N2流量比对AlCrMoSiN涂层组织结构和性能的影响

目的 减少硬质合金刀具在干式切削时产生的切削热,降低切削温度,从而提高刀具使用寿命。向AlCrSiN涂层中掺杂Mo元素,在涂层服役过程中易生成层状MoO_(3)润滑膜,降低刀面与切屑和工件间的摩擦,实现涂层刀具的自润滑功能。方法 利用高功率脉冲磁控溅射和脉冲直流磁控溅射复合技术制备AlCrMoSiN涂层,改变反应气体N_(2)流量,调节涂层的成分和结构。采用X射线衍射仪、扫描电子显微镜分析AlCrMoSiN涂层的物相成分和微观结构,利用纳米压痕仪、划痕仪和摩擦试验机分别测试涂层的力学性能和摩擦学行为。结果 当N_(2)流量比增大,AlCrMoSiN涂层沿(111)晶面择优生长,衍射峰变得尖锐,(111)和(200)晶面衍射峰向小角度偏移。当N_(2)流量比为16%时,涂层的硬度和弹性模量最大,分别为17.56 GPa和292.31 GPa。当N_(2)流量比为18%时,涂层的临界载荷最高,约为70.6 N,摩擦系数最低达0.54,磨损率为1.3×10^(–3)μm^(3)/(N·μm),此时涂层最耐磨。结论 N_(2)流量比对涂层组织结构有重要影响,随着N_(2)流量比增大,涂层的力学性能与摩擦磨损性能逐渐改善。     

轻质Cf/SiOC复合材料表面抗氧化涂层烧蚀性能的研究

目的提高轻质碳纤维增强SiOC(C_f/SiOC)多孔陶瓷复合材料的抗烧蚀性能。方法用TaSi_2、MoSi_2为高温抗氧化组分,SiB_6为烧结助剂,硼硅酸玻璃为粘结剂,采用浆料法在C_f/SiOC复合材料表面制备多层梯度化抗氧化涂层。用氧乙炔考核带涂层复合材料的抗氧化及抗烧蚀性能,并通过扫描电子显微镜对烧蚀后的形貌进行分析。结果采用硼硅酸玻璃能够在较低的温度下获得表面致密的涂层,有效地提升涂层的阻氧能力,同时能够降低涂层与基体材料之间的热失配。通过浆料法能够获得梯度化的抗氧化涂层,即涂层由靠近基体部分的多孔层逐渐过渡至最外层的致密层。在氧乙炔考核烧蚀实验下,涂层表现出优良的抗烧蚀性能,并且随着表面烧蚀温度的不同,表现出不同的烧蚀行为。在1660℃下烧蚀后,线烧蚀率及质量烧蚀率分别为0.03μm/s,2.96×10-8g/(mm2·s),随着烧蚀温度增加至1760℃,线烧蚀率及质量烧蚀率增加至0.06μm/s,1.03×10-7g/(mm2·s)。带涂层的复合材料烧蚀后,涂层表面没有裂纹,但都出现了大量的孔洞,其主要原因是硼硅酸玻璃的挥发,基体材料并没有发生明显的氧化,涂层表现出优良的抗氧化、阻氧能力。结论硼硅酸玻璃的引入能够在较低的温度下获得表面致密的涂层,提升涂层的阻氧能力。制备的多组分抗氧化烧蚀涂层,可以有效地提高C_f/SiOC复合材料的抗烧蚀能力。     

温度与循环热冲击对聚酰亚胺涂层耐蚀性影响

目的研究聚酰亚胺涂层对N80钢的防腐性能和耐热冲击性能。方法采用静电粉末喷涂在N80钢表面获得一种聚酰亚胺防腐涂层,通过高温浸泡实验评价涂层在不同温度下、不同腐蚀介质中的耐蚀性能,通过循环热冲击实验评价涂层的耐热冲击性能,通过扫描电子显微镜(SEM)观察实验前后涂层的表面微观形貌。结果热重分析(TGA)表明,聚酰亚胺涂层的热分解温度(t_(d5))为518℃。电化学交流阻抗测试结果和SEM形貌观测表明,腐蚀介质温度越高,耐蚀性能下降越快,涂层在3.5%Na Cl溶液的耐蚀性能比在25%HCl溶液中更好。涂层在经过不同温度的循环热冲击之后,表面无破损。结论聚酰亚胺涂层具有优异的耐热冲击性能,温度和腐蚀介质对涂层的耐蚀性能有重要影响。     

