The Microstructure and Wear Resistance of a Copper Matrix Composite Layer on Copper via Nitrogen-Shielded Arc Cladding

A TiN and TiN·Ti2Cu reinforced copper matrix composite layer was cladded onto a T3 copper substrate to improve the anti-wear performance of copper products by means of the nitrogen-shielded gas tungsten arc cladding method (N2-GTAC). Better than the traditional preparation method of TiN, the TiN particles in the cladding layer were in situ generated using N atoms of shielding gas and Ti atoms of pre-deposited metal powders. In addition, the composite phase TiN·Ti2Cu occurred in the cladding layer, which also had a positive effect on anti-wearing. As Ti increased, the amount and grain size of TiN·Ti2Cu and TiN increased as a result. The hardness of the cladding layer increased with the increasing amount of reinforced phase generated in the layer. The hardness of the layer reached a maximum of 410 HV, which is nearly 5.1 times greater than that of copper. The TiN·Ti2Cuand TiN-reinforced phases improved the wear resistance of the cladding layers. The cladding layer with 15 wt % Ti had the longsest launch stage (600 s) and the lowest fiction coefficient (0.56).


Introduction
Copper and its alloys are widely used in the manufacturing industry for rotors and stators of power generators, thermal exchanging parts, electric conducting parts in mechanical equipment, and so on.They have excellent thermal and electrical conductivity, plasticity, and corrosion resistance.However, the major failure of copper is its surface wear, which induces the surface's deformation, lowering the strength and hardness of copper materials compared to other materials.Therefore, there has been a great demand for improving the performance of its surface [1][2][3][4].Among the various surface modification methods, one method-the in situ generation of particle-reinforced composites on the surface of metal materials-has the advantage of high controllability and cost-effectiveness, making it an effective way to enhance the surface wear resistance and service life of equipment [5].Nowadays, there are several methods of in situ generation on metal surfaces, including arc cladding [6,7], laser cladding [8][9][10][11], electron beam cladding [12,13], and plasma arc cladding [14,15].Among these methods, arc cladding is becoming one of most promising methods as it is easy to facilitate, highly flexible, and cost-effective.
TiN particles are one of most common reinforced particles that are used to enhance the surface property of metals, as it has a high melting point and hardness, perfect ductility, wear resistance, and electric conductivity [16][17][18].Some researchers have used laser cladding to prepare a TiN/Ti 3 Al particle-reinforced composite on a titanium alloy surface [19,20]; some researchers have used arc cladding and powder made of Ti, BN, and Ni to prepare a TiN-reinforced nickel matrix composite on the surface of 16Mn steel [21]; other researchers have used the power metallurgy method to prepare a nanoscale Cu-based composite with TiN particles [22] In addition, Ti 2 Cu particles regarded as an inevitable reaction of copper and titanium are a hard and brittle phase and usually used as reinforced particles in copper matrix materials.However, TiN•Ti 2 Cu-TiN-reinforced copper matrix composites prepared in situ on the surface of a copper device using arc cladding has seldom been reported.
In this paper, a TiN-and TiN•Ti 2 Cu-reinforced copper matrix composite layer was generated via a N 2 -shielded gas tungsten arc cladding method.The in situ transaction pre-deposited between the nitrogen as a shielding gas, and the Ti and Cu from the powder was conducted on the surface of T3 copper aiming to form TiN•Ti 2 Cu and TiN particles.The analysis is focused on the microstructure and wear resistance of the TiN-and TiN•Ti 2 Cu-reinforced copper matrix composite.

