. is can cause thermal stress, resulting in the formation and propagation of cracks. In addition, TiC powder has a much higher absorption rate of laser energy than Co-based powder. erefore, when a laser beam is applied to the powder of the preset layer, TiC has no time to precipitate and maintains the original morphology. is means that when the content of TiC is large, the TiC particles in the powder of the preset layer fail to decompose Ti and C atoms so that no in situ TiC occurs. Figure 10 exhibits the microhardness distribution of cross section of S0, S1, S2, and S3 coatings. e coating hardness values are divided into 3 zones: HAZ, BZ, and CZ. e hardness values mostly improve greatly from the SUB zone to the HAZ, thereafter, reaching the highest value at the CZ. e LC coating does not only create an extremely high hardness film but also enhances the hardness of the substrate by forming an HAZ with highly hardness value. is is because the quenching affection of the laser beam as the HAZ is heated and cooled down rapidly in the LC process [28]. Far away from the coating surface, this effect reduces its intensity as the thickness of the material increases [18]. e diffusion of the Co, Mo from the coating into the steel substrate, forming a strengthening solid solution, also contributes to the increase in the HAZ hardness [14]. e hardness numbers of the coatings are 499 HV 0.2 , 552 HV 0.2 , 590 HV 0.2 , and 824 HV 0.2 corresponding to S0, S1, S2, and S3 coatings, respectively. e hardness number of the CZ increases gradually from the S0 to the S1, S2, and S3 as the TiC rate increases correspondingly. e hardness of the S0 coating is dramatically improved as comparing to the steel substrate. e appearance of the dendrites structure of the new Cr 1.12 Ni 2.88 phase, as shown in Figure 4(a), which has high hardness value and well dispersion in the matrix is the reason of this improvement.

Microhardness of the Coatings.
is fine Cr 1.12 Ni 2.88 phase also prevents the crystal growth in the material, therefore, constructing the fine grain microstructure. e presence of TiC particles in the S1, S2, and S3 coating powder leads to the formation of TiCo 3 and Cr 2 Ni 3 phases which have a high melting point and high hardness value. Moreover, the unmolten TiC particles and newly in situ TiC forming from the [Ti] and [C] atoms also contribute to the high hardness value of the coating [11], as shown in Figures 5, 8, and 9. erefore, the higher the rate of TiC in the coatings, the higher the hardness number of the coatings due to the extreme high hardness of TiC. Comparing to the steel substrate or the SUB zone, the hardness values rise 2.4, 2.7, 2.8, and 4.0 times corresponding to S0, S1, S2, and S3 coatings, respectively. In conclusion, the hardness numbers of the surface are Distance from clad-substrate interface (μm) S0 S1 S2 S3 Figure 10: Microhardness distribution of cross section of S0, S1, S2, and S3 coatings. significantly strengthened after coating and a higher portion of TiC creates a higher coating.
In the CZ, the hardness numbers of the S1, S2, and S3 coatings experience a fluctuation. e diversity of TiC particle forms such as unmolten TiC particle, in situ TiC particle, and semimolten TiC particle creates an oscillation of the hardness value of them, as shown in Figures 4(a)-4(d). ereafter, the hardness of these coating suffers a fluctuation.
rough the hardness number, we can predict the wear resistance of the coating. e higher hardness almost results in the higher wear resistance as the hardness is the measurement of the ability to resist the local deformation. Xu et al. [34] reported that, with WC powder, the hardness of the CZ could reach 600-800 HV50 depending on the rate of WC. e WC+Co-based coating has a lower hardness comparing to the TiC+Co-based coating due to the fact that hardness of WC is lower than the hardness of TiC. Comparing to TiC powder, adding SiC particle in Co-based coating could result in a higher value of the coating hardness that is up to 1300-1500 HK due to the higher hardness of the SiC [35]. Yang et al. [36] indicated that using TiCN powder leads to a high-value hardness of 703-774 HV, corresponding to 10-20% powder. Comparing to S1 and S2 samples, these hardness numbers are higher due to the higher hardness of TiCN. Implying a rich Cr powder mixing with Co-based alloy could gain a coating with 550 HV, which is much lower than the other types of coatings due to the lower hardness of chromium carbide [37].

