等离子喷涂制备WC-Co-Cu-BaF2/CaF2自润滑耐磨涂层及其高温摩擦性能

通过大气等离子喷涂方法,使用自制的含有WC-Co、Cu和BaF2/CaF2共晶体的复合喷涂粉末,制备出WC-Co-Cu-BaF2/CaF2自润滑耐磨涂层。在200℃、400℃和600℃下进行WC-Co-Cu-BaF2/CaF2涂层和WC-Co涂层的高温摩擦试验,用扫描电镜观察涂层磨损表面微观形貌。结果表明:200℃时,由于WC-Co-Cu-BaF2/CaF2涂层摩擦产物层中含有的WC硬质颗粒引起磨粒磨损,该涂层摩擦因数和磨损率相对较高。而400℃和600℃时,WC-Co-Cu-BaF2/CaF2涂层的摩擦产物层中均无WC颗粒存在,且由于涂层中Cu和BaF2/CaF2等固体润滑剂的作用,生成的摩擦产物层光滑且致密,涂层的摩擦因数和磨损率均较低,在400～600℃下表现出比WC-Co涂层优异的耐磨性能。     

等离子喷涂制备WC-Co-Cu-BaF_2/CaF_2自润滑耐磨涂层及其高温摩擦性能

通过大气等离子喷涂方法,使用自制的含有WC-Co、Cu和BaF2/CaF2共晶体的复合喷涂粉末,制备出WC-Co-Cu-BaF2/CaF2自润滑耐磨涂层。在200℃、400℃和600℃下进行WC-Co-Cu-BaF2/CaF2涂层和WC-Co涂层的高温摩擦试验,用扫描电镜观察涂层磨损表面微观形貌。结果表明:200℃时,由于WC-Co-Cu-BaF2/CaF2涂层摩擦产物层中含有的WC硬质颗粒引起磨粒磨损,该涂层摩擦因数和磨损率相对较高。而400℃和600℃时,WC-Co-Cu-BaF2/CaF2涂层的摩擦产物层中均无WC颗粒存在,且由于涂层中Cu和BaF2/CaF2等固体润滑剂的作用,生成的摩擦产物层光滑且致密,涂层的摩擦因数和磨损率均较低,在400～600℃下表现出比WC-Co涂层优异的耐磨性能。     

NiCrAlYSi/h-BN高温可磨耗封严涂层摩擦磨损性能研究

目的加入h-BN和团聚聚苯酯分别作为固体润滑剂和造孔剂,以提高NiCrAlYSi基封严涂层的高温摩擦磨损性能。方法采用真空熔炼雾化造粒和料浆喷雾造粒技术制备NiCrAlYSi/h-BN聚苯酯复合粉体,再利用大气等离子喷涂技术制备高温可磨耗封严涂层,通过扫描电子显微镜(SEM)、能谱仪(EDS)、CSM摩擦磨损试验机和三维轮廓仪等手段,研究NiCrAlYSi/h-BN封严涂层显微结构、元素组成以及室温和800℃下的摩擦磨损性能,探究涂层在室温和800℃下的磨损机理。结果等离子喷涂NiCrAlYSi/h-BN封严涂层组织比较均匀,涂层结合强度可达15MPa,孔隙率约为32%。室温下封严涂层与DD6镍基单晶高温合金球间的平均摩擦因数为0.897,涂层磨损体积为2.09×10~8μm~3;800℃高温下平均摩擦因数为0.425,涂层磨损体积为3.22×10~8μm~3;封严涂层800℃下有良好的可磨耗性,相应对偶件的磨损较轻;高温下,封严涂层金属基相软化、h-BN的润滑作用和部分金属基相高温下生成自润滑性氧化物,是摩擦因数降低和对偶件磨损较轻的主要原因。NiCrAlYSi/h-BN封严涂层室温的主要磨损机理为涂抹、磨粒磨损和轻微氧化,高温下的主要磨损机理为切削、塑性变形、氧化和粘着磨损。结论等离子喷涂NiCrAlYSi/h-BN高温封严涂层在高温下的可磨耗性能较好。     

Molybdenum based amorphous and nanocrystalline coatings prepared by high velocity oxy-fuel spraying

The high velocity oxy-fuel(HVOF) based thermal spray process has developed as a potential advantageous approach for fabricating various kinds of functional coatings.In this article,the coatings of Mo-based alloy were synthesized using the HVOF process.The microstructure and the mechanical properties of the HVOF-processed coatings were investigated using SEM,TEM,XRD,and hardness and wear tests.Annealing treatment was applied to the as-sprayed coatings to develop the microstructure and its effect on the microstructure and mechanical properties of the coatings was examined.It is found that the HVOF-processed Mo-based alloy coatings are comprised of an amorphous splat matrix embedded with nano-sized crystalline particles.Annealing at temperatures over 950 ℃ results into crystallization of the amorphous matrix.The mechanical properties of the as-sprayed coatings are enhanced with annealing temperature up to 750 ℃ and from 950 to 1050 ℃,keeps constant between 750 and 950 ℃,and reduce over 1050 ℃.The change of the mechanical property with the microstructure was illustrated in the study.     