Materials and Methods
The materials used in this study include commercial pure copper plates (T3, Cu ≥ 99.7 wt %) with dimensions of 100 mm × 100 mm × 10 mm, and the plates were ground with water proof abrasive papers up to 500 grit and cleaned with acetone.The titanium and copper powders were selected and mixed up as cladding materials, for which the proportion of Ti was set as 5 wt %, 10 wt %, 15 wt %, and 20 wt %.The titanium powder had an average particle size of 75 µm, and the purity was greater than 99.95%; the copper powder had an average particle size of 100 µm, and the purity was over 99.5%.The copper and titanium powders were mixed according to certain proportions with turpentine oil and were then pre-coated on the surface of T3 copper with a 1.5 mm thickness.The N 2 -shielded gas tungsten arc was used as a heating resource to clad, and the cladding parameters were as follows: current: 200 A; cladding speed: 5 mm/s; shielded gas flowing velocity: 10 L/min.A thorium tungsten electrode was selected as a negative electrode, the diameter of which was 2.0 mm.
The cross sections of the cladding specimens were prepared for metallographic analysis via a standard polishing technique.The microstructures of the cladding specimens were examined via light microscopy (PMG3) (Olympus, Tokyo, Japan), and scanning electron microscopy (SEM, S-570) (Hitachi, Tokyo, Japan) equipped with an energy dispersive X-ray spectrometer (EDS, TN5500).Phase identification was carried out with an X-ray diffractometer (XRD, D8 Advance) (Bruker, Peoria, IL, USA).The harnesses along the depth of the transverse section were measured using a micro-Vickers hardness test with a load of 100 g and a loading time of 5 s.The friction coefficients were tested via multi-function friction and a wear tester (UMT-3).The specimens were cut in dimensions of 20 mm × 10 mm × 10 mm, and a sliding ball (GCr15 steel, HRC 60) with a diameter of 4 mm was used as the counter body, shown in Figure 1.The wear tests were performed at room temperature at a reciprocating sliding speed of 10 mm/s and a stroke of 5 mm, at a constant normal load of 5 N and under dry sliding conditions.Each test was conducted for 30 min, and the surface of the wear specimens were observed via SEM.
cladding and powder made of Ti, BN, and Ni to prepare a TiN-reinforced nickel matrix composite on the surface of 16Mn steel [21]; other researchers have used the power metallurgy method to prepare a nanoscale Cu-based composite with TiN particles [22] In addition, Ti2Cu particles regarded as an inevitable reaction of copper and titanium are a hard and brittle phase and usually used as reinforced particles in copper matrix materials.However, TiN•Ti2Cu-TiN-reinforced copper matrix composites prepared in situ on the surface of a copper device using arc cladding has seldom been reported.
In this paper, a TiN-and TiN•Ti2Cu-reinforced copper matrix composite layer was generated via a N2-shielded gas tungsten arc cladding method.The in situ transaction pre-deposited between the nitrogen as a shielding gas, and the Ti and Cu from the powder was conducted on the surface of T3 copper aiming to form TiN•Ti2Cu and TiN particles.The analysis is focused on the microstructure and wear resistance of the TiN-and TiN•Ti2Cu-reinforced copper matrix composite.

Materials and Methods
The materials used in this study include commercial pure copper plates (T3, Cu ≥ 99.7 wt %) with dimensions of 100 mm × 100 mm × 10 mm, and the plates were ground with water proof abrasive papers up to 500 grit and cleaned with acetone.The titanium and copper powders were selected and mixed up as cladding materials, for which the proportion of Ti was set as 5 wt %, 10 wt %, 15 wt %, and 20 wt %.The titanium powder had an average particle size of 75 μm, and the purity was greater than 99.95%; the copper powder had an average particle size of 100 μm, and the purity was over 99.5%.The copper and titanium powders were mixed according to certain proportions with turpentine oil and were then pre-coated on the surface of T3 copper with a 1.5 mm thickness.The N2-shielded gas tungsten arc was used as a heating resource to clad, and the cladding parameters were as follows: current: 200 A; cladding speed: 5 mm/s; shielded gas flowing velocity: 10 L/min.A thorium tungsten electrode was selected as a negative electrode, the diameter of which was 2.0 mm.
The cross sections of the cladding specimens were prepared for metallographic analysis via a standard polishing technique.The microstructures of the cladding specimens were examined via light microscopy (PMG3) (Olympus, Tokyo, Japan), and scanning electron microscopy (SEM, S-570) (Hitachi, Tokyo, Japan) equipped with an energy dispersive X-ray spectrometer (EDS, TN5500).Phase identification was carried out with an X-ray diffractometer (XRD, D8 Advance) (Bruker, Peoria, IL, USA).The harnesses along the depth of the transverse section were measured using a micro-Vickers hardness test with a load of 100 g and a loading time of 5 s.The friction coefficients were tested via multi-function friction and a wear tester (UMT-3).The specimens were cut in dimensions of 20 mm × 10 mm × 10 mm, and a sliding ball (GCr15 steel, HRC 60) with a diameter of 4 mm was used as the counter body, shown in Figure 1.The wear tests were performed at room temperature at a reciprocating sliding speed of 10 mm/s and a stroke of 5 mm, at a constant normal load of 5 N and under dry sliding conditions.Each test was conducted for 30 min, and the surface of the wear specimens were observed via SEM.