静电除尘器极板涂敷导电防腐涂料对静电除尘性能影响的研究

为了改善静电除尘器极板防腐性能、增加极板的抗污性能和提高极板清灰效果,用导电防腐涂料涂敷电除尘器极板.提出了涂层比电阻特性数学模型并用实验加以验证.推导了极板沉积粉尘层积累电荷量公式,表明电荷量多少与粉尘层放电时间常数成正比.理论研究结果表明,涂加涂层后,极板上低比电阻粉尘层放电时间常数增大,粉尘层积累电荷量增多,粉尘层与极板问静电附着力增大,有效减弱了粉尘的二次飞扬现象;通过降低涂层的比电阻和涂层厚度,使中高比电阻粉尘层的积累电荷量增加不大.实验测试了涂层对不同比电阻粉尘收尘效率的影响及涂层对极板粉尘剥离率的改善.实验结果显示,涂加涂层后,低比电阻粉尘的收集效率有显著提高,中高比电阻粉尘的收集效率变化不大;极板粉尘剥离率较不加涂层时有很大提高.极板涂敷技术有效延长了极板的使用寿命,在保证除尘效率的前提下提高了极板的清灰效果,是电除尘领域中的一项创新.     

飞机结构表面涂层体系改进研究

针对多型飞机表面涂层体系抗腐蚀性能差这一亟待解决的问题,采用制造状态、大修状态及纳米复合涂层对设计的典型飞机蒙皮对接结构模拟件进行涂装,并利用划格法对涂层体系的层间附着力进行表征。采用加速模拟环境试验的方法,对纳米复合涂层的防腐性能进行考核验证。试验结果表明,纳米复合涂层体系的层间附着力、防腐性能和耐老化性能明显优于制造状态、大修状态涂层体系,在飞机中应用纳米复合涂层可以显著改善结构的抗腐蚀品质。     

物理气相沉积硬质耐腐蚀磨损防护涂层研究进展

叙述了用物理气相沉积技术制备的硬质耐腐蚀磨损防护涂层的研究进展。重点介绍了腐蚀磨损耦合工况特性和作用机理,单元、多元掺杂氮化物涂层,高熵氮化物涂层,多层、纳米多层、纳米复合、梯度氮化物涂层耐腐蚀磨损性能研究,非金属元素/金属元素掺杂DLC涂层、多层复合DLC涂层耐腐蚀磨损性能研究,并对涂层改性、强化机理和腐蚀磨损失效机制进行了总结。最后,提出了未来物理气相沉积硬质耐腐蚀磨损防护涂层重点发展的方向,应重点发展涂层组元/结构设计、力–电耦合损伤机理研究、高效率研发设计、涂层先进制备装备与评估体系等方面的能力。     

采用Pt、Dy改性粘结层的铈酸镧/氧化锆双陶瓷层抗氧化行为研究

目的研究Pt、Dy改性粘结层的铈酸镧/氧化锆双陶瓷层的抗氧化行为。方法采用电镀+EB-PVD的方式在高温合金表面制备带有Pt、Dy掺杂NiAl粘结层的热障涂层(Thermal Barrier Coatings TBCs)。采用双陶瓷层结构设计,顶层为铈酸镧(La_2Ce_2O_7),底层为氧化锆(YSZ)。对涂层在1200℃条件下的热循环行为、微观组织以及失效机制进行了研究。结果经过500次循环后,不掺杂涂层YSZ层与热生长氧化物(TGO)处出现了大量裂纹,Pt/Dy共掺杂的涂层经过1000次循环后界面处结合良好,仅仅是在La_2Ce_2O_7陶瓷顶层中出现了少量的微裂纹。结论在粘结层中加入Pt元素,能有效抑制互扩散区难溶相的析出,延缓涂层的蜕化。     

高强度合金结构钢与高强度铝合金防护层的耐霉性研究

目的研究高强合金结构钢和高强铝合金防护层的耐霉菌腐蚀能力。方法以高强合金结构钢和高强铝合金两种材料为基材分别制备不同防护层,按GJB 150.10A—2009进行实验室霉菌试验,评定防护层的长霉等级。结果两种材料的不同防护层中,除润滑油涂层和阳级氧化层的长霉等级为0~1级外,炮油涂层、涂漆层、镀锌层或锌镍合金层长霉等级均在2~3级。结论高强合金结构钢润滑油涂层耐霉性能良好,镀锌层或锌镍合金层、涂漆层、炮油涂层耐霉性能较差;高强铝合金阳级氧化层耐霉性能良好,炮油涂层、涂漆层耐霉性能较差。     