Dry sliding wear behavior of PVD TiN,Ti55Al45N,and Ti35Al65N coatings at temperatures up to 600 °C

Three PVD nitride coatings (TiN, Ti₅₅Al₄₅N, and Ti₃₅Al₆₅N) with different Al content were deposited on the cemented carbides by cathode arc-evaporation technique. Microstructural and fundamental properties of these nitride coatings were examined. The friction and wear behavior of these coatings were evaluated at temperatures up to 600 °C. The wear surface features of the test samples were examined by scanning electron microscopy. Results showed that the friction coefficient of these nitride coatings is different depending on the temperature. The friction coefficient of TiN coating increased with the increase of test temperature; while the friction coefficient of Ti₅₅Al₄₅N and Ti₃₅Al₆₅N coatings with the addition of Al decreased with the increase of test temperature. The Ti₅₅Al₄₅N and Ti₃₅Al₆₅N coatings exhibited higher wear resistance over the one without Al (TiN coating). The wear resistance of these nitride coatings at high temperature wear tests is significantly dependent on their tribological oxidation behavior. The Ti₅₅Al₄₅N and Ti₃₅Al₆₅N coatings with the addition of Al exhibited improved wear resistance as compared to the TiN coating, which was attributed to that their tribo-chemically formed Al₂O₃ exhibited better tribological properties than the TiO₂ of the latter.     

Friction and Wear Behavior of AlTiN-Coated Carbide Balls Against SKD11 Hardened Steel at Elevated Temperatures

In this study, AlTiN coatings were deposited on YT14 cemented carbide balls by arc ion plating technique. The friction and wear behavior of the AlTiN-coated balls against SKD11 hardened steel was investigated by sliding tests using a ball-ondisk tribometer at various temperatures from 25 to 700 °C in air. The results showed that the friction and wear behavior was significantly influenced by the testing temperature. Obvious fluctuations were observed in the friction curves at elevated temperatures, which could be attributed to the formation and rupture of unstable Fe and Cr oxide layers. As the temperature increased from 25 to 500 °C, the wear rate of the coated balls increased from the scale of 10~(-21)–10~(-20) m~3/N m, and then decreased to 10~(-22) m~3/N m as the temperature further increased to 700 °C. It was also found that the friction and wear behavior of the coated balls was directly dependent on the counterpart materials. As the temperature increased, the main wear mechanism of the coated balls changed from mild abrasive wear and adhesive wear to abrasive wear failure at 500 °C, and then transferred to adhesive wear and mild oxidation wear at 700 °C. For SKD11 hardened steel, the primary wear mechanism changed from delamination wear to abrasive wear and then transferred to plastic deformation and fatigue wear, accompanied by adhesive wear and tribo-oxidation wear.     

Structure and tribological properties of AlCrTiN coatings at elevated temperature

In this study, we analyzed the high temperature tribological behavior of AlCrTiN coatings deposited on WC substrates by low cathodic arc technique. The coatings chemical composition, Al 31 at.%, Cr 16 at.%, Ti 7 at.% and N 46 at.%, and the bonding state were evaluated by X-ray photoelectron spectroscopy. The mechanical properties of the coatings were studied by scratch-test and nanohardness depth sensing indentation. The morphology of the coatings surface, ball scars, wear tracks and wear debris as well as the oxidized samples was examined by scanning electron microscopy (SEM) and energy dispersive X-ray spectroscopy (EDX). The structure was analyzed using X-ray diffraction (XRD). Wear testing was carried out using a high temperature tribometer (pin-on-disc) with alumina balls as counterparts. The evaluation of the friction coefficient with the number of cycles (sliding distance) was assessed at different temperatures and the wear rates of the coatings and balls were determined; the maximum testing temperature was 800 °C. The coating showed an excellent thermal stability and wear resistance. The friction reached a maximum at 500 °C and then decreased, whereas the wear rate was negligible up to 600 °C and increased significantly at higher temperatures.     