Morphology and Microstructure of the Cladding Layer
Figure 2a shows the macro profile of the cross section of 15 wt % cladding specimens; good metallurgy bonding occurred between the base metal and cladding alloy powders, and there were no cracks or pores in the reaction interface.It is evident from Figure 2b that the cladding layer could be divided into two layers-the in situ transaction layer (ISTL) on the top and the remelting layer (RL) in the middle.Moreover, there is a heat affected zone (HAZ) between the RL and base metal.The in situ transaction mainly emerged at the domain of the ISTL, as the density of Ti powder was lower than that of the Cu, and melting Ti powder remained in the top region reacting with N to form a second particle.Thus, in the ISTL region, some second phase particles were distributed among the matrix as an effect of in situ transaction.In addition, in the RL region, the columnar crystals were in a large majority.Via EDS analysis of the RL, Point A contains 97.82 wt % Cu and 2.18 wt % Ti, and is identified as α-Cu (Ti).During the formation of this RL, with the heating effect of the arc cladding, some base metals melted while failing to mix with the cladding powder, and then solidified into columnar crystals (α-Cu).

Morphology and Microstructure of the Cladding Layer
Figure 2a shows the macro profile of the cross section of 15 wt % cladding specimens; good metallurgy bonding occurred between the base metal and cladding alloy powders, and there were no cracks or pores in the reaction interface.It is evident from Figure 2b that the cladding layer could be divided into two layers-the in situ transaction layer (ISTL) on the top and the remelting layer (RL) in the middle.Moreover, there is a heat affected zone (HAZ) between the RL and base metal.The in situ transaction mainly emerged at the domain of the ISTL, as the density of Ti powder was lower than that of the Cu, and melting Ti powder remained in the top region reacting with N to form a second particle.Thus, in the ISTL region, some second phase particles were distributed among the matrix as an effect of in situ transaction.In addition, in the RL region, the columnar crystals were in a large majority.Via EDS analysis of the RL, Point A contains 97.82 wt % Cu and 2.18 wt % Ti, and is identified as α-Cu (Ti).During the formation of this RL, with the heating effect of the arc cladding, some base metals melted while failing to mix with the cladding powder, and then solidified into columnar crystals (α-Cu).The thickness of the ISTL, the RL, and the HAZ with the Ti powder varied from 5 wt % to 20 wt % (Figure 3).When Ti content was limited to 5 wt %, the ISTL was not observed at the surface of the cladding layer, and the thickness of the RL was about 5 mm, the maximum thickness among these specimens.The main reason for this may be that, in this content range, the formation of in situ phases is too limited to form an independent area and that these phases are mainly located in the RL, which may be relevant to the maximum thickness of the RL.When Ti content was up to 10 wt %, an ISTL formed on the top of the cladding layer, which was about 1.3 mm in thickness.As Ti content increased, the thickness of the independent ISTL showed a declining trend, the thickness of the RL dropped significantly from 5 mm to 2.2 mm, and the thickness of the HAZ decreased slightly from 1.5 mm to 0.7.There are two reasons to explain this variation: first, an increasing amount of Ti in the powder led to a decrease in the thermal conductivity of the mixed powder, as the thermal conductivity coefficient of titanium is less than one-tenth of copper; second, the reaction of TiN and the intermetallic compounds (IMCs) needed to absorb the heat from the heat source.Therefore, the more Ti content the powder had, the more heat was assumed in the in situ transaction; with the same amount of heat input, the thicknesses of the ISTL, the RL, and the HAZ each showed declining tendencies.
