铝合金表面等离子喷涂Al2O3-3%TiO2复合涂层工艺参数优化的研究

目的 通过优化等离子喷涂工艺参数，提高铝合金表面等离子喷涂Al2O3-3%TiO2复合陶瓷涂层的结合强度和涂层表截面硬度。方法 用正交试验法，对影响喷涂涂层结合强度和硬度的4个关键喷涂参数进行优化，分别得到喷涂粘结底层Ni-5Al和工作表层Al2O3-3%TiO2的最佳优化参数。结果 通过正交试验确定影响Ni-5Al涂层综合指标的因素由主到次是喷涂电流、喷涂距离、辅气流量、主气流量，最优水平数为2、3、2、1；影响Al2O3-3%TiO2涂层综合指标的因素由主到次是喷距、辅气流量、电流、主气流量，最优水平数为2、3、2、1。Ni-5Al涂层的最佳喷涂工艺参数为：喷涂距离120 mm，喷涂电流520 A，主气流量42 L/min，辅气流量7.5 L/min。Al2O3-3%TiO2复合涂层最佳喷涂工艺参数为：喷涂距离90 mm，喷涂电流530 A，主气流量46 L/min，辅气流量7.8 L/min。最佳工艺下制备的Ni-5Al底层与基体的结合强度为25.2 MPa，Al2O3-3%TiO2复合涂层与Ni-5Al底层的结合强度为17.8 MPa，且其截面硬度在1000HV0.5以上。结论 对喷涂工艺参数进行优化可以得到质量高且稳定的Al2O3-3%TiO2复合喷涂涂层，与非最佳工艺参数喷涂涂层相比，各指标均有较大提高。     

等离子喷涂Cr2O3-8％TiO2涂层参数优化研究

等离子喷涂陶瓷涂层与基体的结合强度往往较小,限制了其实际应用,为了提高结合强度,用正交试验方法研究了等离子喷涂工艺的4个主要参数(喷涂距离、电流、主气流量和辅气流量)对Cr2O3-8%TiO2涂层结合强度的影响,确定了优化工艺并进行了验证试验,比较了工艺优化前后涂层的结合强度、孔隙率和显微硬度.结果表明:影响涂层结合强度的因素主次顺序是喷涂距离、电流、辅气流量、主气流量,工艺优化后能显著提高Cr2O3-8%TiO2涂层的性能,优化工艺喷涂的 Cr2O3-8%TiO2涂层结合强度达到29.2MPa,孔隙率为3.80%,显微硬度为2 528HV.     

基于遗传神经网络的等离子喷涂纳米ZrO2-7%Y2O3涂层工艺参数优化

将BP神经网络和遗传算法相结合用于等离子喷涂纳米ZrO2-7％ Y2O3涂层的工艺参数优化,根据正交试验结果对模型结构进行训练,建立了喷涂距离、喷涂电流、主气压力、辅气压力与涂层结合强度和显微硬度之间的BP神经网络模型,并基于遗传算法对涂层结合强度和显微硬度进行了单目标和多目标参数优化.结果表明,模型预测值与试验值十分接近,说明该网络模型是正确和可靠的.遗传算法优化的涂层最大结合强度和显微硬度(HV)分别为44.0 MPa和12.663 GPa;当涂层结合强度和显微硬度两个性能参数权重相同时,在喷涂距离90.66 mm、喷涂电流934.63 A、主气压力0.304MPa和辅气压力0.898 MPa时涂层综合性能最优.     

等离子喷涂Cr2 03 -8% Ti02涂层参数优化研究

等离子喷涂陶瓷涂层与基体的结合强度往往较小,限制了其实际应用,为了提高结合强度,用正交试验方法研究了等离子喷涂工艺的4个主要参数（喷涂距离、电流、主气流量和辅气流量）对Cr2 03 -8% TiO2涂层结合强度的影响,确定了优化工艺并进行了验证试验,比较了工艺优化前后涂层的结合强度、孔隙率和显微硬度。结果表明：影响涂层结合强度的因素主次顺序是喷涂距离、电流、辅气流量、主气流量,工艺优化后能显著提高Cr2 03一8 % TiO2涂层的性能,优化工艺喷涂的Cr2 03 -8% Ti02涂层结合强度达到29. 2MPa,孔隙率为3.80%,显微硬度为2 528HV。     

喷涂工艺参数对硅灰石涂层结构的影响

采用等离子喷涂方法,在不同喷涂距离、主气流量和喷涂功率下制备硅灰石涂层.使用扫描电镜观察了涂层的微观形貌,研究了喷涂工艺参数对涂层结构的影响.结果表明,在较大主气流量下,随着喷涂距离增加,涂层粒子扁平化程度降低,涂层内孔隙逐渐增多;在较小主气流量下,涂层粒子扁平化程度随喷涂距离增加呈现先增加后减小的趋势.主气流量增加,涂层致密,粒子扁平充分.喷涂功率增加,粒子熔化好,涂层致密;但随喷涂功率进一步增加,涂层中出现较多的圆形孔隙.喷涂工艺参数对涂层结构的影响主要通过影响熔融粒子的温度和速度所致.     