镍铁合金/铁包云母粉复合吸波涂层材料的频散特性

目的探究不同质量分数配比的镍铁合金/铁包云母粉复合吸波涂层材料的频散特性。方法利用扫描电镜(SEM)观察镍铁合金和铁包云母粉的微观形貌,并使用仪器附带的能谱分析仪对样品所选区域的各元素含量进行测量。用矢量网络分析仪研究了不同质量分数下的镍铁合金/石蜡、铁包云母粉/石蜡同轴样品的介电常数与磁导率。用弓形法测试在2~18 GHz频段内镍铁合金和铁包云母粉以不同质量比加入环氧树脂-聚酰胺体系中制备的不同厚度的单层吸波涂层的反射损耗。结果镍铁合金频散特性较好,对电磁波损耗较大,将其作为吸波涂层的填料,减少吸收剂的用量同时降低了涂层的厚度。铁包云母粉的介电常数的实部较低,与自由空间的阻抗匹配较好,拓宽了吸波频带。镍铁合金和铁包云母粉作为填料,以质量分数30%/30%制备厚度1.2 mm的单层吸波涂层,在2~18 GHz其最小反射值达到了-21.8 d B,小于-10 d B的带宽达到10.5 GHz。结论镍铁合金与铁包云母粉以合适质量比复合,制备的吸波涂层材料厚度薄、吸波频带宽。     

Al2O3/Ni-P-SiC复合涂层组织与性能的研究

目的 采用化学复合镀技术对微弧氧化进行封孔,进而得到抗烧蚀性能优良的Al2O3/Ni-P-SiC复合涂层。方法 通过采用扫描电镜(SEM)、光学金相显微镜(OM)、显微硬度仪(Microhardness Tester)、X射线衍射仪(XRD)、氧–乙炔烧蚀试验(Oxy-Acetylene Ablation Test)等方法,对复合涂层的表面形貌、截面形貌、厚度、显微硬度、物相和抗烧蚀性能等进行分析。结果 陶瓷层原始表面完全被化学镀层覆盖,所制得的复合涂层厚度均匀,化学镀层与陶瓷层紧密嵌合。镀液中的SiC浓度对镀覆的速度、镀层中SiC粒子的共沉积量有着较大的影响。当粒子质量浓度为16~20 g/L时,颗粒的共沉积量较大。化学复合镀60 min可以得到厚度20 μm左右的Ni-P-SiC镀层,SiC颗粒分布均匀。当镀液中SiC质量浓度为16 g/L时,镀层具有最高的硬度。对比未处理、仅微弧氧化和Al2O3/Ni-P-SiC复合涂层试样,Al2O3/Ni-P-SiC复合涂层试样具有最佳的抗烧蚀性能。结论 Al2O3/Ni-P-SiC复合涂层均匀、致密,具有良好的抗烧蚀。     

Tool wear of coated drills in drilling CFRP

This study aimed to investigate the wear of certain coated drills when drilling carbon fiber reinforced composites (CFRP). Three different drills were used in the drilling experiments: uncoated, diamond coated and AlTiN coated carbide (WC–Co) drills. The tool wear in CFRP machining was quite different from that in conventional metal machining. The primary wear type was a dulling or blunting of the cutting edge, which has been referred to as edge rounding wear or edge recession. In this paper, a hypothesis has been developed to explain the edge rounding wear in CFRP machining. Due to the fracture-based chip formation of CFRP, there is lack of the work material stagnation zone in front of the cutting edge, which normally prevents the edge wear in metal machining. Series of wear lead to rapid dulling of the cutting edge. The resistance to edge rounding wear on the coated as well as uncoated drills has been investigated. The diamond coating significantly reduces the edge rounding wear. However, AlTiN coated drills showed no visible improvement over the uncoated carbide drill, despite of their high hardness, thus not protecting the drill. The wear mechanisms of the uncoated carbide drill and coatings are discussed. It is believed that the 2-body and 3-body abrasive wear fail to explain the observed tool wear in CFRP drilling. However, the wear of the coatings and uncoated carbide substrate from tribo-meter tests correlated well with the tool wear in the CFRP drilling. Therefore, the tribo-meter test can be used to screen the prospective tool materials before carrying drilling experiment.     