TRIBOLOGICAL AND HIGH SPEED TURNING PERFORMANCE IN Ti1-xAlxN COATINGS PREPARED BY CLOSE-FIELD UNBALANCED MAGNETRON SPLTTERING

Titanium-aluminium-nitride (Ti1-xAlxN) coatings were deposited by close-field unbalanced magnetron sputtering on M42 steel substrates and WC-6wt%Co inserts at 450℃. The tribological behavior was analyzed by sliding against steel and WC-6wt%Co balls, while the turning performance was evaluated by a conventional turning machine at high cutting speeds without using coolants. In the tribological tests, the formation of transfer layer and the variations of hardness of the coatings played an important role for sliding against steel balls. For the coatings sliding against WC-6wt%Co balls, the Ti-Al-N coatings showed a similar friction coefficient, but the TiN coating exhibited a lower value. The difference could be explained by the tri-oxidation wear mechanism. In the turning tests, a superior cutting performance of the coating was found at x=0.45, which endured 38 minutes before the tool flank wear reached the maximum value of 0.3mm, whereas only 20 minutes were endured for the TiN coating. The excellent performance of the coatings in the turning tests could be explained by the enhanced mechanical properties and oxidation/diffusion resistance of the coatings.     

High temperature performance of arc-sprayed aluminum bronze coatings for steel

1 Introduction The aluminum bronze coatings on steel substrate which are sprayed by electric arc process have been developed as possible new candidates for the use to high temperature applications, while their corrosion properties at high temperature in …     

Engineering HVOF-Sprayed Cr3C2-NiCr Coatings: The Effect of Particle Morphology and Spraying Parameters on the Microstructure, Properties, and High Temperature Wear Performance

Chromium carbide-based thermally sprayed coatings are widely used for high temperature wear applications (typical temperature range from 540 to 900 °C). In these extreme environments at those temperatures, several phenomena will degrade, oxidize, and change the microstructure of the coatings, thereby affecting their wear behavior. Although it can be easily conceived that the Cr₃C₂-NiCr coating microstructure evolution after high temperature exposure will depend on the as-sprayed microstructure and spraying parameters, very little has been done in this regard. This study intends to develop a better understanding of the effect of spraying parameters on the resulting chromium carbide coating microstructure after high temperature operation and high temperature sliding wear properties. The microstructures of different coatings produced from two morphologies of Cr₃C₂-NiCr powders and under a window of in-flight particle temperature and velocity values were characterized through x-ray diffraction and scanning electron microscopy. Sliding wear at 800 °C was performed and the wear behavior correlated with the spraying parameters and coating microstructure. Vickers microhardness (300 gf) of the coatings before and after sliding wear was also measured.     

The Influence of Temperature on Frictional Behavior of Plasma-Sprayed NiAl-Cr2O3 Based Self-Adaptive Nanocomposite Coatings

Frictional behavior of nano and hybrid-structured NiAl-Cr₂O₃-Ag-CNT-WS₂ adaptive self-lubricant coatings was evaluated at a range of temperatures, from room temperature to 700 °C. For this purpose, hybrid structured (HS) and nanostructured (NS) composite powders with the same nominal compositions were prepared by spray drying and heat treatment techniques. A series of HS and NS coating samples were deposited on steel substrate by an atmospheric plasma spraying process. The tribological behavior of both coatings was studied from room temperature to 700 °C at 100° intervals using a custom designed high temperature wear test machine. Scanning electron microscopy was employed for the evaluation of the composite coatings and worn surfaces. Experimental results indicated that the hybrid coating had inferior tribological properties when compared to the nanostructured coating, showing the attractive frictional behavior on the basis of low friction and high wear resistance; the NS coating possessed a more stable friction coefficient in the temperature range of 25-700 °C against alumina counterface. Microstructural examinations revealed more uniformity in NS plasma-sprayed coatings.     