等离子喷涂AlSi-ployester封严涂层工艺优化研究

采用AlSi-ployester粉末和PARXAIR-3710等离子喷涂系统制备封严涂层.为使AlSi-ployester等离子喷涂涂层获得优良的涂层性能,选择涂层结合强度为判据,通过正交试验对AlSi-ployester等离子喷涂工艺进行了优化.利用扫描电镜,Axio lmager.A lm金相图像分析系统等手段对涂层形貌和孔隙率进行分析,同时对涂层的硬度、抗热震性能进行了测试.确定优化后的工艺参数为:电弧电流790A.主气流量62.7 L/min,辅气流量5 L/min,喷涂距离100mm.结果表明,电弧电流、主气流量、辅气流量、喷涂距离对AlSi-ployester涂层结合强度具有不同的影响,在优化的喷涂工艺参数条件下,AlSi-ployester涂层结合强度可达6.9MPa,具有较好的硬度和热震性能,可为今后等离子喷涂系统工艺参数的选定提供参考.     

球扁钢用铸铁轧辊表面等离子喷涂Cr3C2-25NiCr涂层工艺优化

以球扁钢轧制用铸铁轧辊的表面强化为目的,对等离子喷涂Cr3C2-25NiCr涂层工艺进行了研究.结果表明,影响涂层强度的因素依次为功率、喷涂距离、主气流量和送粉速率,Cr3C2-25NiCr涂层最佳工艺参数是喷涂距离130 mm,主气流量69.8 L/min-1,送粉速率25 g/min,功率20 kW.采用优化后的等离子喷涂工艺制备的涂层,呈典型的层状结构,粒子熔化充分,组织致密,孔隙率低,与基体结合较紧密.     

等离子喷涂NiCrAl涂层工艺优化研究

采用Metcod43NS(成分NiCrAl)粉末和PARXAIR-5710等离子喷涂系统制备NiCrAl涂层,为了使Ni-CrAl等离子喷涂涂层获得优良的涂层性能,选择涂层结合强度为判据,通过正交试验对NiCrAl等离子喷涂工艺进行了优化。利用扫描电镜,Axio Imager.A 1 m金相图像分析系统等手段对涂层界面形貌和孔隙率进行分析,同时对涂层的结合强度以及显微硬度进行测试。确定优化后的喷涂工艺参数为:喷涂电流为700 A,喷涂距离140 mm,主气流量56.6 L/min,辅气流量28.3 L/min。研究结果表明,喷涂电流、喷涂距离、主气流量、辅气流量对NiCrAl涂层结合强度具有不同的影响,在优化的喷涂工艺参数条件下,NiCrAl涂层结合强度为59.23 MPa,显微硬度为268HV,孔隙率为4.97%。     

等离子喷涂纳米结构ZrO2陶瓷涂层的工艺研究

研究工艺参数对等离子喷涂纳米结构ZrO2陶瓷涂层微观组织和力学性能的影响,采用三因素三水平正交试验法对喷涂电压、电流和主气流速三个主要参数进行了优化设计.采用定量金相分析法分析了涂层未熔化区域的大小,并测定了涂层的结合强度、裂纹扩展抗力和磨损性能.结果表明,制备纳米结构ZrO2陶瓷涂层的最佳工艺参数为电流540A,电流63V,主气流量45 L/min.     

等离子喷涂工艺参数对粒子速度和温度的影响

在G型喷嘴下，利用SprayWatch-2i喷涂粒子速度、温度测试仪在线测量粒子的飞行参数，研究了等离子喷涂工艺参数对喷涂粒子速度和温度的影响，并对等离子喷涂氧化锆粉末的主要工艺参数进行优化分析。在诸因素中．气体流量对粒子速度和温度的影响最为显著，随着主气流量的增加，粒子速度有所增加。     

Cold-Sprayed Magnesium Coatings Deposited with Helium and Air

Cold-sprayed magnesium coatings have been little researched although cold spraying has been applied to deposit a large number of materials such as metals,metal matrix composites.In the present study,helium gas and air were employed as the propelling gases to deposit Mg coatings under the temperature of 600℃and 630℃.The effect of gas types on the coating microstructure was investigated.It is much interesting to find that the particle deposition efficiency using helium gas as propelling gas is lower than that using air.This suggests that strong erosion occurred during cold spraying using helium gas.The porosity of the coating using helium gas is lower than that using air.In addition,the in-flight particle velocity was also simulated by the FLUENT software to explore the effect of gas types.The modeled results show that the in-flight particle velocity using helium is higher than the erosion velocity of Mg particle.     