The XRD analysis of the cladding layer with 5 wt % and 20 wt % Ti is shown in Figure 4.It is clear that, after arc cladding, the diffraction peaks of β-Ti disappeared, and the diffraction peaks of the TiN phase alternatively appeared.Moreover, the diffraction peak of the α-Cu phase remained.According to the chemical composition of the powder and base metal, it is easy to conclude that TiN was in situ generated in the cladding layer using the Ti atoms from the metal powder and the N The thickness of the ISTL, the RL, and the HAZ with the Ti powder varied from 5 wt % to 20 wt % (Figure 3).When Ti content was limited to 5 wt %, the ISTL was not observed at the surface of the cladding layer, and the thickness of the RL was about 5 mm, the maximum thickness among these specimens.The main reason for this may be that, in this content range, the formation of in situ phases is too limited to form an independent area and that these phases are mainly located in the RL, which may be relevant to the maximum thickness of the RL.When Ti content was up to 10 wt %, an ISTL formed on the top of the cladding layer, which was about 1.3 mm in thickness.As Ti content increased, the thickness of the independent ISTL showed a declining trend, the thickness of the RL dropped significantly from 5 mm to 2.2 mm, and the thickness of the HAZ decreased slightly from 1.5 mm to 0.7.There are two reasons to explain this variation: first, an increasing amount of Ti in the powder led to a decrease in the thermal conductivity of the mixed powder, as the thermal conductivity coefficient of titanium is less than one-tenth of copper; second, the reaction of TiN and the intermetallic compounds (IMCs) needed to absorb the heat from the heat source.Therefore, the more Ti content the powder had, the more heat was assumed in the in situ transaction; with the same amount of heat input, the thicknesses of the ISTL, the RL, and the HAZ each showed declining tendencies.
The XRD analysis of the cladding layer with 5 wt % and 20 wt % Ti is shown in Figure 4.It is clear that, after arc cladding, the diffraction peaks of β-Ti disappeared, and the diffraction peaks of the TiN phase alternatively appeared.Moreover, the diffraction peak of the α-Cu phase remained.According to the chemical composition of the powder and base metal, it is easy to conclude that TiN was in situ generated in the cladding layer using the Ti atoms from the metal powder and the N atoms from the shielding gas.Two phases, i.e., α-Cu and TiN, formed in the layer of the 5 wt % specimen, while three phases, i.e., α-Cu, TiN, and Ti 2 Cu•TiN, formed in the layer of the 20 wt % specimen.It is worth mentioning that TiN was not only in the single phase, but also in the form of a composite phase-Ti 2 Cu•TiN.Obviously, the Ti 2 Cu phase was synthesized in the arc molten pool using Ti and Cu atoms to form IMCs, and Ti 2 Cu combined with TiN generated a composite phase-Ti 2 Cu•TiN.
Coatings 2016, 6, 67 4 of 9 atoms from the shielding gas.Two phases, i.e., α-Cu and TiN, formed in the layer of the 5 wt % specimen, while three phases, i.e., α-Cu, TiN, and Ti2Cu•TiN, formed in the layer of the 20 wt % specimen.It is worth mentioning that TiN was not only in the single phase, but also in the form of a composite phase-Ti2Cu•TiN.Obviously, the Ti2Cu phase was synthesized in the arc molten pool using Ti and Cu atoms to form IMCs, and Ti2Cu combined with TiN generated a composite phase-Ti2Cu•TiN.Figure 5 shows the microstructure of the cladding layer of the 20 wt % specimen, and it can be seen that there are three different shape structures in this profile.Thus, these points represent these three structures and were measured by EDS analysis.Point 1 shows that there is a large amount of Ti and small proportions of N and Cu in the area around that point.Combined with the result of XRD, the phase around Point 1 can be defined as Ti2Cu•TiN.The phase in the region of Point 2 has a dendrite crystal structure that has a large proportion of N and small proportions of Ti and Cu.It can be inferred that N reacted with Ti to form TiN and residual N solutes in α-Cu.Therefore, the phase in the region of Point 2 can be defined as TiN and the α-Cu that solutes some N.In addition, in the Point 3 area, the main element is Cu, which means that the phase in this area is Ti, an α-Cu dissolving element.atoms from the shielding gas.Two phases, i.e., α-Cu and TiN, formed in the layer of the 5 wt % specimen, while three phases, i.e., α-Cu, TiN, and Ti2Cu•TiN, formed in the layer of the 20 wt % specimen.It is worth mentioning that TiN was not only in the single phase, but also in the form of a composite phase-Ti2Cu•TiN.Obviously, the Ti2Cu phase was synthesized in the arc molten pool using Ti and Cu atoms to form IMCs, and Ti2Cu combined with TiN generated a composite phase-Ti2Cu•TiN.Figure 5 shows the microstructure of the cladding layer of the 20 wt % specimen, and it can be seen that there are three different shape structures in this profile.Thus, these points represent these three structures and were measured by EDS analysis.Point 1 shows that there is a large amount of Ti and small proportions of N and Cu in the area around that point.Combined