Improvement of the oxidation and wear resistance of pure Ti by laser cladding at elevated temperature

NiCrBSi and NiCrBSi/WC-Ni composite coatings were produced on pure Ti substrates by the laser cladding technology. Thermal gravimetric (TG) analysis was used to evaluate the high temperature oxidation resistance of the laser cladding coatings. The friction and wear behavior was tested through sliding against the Si₃N₄ ball at elevated temperatures of 300 °C and 500 °C. Besides, the morphologies of the worn surfaces and wear debris were analyzed by scanning electron microscopy (SEM) and three dimensional non-contact surface mapping. The results show that the microhardness, high temperature oxidation resistance and high temperature wear resistance of the pure Ti substrates are greatly increased. For the pure Ti substrate, the wear behavior is dominated by adhesive wear, abrasive wear and severe plastic deformation, while both laser cladding coatings, involving only mild abrasive and fatigue wear, are able to prevent the substrates from severe adhesion and abrasive wear. In particular, the laser cladding NiCrBSi/WC-Ni composite coating shows better high temperature wear resistance than the NiCrBSi coating, which is due to the formation of a hard WC phase in the composite coating.     

NiCrBSi超音速火焰喷涂层在不同温度下的磨损行为

采用超音速火焰喷涂在铸铁表面制备了NiCrBSi喷涂涂层,以研究其在不同温度下的摩擦磨损行为.?采用pin-on-disc试验设备在室温和300?℃下对NiCrBSi涂层进行了摩擦磨损试验,分析了温度对NiCrBSi涂层摩擦系数和磨损率的影响规律;采用XRD和SEM对NiCrBSi喷涂态涂层进行了微观组织结构分析;通过...     

等离子喷涂 NiCr / Cr3 C2 -hBN 复合涂层的制备及摩擦性能研究

目的加入h BN作为固体润滑剂,提高Ni Cr/Cr3C2复合涂层的摩擦性能。方法采用化工冶金包覆、喷雾造粒和固相合金化技术制备Ni Cr/Cr3C2-10%h BN复合粉体,再采用等离子喷涂技术制备复合涂层。通过扫描电子显微镜(SEM)、X射线衍射(XRD)和高温摩擦磨损试验等手段研究粉体和涂层的显微结构、物相组成以及室温至800℃的摩擦磨损性能,探讨Ni Cr/Cr3C2-10%h BN复合涂层在室温和400,800℃下的磨损机理。结果等离子喷涂Ni Cr/Cr3C2-10%h BN复合涂层呈典型的层状结构,涂层结合强度可达24 MPa,孔隙率为(8.47±0.5)%。涂层的摩擦系数和磨损率均随着温度的升高而先升高,后逐渐降低,400℃时最高,分别约为0.59和9.2×10-4mm3/(N·m),800℃时分别降至0.45和4.1×10-4mm3/(N·m)。高温下,h BN润滑膜和金属氧化物的形成是摩擦系数和磨损率降低的主要原因。室温下涂层的主要磨损机制是脆性断裂;400℃时,涂层的主要磨损机制是脆性断裂、塑形变形和轻微粘着磨损;800℃时,涂层的主要磨损机制是塑性变形、氧化、粘着磨损和涂层转移至对偶件。结论等离子喷涂Ni Cr/Cr3C2-10%h BN复合涂层在室温和高温下的润滑性能较好。     

真空退火处理对掺Cr类石墨碳膜力学和摩擦学性能的影响

采用闭合场非平衡磁控溅射离子镀技术制备了掺Cr类石墨镀层,研究了真空退火温度对镀层的硬度、结合强度、摩擦系数和比磨损率的影响规律,通过X射线衍射(XRD)分析了镀层结构随退火温度的变化.结果表明:随退火温度的升高,镀层有新相生成,镀层的膜基结合强度降低,镀层硬度随温度的升高先增加后降低,退火温度为500℃时,镀层显微硬度最大;随退火温度的升高镀层摩擦系数呈现出先降低后升高的变化趋势,比磨损率逐渐增大.     

Effect of hydrogen content in a-C:H coatings on their tribological behaviour at room temperature up to 150 °C

Hydrogenated amorphous carbon (a-C:H) coatings deposited onto steel substrates by plasma assisted CVD, using different precursor gases (1 < H/C ratio < 4) were tested for their tribological behaviour. The H content in these coatings ranged from 25 to 29 at.%. Fretting mode I tests were performed on different couples consisting of coated and/or uncoated first bodies. Some tests were performed after a heat treatment of the coatings. As-deposited a-C:H/corundum couples tested at 23 °C and 50% RH showed lowering of the coefficient of friction at increasing normal load. Graphitisation is taking place in sliding contacts at high normal loads. For a-C:H/corundum couples a clear minimum in the coefficient of friction was noticed at 100 °C for coatings containing 27 at.% H. The coefficient of friction recorded on such couples is high compared to the one recorded on as-deposited a-C:H/a-C:H couples. However for the a-C:H/a-C:H couple, a lowering of the coefficient of friction with increasing fretting test temperature was noticed. The decreasing coefficient of friction was accompanied by an increasing wear. Graphitisation is causing severe degradation of a-C:H coatings at high test temperatures. An energetic analysis of the wear is finally reported. It appeared that the wear volume recorded at RT on as-deposited a-C:H coatings varies linearly with the cumulative dissipated energy. The wear rate coefficient decreases with increasing H-content. A stabilization of the sp³ bonds with increasing H-content might explain this behaviour. Confirmation was found by performing high temperature fretting tests. Interesting is the finding that fretting tests at RT performed after a thermal treatment of a-C:H coatings at either 100 or 150 °C, show a friction and wear behaviour identical to the ones recorded on as-deposited coatings tested at RT.     