微束等离子喷涂NiCrBSi涂层

采用微束等离子喷涂方法在St37低碳钢上制备了NiCrBSi涂层.研究了基材温度、等离子气体流量、喷涂距离和电流强度等工艺参数对涂层组织结构和性能的影响.采用光学显微镜观察涂层的组织结构,用Perthometers M4P 150测定涂层的表面粗糙度,以及用LECO TC316气体抽提仪检测涂层的氧含量.结果表明,在试验条件下,喷涂参数对涂层组织和性能产生较大的影响.随着电流和基材温度的增加涂层的粗糙度降低,涂层的氧含量随着基材温度和喷涂距离的增加而增加.大多数涂层的显微硬度大于600 HV0.2.尽管粒子速度较低,涂层的平均结合强度仍然大于50 MPa.     

前驱体溶液等离子喷涂参数对涂层形貌的影响及沉积行为机理研究

目的对不同喷涂工艺参数下涂层的相结构、显微形貌进行研究,确定优化的喷涂工艺参数,讨论分析涂层的沉积行为机理。方法采用前驱体溶液等离子喷涂(SPPS)的方法制备纳米Yb_2O_3稳定的ZrO_2(YbSZ)涂层。在传统等离子喷涂的基础上,增加液料雾化装置,雾化喷嘴将溶液雾化后直接注入到等离子弧中,通过控制喷涂距离及喷涂功率,研究了涂层相结构、结晶度、晶粒尺寸以及显微形貌的变化趋势,并且结合显微形貌讨论了沉积机理。结果涂层呈现团聚大颗粒、纳米级粒子、大小均匀的孔隙三种显微形貌,大颗粒之间呈堆积形态。当喷涂功率为30 kW时,涂层呈现m-ZrO_2,平均晶粒尺寸达669 nm。随着喷涂距离、喷涂功率的增加,样品中检测到单一的t-ZrO_2相,而且纳米尺寸颗粒的数量大大增加,孔径变小。随着喷涂距离由60 mm增加到100 mm,平均晶粒尺寸先由429 nm减小到177 nm,随后又增加到319 nm。结论喷涂参数影响晶粒的结晶度、晶粒尺寸以及涂层的显微形貌,低功率下得到的涂层存在糊状未结晶组织。增大喷涂功率,可以有效增大结晶度和晶粒尺寸;随着喷涂距离的增大,晶粒尺寸先减小后增大。雾化液滴在等离子火焰中一般要经历浓缩、饱和、固化、析晶形核长大、粒子重熔扁平化的历程,喷涂功率越高,经历温区越高,液滴演变就越充分,通过优化工艺参数可以得到不同结构性能的功能涂层。     

等离子喷涂TiO2基涂层工艺参数优化研究

目的对TiO_2基涂层的等离子喷涂工艺参数进行优化。方法采用正交实验、基材温度采集并结合涂层微观形貌分析、能谱分析、结合强度试验、显微硬度测试等方法,研究了喷涂电流、喷涂距离、主气流量对涂层组织及性能的影响规律,并获得了优化的喷涂工艺参数。结果涂层分熔融区和部分熔融区,呈现双模结构的混合微观结构特征,截面形貌凹凸不平,并以机械结合为主。拉断后,涂层断裂面呈韧窝状,由陶瓷层到粘结层呈台阶状过渡,陶瓷层整体的内聚结合强度优于陶瓷层与粘结层结合界面的结合强度。涂层条带状夹杂随着粉末流到达基板的温度的增加而减少,对结合强度影响不显著,但对硬度影响较显著。等离子喷涂过程中,粉末流到达基板的温度在一定范围内时,涂层性能随着粉末流到达基板的温度的增加而增加,但粉末流到达基板的温度过大,涂层性能降低。结论获得最优涂层必须采用最优工艺参数,工艺参数对涂层综合性能的影响主次顺序为喷涂电流、喷涂距离、主气流量,得到的优化工艺参数为:喷涂电流350 A,喷涂距离110 mm,主气流量2100 L/h。     

超音速等离子喷涂NiCr-Cr3C2工艺的参数优化

采用四因素三水平正交试验,通过在线监测喷涂粒子的温度和速度,对电流、电压、喷涂距离和主气流量四个超音速等离子喷涂的主要参数进行优化设计.结果表明:四个因素对喷涂粒子温度的影响均较大,电压和主气流量对喷涂粒子速度的影响较大;优化的工艺参数为电压150 V、电流400A、喷涂距离85 cm、氩气流量4.2m3/h,采用该优...     