with the result of XRD, the phase around Point 1 can be defined as Ti2Cu•TiN.The phase in the region of Point 2 has a dendrite crystal structure that has a large proportion of N and small proportions of Ti and Cu.It can be inferred that N reacted with Ti to form TiN and residual N solutes in α-Cu.Therefore, the phase in the region of Point 2 can be defined as TiN and the α-Cu that solutes some N.In addition, in the Point 3 area, the main element is Cu, which means that the phase in this area is Ti, an α-Cu dissolving element.Figure 5 shows the microstructure of the cladding layer of the 20 wt % specimen, and it can be seen that there are three different shape structures in this profile.Thus, these points represent these three structures and were measured by EDS analysis.Point 1 shows that there is a large amount of Ti and small proportions of N and Cu in the area around that point.Combined with the result of XRD, the phase around Point 1 can be defined as Ti 2 Cu•TiN.The phase in the region of Point 2 has a dendrite crystal structure that has a large proportion of N and small proportions of Ti and Cu.It can be inferred that N reacted with Ti to form TiN and residual N solutes in α-Cu.Therefore, the phase in the region of Point 2 can be defined as TiN and the α-Cu that solutes some N.In addition, in the Point 3 area, the main element is Cu, which means that the phase in this area is Ti, an α-Cu dissolving element.The microstructures of the cladding layer with variation in Ti content are shown in Figure 6.It can be seen that the black and yellow phase is Ti2Cu•TiN, the fine silver-gray phase is TiN, and the matrix phase is α-Cu.In the specimen of 5 wt % Ti, the main phase is α-Cu with some silver-gray TiN phase distributed therein.In the specimen of 15 wt % Ti, the amount of yellow phase Ti2Cu•TiN, which is dispersed uniformly, markedly increases, as TiN does.The average size of the Ti2Cu•TiN phases is 10 μm.In the specimen of 20 wt % Ti, a large amount of Ti2Cu•TiN emerges and becomes the main phase in the cladding layer, and the average size of Ti2Cu•TiN increases to 15 μm.Through a comparison of specimens of different Ti proportions, it could be concluded that, as Ti increased in the cladding powder, the amount of Ti2Cu•TiN phase, as well as its shape, increases.By contrast, the increasing trend of TiN is limited.The proportion of these three phases varying in Ti content has a vital influence on the mechanical property of the cladding layer.The microstructures of the cladding layer with variation in Ti content are shown in Figure 6.It can be seen that the black and yellow phase is Ti 2 Cu•TiN, the fine silver-gray phase is TiN, and the matrix phase is α-Cu.In the specimen of 5 wt % Ti, the main phase is α-Cu with some silver-gray TiN phase distributed therein.In the specimen of 15 wt % Ti, the amount of yellow phase Ti 2 Cu•TiN, which is dispersed uniformly, markedly increases, as TiN does.The average size of the Ti 2 Cu•TiN phases is 10 µm.In the specimen of 20 wt % Ti, a large amount of Ti 2 Cu•TiN emerges and becomes the main phase in the cladding layer, and the average size of Ti 2 Cu•TiN increases to 15 µm.Through a comparison of specimens of different Ti proportions, it could be concluded that, as Ti increased in the cladding powder, the amount of Ti 2 Cu•TiN phase, as well as its shape, increases.By contrast, the increasing trend of TiN is limited.The proportion of these three phases varying in Ti content has a vital influence on the mechanical property of the cladding layer.The microstructures of the cladding layer with variation in Ti content are shown in Figure 6.It can be seen that the black and yellow phase is Ti2Cu•TiN, the fine silver-gray phase is TiN, and the matrix phase is α-Cu.In the specimen of 5 wt % Ti, the main phase is α-Cu with some silver-gray TiN phase distributed therein.In the specimen of 15 wt % Ti, the amount of yellow phase Ti2Cu•TiN, which is dispersed uniformly, markedly increases, as TiN does.The average size of the Ti2Cu•TiN phases is 10 μm.In the specimen of 20 wt % Ti, a large amount of Ti2Cu•TiN emerges and becomes the main phase in the cladding layer, and the average size of Ti2Cu•TiN increases to 15 μm.Through a comparison of specimens of different Ti proportions, it could be concluded that, as Ti increased in the cladding powder, the amount of Ti2Cu•TiN phase, as well as its shape, increases.By contrast, the increasing trend of TiN is limited.The proportion of these three phases varying in Ti content has a vital influence on the mechanical property of the cladding layer.