Friction and Wear.
Because S3 coating is not well combined with H13 substrate, the test of the friction and wear performance only selects S0, S1, and S2 samples. e Advances in Materials Science and Engineering maximum working temperature of hot work tool steel is 700°C, so the maximum testing temperature is chosen as 700°C. Figure 11 demonstrates the friction coefficient of the S0, S1, and S2 samples at room temperature and 700°C. At room temperature, the coefficient values of these coating samples slightly fluctuate around 0.5-0.6. At 700°C, the coefficient value of the S0 coating increase from 0 to 0.4 after 600 seconds due to the wear of the oxide layer, indicating the shift from the minor wear abrasion to a more severe wear state. e average coefficient value of the S1 coating at 700°C strongly oscillated around 0.62. e coefficient value of the S2 coating at 700°C is always stable around 0.6. ese results prove that the S0, S1, and S2 coatings have a great improvement on the wear resistance of H13 steel. e coating layer enhances the hardness of the surface, prevents it from being deformed or failure.
e results also show that the wear resistance of S2 coating is higher than S0. Because in the process of generating molten coatings, TiC particles are decomposed and recombined to form new TiC particles.
ese new TiC particles are strongly bonded to the matrix, having a very high hardness, and uniformly dispersed throughout the coating, thus, improving the wear resistance of the coating. Under the friction force, these enhanced TiC particles have a strong anti-deformation effect. e reasons are that they can resist the force and they play an important role in minimizing wear for the matrix. Moreover, during the decomposition process of TiC particles, they could combine with other molten elements to produce perinatal dendrite solid solution [29]. S2 coating is mainly composed of initially TiC, in situ TiC, Cr 2 Ni 3 , and c-Co solid solution. is solution is formed and spread evenly on the fine, small dendrite, and eutectic [30], therefore, increasing durability for cohesion between these microstructures and improving the durability and wear resistance of the coating. In addition, S2 sample does not appear plastic deformation; its wear mechanism is mainly adhesion type. In addition, the hardness of S2 is higher than S0, minimizing the surface deformation, thus, delaying the time of cracking formation as well as its development speed. ese effects result in reducing the risk of cracks failure. e friction coefficient of S2 was stable with a quite high value. Candel et al. [32] show that when the laser beam's power density increases, the wear resistance is almost unchanged. Due to the influence on the concentration of TiC, this contributes to the increase in the growth time of TiC in c-Co, thereby forming a quite smooth friction surface. S2 coating has better antiwear performance as their TiC content is higher. When the S2 coating and the friction part are facing each other, as S2 is mainly composed of carbides, the friction parts are easily embedded in the softer c-Co solid solution. In addition, during the ploughing process, friction parts encounter fewer obstacles; as a result, a deeper furrow is formed. Secondly, the hardness of S2 sample is higher than S1 one. In the wear process, increasing the coating hardness can reduce the deformation of the coating surface, decrease the propagation speed, postpone crack initiation time, and delay the chance of crack nucleation. However, the friction coefficient of the S2 coating is higher than S1. It may be due to the existence of hard phases in S2. Under high stress for a long time, the massive hard phase flakes and peels; thus, wear resistance is reduced [31]. Figure 12 exhibits the XRD diagrams of the coating after wear testing of S0, S1, and S2 coatings at room temperature and 700°C. e results show that, in the S1 sample, CoO
the S0 and S2 coatings, they do not exist. At 700°C, the S0 coating contents are CoCr 2 O 4 , while the S1 coating has CoO, CoTiO 3 , and a small amount of NiCr 2 O 4 . e S2 sample possesses a great amount of CoCr 2 O 4 and NiCr 2 O 4 phases. erefore, the existence of these oxides could influence the wear mechanism of the coating. At 700°C, the wear mechanism of the S0, S1, and S2 coatings are mostly oxidation wear and fatigue wear. e reasons are the oxidation of the samples surface and the forming of the oxide layers. ese oxide layers can protect the sample from wear. Nevertheless, they are brittle and can be cracked under the load, leading to fatigue spalling [33]. e oxidation and sloughing process take turns to each other during the wear process, therefore, improving the wear resistance at the hightemperature conditions.