An Approach to Theoretical Modeling and Simulation of Face Milling Forces

A new approach to theoretical modeling and simulation of face milling forces is presented. The present approach is based on a predictive machining theory in which machining characteristic factors in continuous cutting with a single-point cutting tool can be predicted from the workpiece material properties, tool geometry, and cutting conditions. The action of a milling cutter is considered as the simultaneous work of a number of single-point cutting tools, and the milling forces are predicted from input data of workpiece material properties, cutter parameters and tooth geometry, cutting condition, cutter and workpiece vibration structure parameters, and types of milling. A predictive force model for face milling is developed using this approach. In the model, the workpiece material properties are considered as functions of strain, strain rate, and temperature. The ratio of cutter tooth engagement over milling is taken into account for the determination of temperature in the cutting region. Cutter runout is included in the modeling for the chip load. The relative displacement between the cutter and workpiece due to the cutter and workpiece vibration is also included in the modeling to consider the effect on the undeformed chip thickness. A milling force simulation system has been developed using the model, and face milling experimental tests have been conducted to verify the simulation system. It is shown that the simulation results agree well with experimental results.     

Process capability study of laser assisted micro milling of a hard-to-machine material

Laser assisted micro milling (LAMM) is capable of generating three-dimensional micro scale features in hard-to-machine materials. This paper compares the process capability of LAMM with conventional micro milling of a hardened tool steel. In particular, the potential advantages of LAMM over micro milling with respect to cutting forces, tool wear, material removal rate, burr formation and surface roughness are investigated when micro milling hardened A2 tool steel (62 HRC). The results show that LAMM has significant advantages over micro milling, especially in terms of cutting forces, material removal rate and tool wear. The average reduction in the resultant cutting force is found to be up to 69% with laser assist. In addition, tool wear is found to be substantially less with laser assist even when the material removal rates are increased by a factor of six over the tool manufacturer recommended cutting conditions.     

Crater Wear Evolution in Multilayer Coated Carbides During Machining Using Confocal Microscopy

Steady-state turning experiments were carried out with multilayer coated inserts consisting of TiN/Al₂O₃/TiCN deposited on a carbide substrate. Confocal microscopy was used for the first time to observe the topography of crater wear evolution in multilayer coated inserts. A hump made of TiN coating next to a growing crater of Al₂O₃, traces of attached steel, and the maximum depth regions have been identified. Scoring marks were also detected in the TiN layer, indicating the presence of abrasion wear. Interestingly, the crater depth was stagnant once it reached the Al₂O₃ layer, and the wear progresses by broadening the area of exposed Al₂O₃. It was concluded that the effectiveness of multilayer coated tools comes from the dissolution resistance of the Al₂O₃ layer, which delays depth growth and develops the wear front into a wider area. Confocal microsocopy was found to be a valuable tool to obtain wear topography for multilayer coated tools.     

大气等离子和超音速火焰喷涂CoCrAlYSi-hBN涂层组织和性能对比

目的 针对航空发动机叶片榫头/榫槽摩擦副工作中的微动磨损问题,开展CoCrAlYSi-hBN抗微动磨损涂层研究.方法 通过大气等离子(APS)和超音速火焰(HVOF)喷涂工艺,制备CoCrAlYSi-hBN涂层,采用扫描电镜(SEM)研究涂层的形貌和微观组织,采用显微硬度计和拉伸试验机测试涂层的显微硬度和结合强度,采用SRV试验机探究涂层的摩擦磨损性能.结果 APS喷涂CoCrAlYSi-hBN涂层熔化更充分,显微组织均匀,具有更多高含量的hBN和孔隙;HVOF喷涂CoCrAlYSi-hBN涂层显微组织具有明显的层状结构,涂层致密,hBN和孔隙含量少;APS喷涂CoCrAlYSi-hBN涂层的硬度平均值为168.4HV0.3,结合强度平均值为44.6 MPa,远小于HVOF喷涂CoCrAlYSi-hBN涂层的硬度(327.1HV0.3)和结合强度平均值(59.5 MPa).相比HVOF喷涂CoCrAlYSi-hBN涂层,APS喷涂CoCrAlYSi-hBN涂层虽然有更低的摩擦系数(0.75),但涂层磨损更严重,涂层磨痕表面有明显的涂层剥落,HVOF喷涂CoCrAlYSi-hBN涂层磨痕则出现更多的犁沟.结论 HVOF喷涂工艺制备的CoCrAlYSi-hBN涂层的综合性能优于APS喷涂CoCrAlYSi-hBN涂层,在摩擦过程中,两种工艺制备的CoCrAlYSi-hBN涂层都会转移到对偶件上,从而减少对偶件的磨损,有作为叶片榫头抗微动磨损涂层的潜力.     