Micro-Hardness and Anti-Wear Performance of Cladding Layer
Figure 7 shows the hardness of cladding layers with variation in Ti content.It can be seen that the hardness varies in layers with different Ti amounts.Taking the 20 wt % Ti specimen, for example, the maximum occurs in the region of the ISRL, which is about 410 HV.This hardness is 5.2 times greater than that of the T3 copper (81 HV).The maximum hardness of 15 wt %, 10 wt %, and 5 wt % is 305 HV, 271 HV, and 178 HV, respectively.The significant improvement in the hardness of the cladding layer is mainly due to the fact that the Ti 2 Cu•TiN and TiN phases played a role in the second phase, strengthening the matrix.In addition, within the sample with the same Ti amount, the variation curve of the hardness increases first and decreases afterwards because the reinforced phases at the surface were burned and significantly lost.Usually, the hardness 0.5-1 mm away from the surface reaches the climax point.

Micro-Hardness and Anti-Wear Performance of Cladding Layer
Figure 7 shows the hardness of cladding layers with variation in Ti content.It can be that the hardness varies in layers with different Ti amounts.Taking the 20 wt % Ti specimen, for example, the maximum occurs in the region of the ISRL, which is about 410 HV.This hardness is 5.2 times greater than that of the T3 copper (81 HV).The maximum hardness of 15 wt %, 10 wt %, and 5 wt % is 305 HV, 271 HV, and 178 HV, respectively.The significant improvement in the hardness of the cladding layer is mainly due to the fact that the Ti2Cu•TiN and TiN phases played a role in the second phase, strengthening the matrix.In addition, within the sample with the same Ti amount, the variation curve of the hardness increases first and decreases afterwards because the reinforced phases at the surface were burned and significantly lost.Usually, the hardness 0.5-1 mm away from the surface reaches the climax point.Figure 8 shows the friction coefficients of different amounts of Ti and the substrate, and it is evident that, with the addition of the cladding layer on the copper, the friction performance improved relative to the T3 copper.The launch stage was about 150 s, and the friction coefficient was 0.72.By contrast, with the cladding layers distributed with TiN and Ti2Cu•TiN, the launch stages last longer: 210 s (5 wt % Ti), 208 s (10 wt % Ti), 638 s (15 wt % Ti), and 552 s (20 wt % Ti).The increase in the duration of the launch stage entails that the cladding layer is more wear-resistant than the substrate.Upon reaching the stable friction period, the friction coefficients of the layer with different Ti amounts tended to stabilize.Their values are as follows: 0.68 (5 wt % Ti), 0.61 (10 wt % Ti), 0.56 (15 wt % Ti), and 0.62 (20 wt % Ti).This reveals that, although the friction coefficient of 5 wt % is close to the substrate, the friction coefficients improved when the proportion of Ti was above 10 wt %.Among the specimens with different Ti amounts, the cladding layer of 15 wt % Ti had the lowest friction coefficient 0.56.
Figure 9 shows the wearing morphology of the substrate and layers with different Ti amounts.Ploughed grooves and copper abrasive chips on the T3 copper are evident (Figure 9a).The grooves were generated as a cutting function of the GCr15 ball, with a certain level of sliding tangential force on the T3 surface.The main reason for the abrasive chips is that the T3 copper surface experienced a serious softening effect and plastic deformation during the abrasion with the GCr15 ball.Abrasive chips, which adhered to the adjacent area of the surface, then formed.Therefore, the main abrasive mechanisms of the T3 copper were micro-cutting and adhesive wear.From Figure 9b, it