Conclusions
(1) Co-based coating and TiC/Co-based composite coating were prepared on the surface of H13 mold steel by laser cladding. e coatings with a TiC percentage of less than 20% achieve a metal bonding type on the steel substrate. Applying the LC method could improve the hardness and wear resistance of the hot dies surface.
(2) Co50 alloy coatings are mainly composed of solid solutions c-Co and Cr 1.12 Ni 2.88 . In Co+10% TiC coating, there are TiC, TiCo 3 , Cr 2 Ni 3 , and Cr-Ni-Fe-C phases. Co+20% TiC composite coating consists of TiC, Cr 2 Ni 3 , and c-Co, while Co+30% TiC coating consists mainly of TiC and c-Co. (3) TiC in the TiC/Co50 composite coating is composed of two parts: incompletely melted TiC and in situ TiC. In situ TiC generated in the subsequent solidification process after the decomposition of TiC. TiC exists in different shapes: original TiC, fine particle TiC, segregated TiC, petal-shaped TiC, and branchshaped TiC. TiC size also gradually increases in the direction from the bonding zone to the surface layer. (4) e TiC content has a great effect on the morphology of TiC in the composite coating, and the morphology of TiC in different areas of the coating is different. In 10% TiC+Co50 coating, TiC mainly appears as undermelted, fine particles, precipitates, and appears as polygons and petals. From the bottom of the coating, the number of TiC petals is increasing, and the particle size is increasing. In 20% TiC+Co50 coating, TiC in the coating mainly appears as undermelted, fine particles, and dendritic morphology. Moreover, from the bottom of this coating to the surface, the particle size of the undermelted TiC shows a clear gradient change. 30% TiC+SCo50 coating does not have in situ TiC, and there is no obvious gradient change in the particle size of undermelted TiC. (5) After being coated by the LC method with TiC/Co50 mixture, the surface hardness of the H13 steel is greatly improved. e hardness numbers of the coating are 499 HV 0.2 , 552 HV 0.2 , 590 HV 0.2 , and 824 HV 0.2 , corresponding to Co50 coating, 10% TiC+Co50 coating, 20% TiC+Co50 coating, and 30% TiC+Co50 coating, respectively, which are 2.4-4.0 times higher than the H13 steel hardness. Adding TiC helps to increase the hardness of the coating to 53-325 HV 0.2 . e higher rate of TiC, the higher the hardness of the coating. e coating of TiC/Co50 mixture significantly enhances the wear resistance of the H13 steel surface. (6) e wear resistance of Co50 alloy, Co+10% TiC, and Co+20% TiC composite coatings is significantly higher than that of H13 steel, showing excellent wear characteristics. e friction coefficient of the coatings which have TiC is very stable. erefore, the coatings can meet the demands of tool steels applications. Moreover, the wear mechanism of the coating at room temperature is mainly brittle spalling, adhesive, and ploughing. At 700°C, the wear mechanism is mainly oxidation and fatigue. After coating by the LC method, the service life of the H13 tool steel will be greatly elongated. e research is very useful for the improvement of the wear resistance of the H13 steel.

Data Availability
e data used to support the findings of this study are available from the corresponding author upon request.

Conflicts of Interest
e authors declare that there are no conflicts of interest regarding the publication of this paper.