高耐磨化学复合镀层的研究

为了改善化学镀Ni-P合金镀层的耐磨性能,提高化学镀Ni-P合金镀层的使用寿命,实验中分别在化学镀液中加入了硬质相SiC粒子、Al2O3粒子以及具有自润滑性能的PTFE粒子,使它们与Ni-P合金一起共沉积,从而制备出具有特殊功效的高耐磨复合镀层.实验结果表明:化学镀Ni-P-SiC以及Ni-P-Al2O3复合镀层由于硬质粒子的加入使镀层的耐磨性比Ni-P镀层提高了6倍左右;Ni-P-PTFE复合镀层的摩擦系数可达0.063,远小于Ni-P镀层0.2的摩擦系数,同时耐磨性能也比Ni-P合金镀层有了较为明显的提高.     

C/C-SiC-ZrB2复合材料表面SiC/ZrB2-SiC/SiC涂层的制备及抗氧化烧蚀性能研究

目的研究C/C-SiC-ZrB_2复合材料表面SiC/ZrB_2-SiC/SiC涂层的制备、抗氧化烧蚀性能与机理。方法选择ZrB_2和SiC改性的C/C复合材料为基体,通过包埋-刷涂法在C/C-SiC-ZrB_2复合材料表面制备了SiC/ZrB_2-SiC/SiC多重抗氧化涂层,并对复合材料的微结构、抗氧化烧蚀性能与机理进行分析和研究。结果制备了一种三层结构的SiC/ZrB_2-SiC/SiC超高温陶瓷复合涂层,获得了风洞考核试验下的复合材料微结构变化、线烧蚀率等试验数据,并得到了C/C-SiC-ZrB_2复合材料的氧化烧蚀机理。结论 SiC/ZrB_2-SiC/SiC涂层对C/C-SiC-ZrB_2复合材料的抗氧化和耐烧蚀性能具有明显提升,有效提高了C/C-SiC-ZrB_2复合材料的综合热防护性能。     

Analysis of machined surface quality in a single-pass of ball-end milling on Inconel 718

The ball-end milling process is widely used for generating three-dimensional sculptured surfaces with definite curvature. In such cases, variation of surface properties along the machined surface curvatures is not well understood. Therefore, this paper reports the effect of machining parameters on the quality of surface obtained in a single-pass of a ball-end milling cutter with varying chip cross-sectional area. This situation is analogous to generation of free form cavities, pockets, and round fillets on mould surfaces. The machined surfaces show formation of distinct bands as a function of instantaneous machining parameters along the periphery of cutting tool edge, chip compression and instantaneous shear angle. A distinct variation is also observed in the measured values of surface roughness and micro-hardness in these regions. The maximum surface roughness is observed near the tool tip region on the machined surface. The minimum surface roughness is obtained in the stable cutting zone and it increases towards the periphery of the cutter. Similar segmentation was observed on the deformed chips, which could be correlated with the width of bands on the machined surfaces. The sub-surface quality analysis in terms of micro-hardness helped define machining affected zone (MAZ). The parametric effects on the machining induced shear and residual stresses have also been evaluated.     

不同B_(4)C含量对冷喷涂Al/B_(4)C复合涂层防腐与耐磨性能的影响

目的分析不同B_(4)C含量对冷喷涂Al/B_(4)C复合涂层防腐和耐磨性能的影响,探索利用冷喷涂低温特点制备Al/B_(4)C复合涂层的可行性。方法利用冷喷涂方法制备4种B_(4)C含量的Al/B_(4)C复合涂层,并利用各种方法表征涂层的结合特征、耐磨性能和防腐性能。结果冷喷涂过程不会改变铝和碳化硼的物相,碳化硼颗粒主要以嵌入方式结合在涂层中,会产生结合缺陷。在本研究中,B_(4)C的质量分数最高可达到34.53%左右,涂层的结合强度随粉末中碳化硼含量的增加先增加、后降低,最高可达26.67 MPa。微区电化学试验分析涂层内部微电位差值,发现Al/B_(4)C界面存在电位差,腐蚀反应会优先在Al/B_(4)C界面发生,从而破坏金属Al成膜,使涂层的耐蚀性能与略低于铝块材。结论冷喷涂技术可以制备微观结构和结合性能良好的高B_(4)C含量Al/B_(4)C复合涂层,涂层中B_(4)C的质量分数最高达34.53%,预期具有良好的热中子吸收性能。同时,B_(4)C颗粒的加入,使得涂层的耐磨性能大大的提升,但是耐蚀性能相比于铝材料略有降低,是未来需要改善的方向。