Optimization of Atmospheric Plasma Spray Process Parameters using a Design of Experiment for Alloy 625 coatings

Alloy 625 is a Ni-based superalloy which is often a good solution to surface engineering problems involving high temperature corrosion, wear, and thermal degradation. Coatings of alloy 625 can be efficiently deposited by thermal spray methods such as Air Plasma Spraying. As in all thermal spray processes, the final properties of the coatings are determined by the spraying parameters. In the present study, a D-optimal experimental design was used to characterize the effects of the APS process parameters on in-flight particle temperature and velocity, and on the oxide content and porosity in the coatings. These results were used to create an empirical model to predict the optimum deposition conditions. A second set of coatings was then deposited to test the model predictions. The optimum spraying conditions produced a coating with less than 4% oxide and less than 2.5% porosity. The process parameters which exhibited the most important effects directly on the oxide content in the coating were particle size, spray distance, and Ar flow rate. The parameters with the largest effects directly on porosity were spray distance, particle size, and current. The particle size, current, and Ar flow rate have an influence on particle velocity and temperature but spray distance did not have a significant effect on either of those characteristics. Thus, knowledge of the in-flight particle characteristics alone was not sufficient to control the final microstructure. The oxidation index and the melting index incorporate all the parameters that were found to be significant in the statistical analyses and correlate well with the measured oxide content and porosity in the coatings.

Influence of Helium and Nitrogen Gases on the Properties of Cold Gas Dynamic Sprayed Pure Titanium Coatings

This study investigates the effect of propellant gas, helium, and nitrogen during cold spraying of titanium coatings. Coatings were characterized by SEM and were evaluated for their deposition efficiency (DE), microhardness, and porosity. In selected conditions, three particle velocities were investigated in which for each condition, the propelling gases?? temperature and pressure were attuned to attain similar particle velocities for each gas. Observations show that loosely bonded particles can be detached by high-pressure supersonic gas stream. Selected coatings were characterized by XPS to analyze the occurrence of oxidation and nitridation. Although generally accepted that coating characteristics can be affected by particle temperature, results show that for the same particle velocity, DE and coating density are also a function of substrate temperature. In addition, a thick and fully dense cold sprayed titanium coating was achieved with optimized spray parameters and nozzle using helium. The corresponding average particle velocity was 1173 m/s.     

Effect of in-flight particle velocity on the performance of plasma-sprayed YSZ electrolyte coating for solid oxide fuel cells

In this paper, the effect of particle velocity on the characteristics of atmospheric plasma-sprayed yttria stabilized zirconia was investigated through adjusting auxiliary helium flow rate. The temperature and velocity of in-flight particles were measured with the DPV2000 diagnostic system. The results showed that helium flow rate significantly influenced particle velocity and less distinctly influenced particle temperature. The microstructure of the coatings was characterized by scanning electron microscopy and X-ray diffraction analyzer. The ionic conductivity of the deposits through thickness direction was measured by a potentiostat/galvanostat based on three-electrode assembly approach in a temperature range of 500-1000 °C. The specific gas permeability was estimated through measuring the coating gas flow rate with a home-made experimental setup. The results showed that the gas permeability was improved by increasing the in-flight particle velocity. However, the in-flight particle velocity had little effect on the ionic conductivity of specimens.     

喷涂距离对等离子喷涂WC-12Co涂层抗冲蚀磨损性能的影响

为提高WC-12Co涂层抗冲蚀磨损性能,在Q235钢基体上采用大气等离子喷涂(APS)方法制备WC-12Co涂层,研究了喷涂距离对粒子温度与速度、涂层组织结构、力学性能及抗冲蚀磨损性能的影响。结果表明:喷涂距离对涂层质量影响较为明显,喷涂距离为130 mm时涂层质量较好,粒子速度与温度达到较好的配合,涂层抗冲蚀磨损能力较强。喷涂距离为120 mm与140 mm时涂层抗冲蚀磨损能力较差。550μm(30目)沙粒直径对涂层冲蚀磨损量大,沙粒速度为15.68 m/s比13.33 m/s沙粒速度冲蚀磨损量大;冲蚀角为60°时冲蚀磨损量最大,30°冲蚀磨损量最小。