is evident that the main abrasive mechanism was micro-cutting, as there are uniform grooves on the surface of the cladding layer.The adhesive wear effect here is not obvious, because the layer was reinforced by Ti, and the hardness improved.Figure 9c shows that the surface of the wearing area was relatively Figure 8 shows the friction coefficients of different amounts of Ti and the substrate, and it is evident that, with the addition of the cladding layer on the copper, the friction performance improved relative to the T3 copper.The launch stage was about 150 s, and the friction coefficient was 0.72.By contrast, with the cladding layers distributed with TiN and Ti 2 Cu•TiN, the launch stages last longer: 210 s (5 wt % Ti), 208 s (10 wt % Ti), 638 s (15 wt % Ti), and 552 s (20 wt % Ti).The increase in the duration of the launch stage entails that the cladding layer is more wear-resistant than the substrate.Upon reaching the stable friction period, the friction coefficients of the layer with different Ti amounts tended to stabilize.Their values are as follows: 0.68 (5 wt % Ti), 0.61 (10 wt % Ti), 0.56 (15 wt % Ti), and 0.62 (20 wt % Ti).This reveals that, although the friction coefficient of 5 wt % is close to the substrate, the friction coefficients improved when the proportion of Ti was above 10 wt %.Among the specimens with different Ti amounts, the cladding layer of 15 wt % Ti had the lowest friction coefficient 0.56.
Figure 9 shows the wearing morphology of the substrate and layers with different Ti amounts.Ploughed grooves and copper abrasive chips on the T3 copper are evident (Figure 9a).The grooves were generated as a cutting function of the GCr15 ball, with a certain level of sliding tangential force on the T3 surface.The main reason for the abrasive chips is that the T3 copper surface experienced a serious softening effect and plastic deformation during the abrasion with the GCr15 ball.Abrasive chips, which adhered to the adjacent area of the surface, then formed.Therefore, the main abrasive mechanisms of the T3 copper were micro-cutting and adhesive wear.From Figure 9b, it is evident that the main abrasive mechanism was micro-cutting, as there are uniform grooves on the surface of the cladding layer.The adhesive wear effect here is not obvious, because the layer was reinforced by Ti, and the hardness improved.Figure 9c shows that the surface of the wearing area was relatively flat, and the grooves appear narrow and short, which is mainly because the occurrence of Ti 2 Cu•TiN and TiN reinforced the matrix and kept the GCr15 ball from pressing into the cladding layer.Figure 9d shows the wearing appearance of the 20 wt % specimen; the wearing area was rougher than the other specimens, and there are large-sized pits exposed to the air.This coarse wearing surface resulted in an increase in friction coefficient.
flat, and the grooves appear narrow and short, which is mainly because the occurrence of Ti2Cu•TiN and TiN reinforced the matrix and kept the GCr15 ball from pressing into the cladding layer.Figure 9d shows the wearing appearance of the 20 wt % specimen; the wearing area was rougher than the other specimens, and there are large-sized pits exposed to the air.This coarse wearing surface resulted in an increase in friction coefficient.flat, and the grooves appear narrow and short, which is mainly because the occurrence of Ti2Cu•TiN and TiN reinforced the matrix and kept the GCr15 ball from pressing into the cladding layer.Figure 9d shows the wearing appearance of the 20 wt % specimen; the wearing area was rougher than the other specimens, and there are large-sized pits exposed to the air.This coarse wearing surface resulted in an increase in friction coefficient.