V-Al-C-N宽温域涂层的制备及其摩擦学行为

目的 设计制备用于高速切削难加工材料的长寿命刀具涂层.方法 采用三靶磁控共溅射技术,通过改变石墨靶材的溅射功率,调控不同润滑相的配比,制备具有不同C含量的V-Al-C-N纳米复合涂层.利用纳米压痕仪和高温摩擦试验机,对涂层的力学性能和摩擦学性能进行检测.采用透射电镜和扫描电镜观察涂层的显微结构和摩擦磨损表面形貌,并分析...     

Effect of Particle Size on Wear of Particulate Reinforced Aluminum Alloy Composites at Elevated Temperatures

The present paper describes the effect of particle size on operative wear mechanism in particle reinforced aluminum alloy composites at elevated temperatures. Two composites containing zircon sand particles of 20-32 μm and 106-125 μm were fabricated by stir casting process. The dry sliding wear tests of the developed composites were performed at low and high loads with variation in temperatures from 50 to 300 °C. The transition in wear mode from mild-to-severe was observed with variation in temperature and load. The wear at 200 °C presented entirely different wear behavior from the one at 250 °C. The wear rate of fine size reinforced composite at 200 °C at higher load was substantially lower than that of coarse size reinforced composite. Examination of wear tracks and debris revealed that delamination occurs after run in wear mode followed by formation of smaller size wear debris, transfer of materials from the counter surfaces and mixing of these materials on the contact surfaces. The volume loss was observed to increase with increase in load and temperature. Composite containing bigger size particles exhibit higher loss under similar conditions.     

Effect of Microstructure on Wear Behavior of Iron Aluminide Based Coatings

MORE ATTENTIONS have been paid to ironaluminide intermetallics(including FesAl and FeAl)since1970s in view of the combination of low cost,lower density,remarkable resistance to erosion,sulfidizing and oxidizing at high temperature.However,industrial application of these alloys has been verylimited due to their poor ductility and fracturetoughness at room temperature as well as difficulty toshaping[1J.The feasibility to produce Fe-Al basedcoatings by using high velocity arc spraying(HV…     

等离子喷涂NiCrAlY-Cu涂层中Cu在宽温域环境下的扩散及摩擦耗散机制

含软金属自适应涂层在摩擦过程因软金属独特的性能而具备良好的摩擦学性能,然而在不断摩擦过程中软金属会发生一定的耗散导致涂层失效。为了研究软金属润滑剂在宽温域摩擦过程中的耗散机制,利用等离子喷涂技术制备NiCrAlY-Cu涂层;通过分析热处理及宽温域摩擦前后涂层的组分与形貌演变,揭示NiCrAlY-Cu涂层中Cu的高温扩散及宽温域摩擦耗散机制。结果表明：Cu以片层状分布在NiCrAlY基础相中,软金属Cu在温度单因素影响下垂直向涂层表面扩散,随着温度的升高扩散加剧。在1000℃环境下Cu在涂层内部发生平行扩散,并最终呈现弥散态分布。在中低温环境下随着温度的升高Cu的剪切强度降低进而使得涂层摩擦因数逐渐下降,但是由于Cu呈片层状分布,随着温度的升高涂层发生疲劳剥落导致磨损率升高。随着温度的进一步升高,Cu扩散加剧,片层状Cu减少,同时发生氧化,使得摩擦因数升高,磨损率降低。在宽温域摩擦过程中由于温度和载荷的共同影响,Cu在涂层中的摩擦耗散机制为Cu垂直向涂层表面扩散,由磨痕区域内向磨痕外平行扩散。同时,磨痕内聚集的Cu以磨屑形式逐渐损耗。提出在不同温域摩擦过程中受力-热耦合影响的软金属耗散机...