1.
The TiN•Ti 2 Cu-and TiN-reinforced copper matrix composite layer was in situ prepared on the surface of T3 copper successfully by means of N 2 shielding gas tungsten arc cladding technology.The interface between the cladding layer and the substrate has a fine and uniform distribution without cracks and slags.As Ti increased, TiN•Ti 2 Cu and TiN increased as a result.

2.
The hardness of the cladding layer increased as the amount of reinforced phase generated in the layer increased.The hardness of the layer reached a maximum of 410 HV, 5.1 times greater than that of copper.

3.
The TiN•Ti 2 Cu-and TiN-reinforced phases improved the wear resistance of the cladding layers.
The cladding layer with 15 wt % Ti had a longest launch stage of 638 s and a minimum fiction coefficient of 0.56.

Figure 1 .
Figure 1.Sketch of dry sliding friction and wear test.Figure 1. Sketch of dry sliding friction and wear test.

Figure 1 .
Figure 1.Sketch of dry sliding friction and wear test.Figure 1. Sketch of dry sliding friction and wear test.

Figure 3 .
Figure 3.The thickness of the ISTL, the RL, and the HAZ with varying Ti content.

Figure 3 .
Figure 3.The thickness of the ISTL, the RL, and the HAZ with varying Ti content.

Figure 3 .
Figure 3.The thickness of the ISTL, the RL, and the HAZ with varying Ti content.

Figure 5 .
Figure 5. Microstructure morphology of the cladding metal in 20 wt % Ti powder and EDS analysis of point 1, point 2 and point 3.

Figure 5 .
Figure 5. Microstructure morphology of the cladding metal in 20 wt % Ti powder and EDS analysis of point 1, point 2 and point 3.

Figure 5 .
Figure 5. Microstructure morphology of the cladding metal in 20 wt % Ti powder and EDS analysis of point 1, point 2 and point 3.

Figure 7 .
Figure 7.The micro-hardness of the cladding layer with different Ti amounts.

Figure 7 .
Figure 7.The micro-hardness of the cladding layer with different Ti amounts.

Figure 8 .Figure 9 .
Figure 8. Friction coefficient of the cladding layer with different Ti amounts.

Figure 8 .
Figure 8. Friction coefficient of the cladding layer with different Ti amounts.

Figure 8 .Figure 9 .
Figure 8. Friction coefficient of the cladding layer with different Ti amounts.