精密加工表面粗糙度在线检测系统的研究

介绍一个高精度的激光光纤传感式精密加工表面粗糙度在线检测系统。系统的工作原理基于表面散射理论,综合采用了光强补偿、调制、单通道信号处理以及互补采样等一系列技术,确保了测量的高精度。系统使用了单片微机,包括信号切换、互补采样、运算处理及显示打印等测量全过程,均由单片机控制     

石墨烯/聚合物导电复合材料研究进展

石墨烯是新一代的纳米级碳材料,具有优异的机械、导电性能以及其他的功能性能,是制备聚合物导电复合材料的理想填充物.对石墨烯的常用制备方法进行比较并分析其优点与不足,介绍了石墨烯及其复合材料的导电及机械性能,并对石墨烯及其聚合物导电复合材料的应用研究进展进行了系统的综述.最后,对该领域所存在的问题进行了总结,并展望了其发展趋势.     

动力传输齿轮表面闪温的部分弹流热分析

采用部分热弹性流体动力润滑理论对非修缘直齿轮的表面闪温进行了研究。通过数值计算过程,分析了齿轮在一个啮合循环中,表面粗糙纹理、表面粗糙度等形貌参数及工况参数对轮齿表面和油膜内闪温的影响规律。本文的研究方法对齿轮胶合机理和提高齿轮胶合承载能力的研究都是有意义的。     

星用材料静电放电信号分析

地球同步轨道卫星的在轨故障分析表明,ESD(静电放电)是导致卫星故障的重要原因之一,它约占故障总数的30%左右。文章叙述了ESD 信号的定量分析方法并报导了若干星用材料的充电和放电特性,其中包括Ag-SiO_2微晶玻璃、S-853白漆、SB-3消光黑漆、阳极化铝等材料。     

碳纤维表面改性研究进展

文章阐述了碳纤维增强树脂基复合材料中界面的粘接机理 ,介绍了碳纤维的表面结构与性能 ,重点综述了常用的碳纤维表面处理方法。     

新型损伤容限钛合金高速铣削表面完整性分析(英文)

研究新型损伤容限钛合金TC21在不同的刀具磨损状态下,采用高速铣削与常规铣削的加工表面完整性,重点研究表面粗糙度、加工硬化层、金相组织等因素对表面完整性的影响。结果表明,高速铣削能够获得良好的表面质量并提高加工的效率,同时通过观察加工硬化层与金相组织可以发现,即使是刀具在严重磨损的状态下,也不会出现比较严重的加工硬化现象。     

CF/PEEK复合材料超声辅助铣削力和表面质量研究

为改善碳纤维增强聚醚醚酮复合材料（CF/PEEK）在铣削加工时所产生的毛刺、分层以及表面凹坑等缺陷，采用超声辅助铣削的加工方式分别沿0°、45°、90°、135°四种纤维方向角对CF/PEEK进行实验，并与传统铣削进行对比研究。结果表明：超声辅助铣削与传统铣削相比，切削力更小且加工质量更优。沿90°纤维方向角对试件进行超声辅助铣削，切削力、表面粗糙度和毛刺高度降幅最显著，分别降低了16.79%、28.9%和71.9%。而且在相同的加工参数下，超声辅助铣削与传统铣削相比，能够有效地改善表面凹坑、分层等表面缺陷。     

表面处理对聚酰亚胺柔性复合材料粘结性能的影响

使用聚酰亚胺(PI)膜和PI纤维编织布制备深空探测用柔性织物复合材料,研究表面处理对PI膜和PI纤维编织布之间粘结性能的影响。采用自制表面处理剂分别对PI膜和PI纤维编织布的表面进行处理,再经硅橡胶胶黏剂粘结制备柔性复合材料。使用T剥离强度试验方法测试柔性织物复合材料的层间胶接性能,并分析复合材料剥离面的形貌状态。结果显示,PI膜和PI织物的表面处理可以显著提高柔性织物复合材料的T剥离强度。其中,PI膜和PI织物未经表面处理时,柔性织物复合材料的T剥离强度为8.9 N/cm。对PI膜进行表面处理,或者对PI膜和PI织物均进行表面处理的情况下,柔性织物复合材料的T剥离强度增加至11.7 N/cm和12.8 N/cm,分别提高了31.5%和43.8%。这表明对PI膜及PI织物进行合理的表面处理,可以显著提高柔性织物复合材料的胶接性能。     

Improving profile accuracy and surface quality of blisk by electrochemical machining with a micro inter-electrode gap

Electrochemical machining (ECM) has emerged as an important option for manufacturing the blisk. The inter-electrode gap (IEG) distribution is an essential parameter for the blisk precise shaping process in ECM, as it affects the process stability, profile accuracy and surface quality. Larger IEG leads to a poor localization effect and has an adverse influence on the machining accuracy and surface quality of blisk. To achieve micro-IEG (<50 μm) blisk finishing machining, this work puts forward a novel variable-parameters blisk ECM strategy based on the synchronous coupling mode of micro-vibration amplitude and small pulse duration. The modelling and simulation of the blisk micro-IEG machining have been carried out. Exploratory experiments of variable-parameters blisk ECM were carried out. The results illustrated that the IEG width reduced with the progress of variable parameter process. The IEG width of the blade’s concave part and convex part could be successfully controlled to within 30 μm and 21 μm, respectively. The profile deviation for the blade’s concave surface and convex surface are 49 μm and 35 μm, while the surface roughness reaches R_a = 0.149 μm and R_a = 0.196 μm, respectively. The profile accuracy of the blisk leading/trailing edges was limited to within 91 μm. Compared with the currently-established process, the profile accuracy of the blade’s concave and convex profiles was improved by 50.5 % and 53.3 %, respectively. The surface quality was improved by 53.2 % and 50.9 %, respectively. Additionally, the machined surface was covered with small corrosion pits and weak attacks of the grain boundary due to selective dissolution. Some electrolytic products were dispersed on the machined surface, and their components were mainly composed of the carbide and oxide products of Ti and Nb elements. The results indicate that the variable-parameters strategy is effective for achieving a tiny IEG in blisk ECM, which can be used in engineering practice.     

Improving surface integrity when drilling CFRPs and Ti-6Al-4V using sustainable lubricated liquid carbon dioxide

In the quest for decreasing fuel consumption and resulting gas emissions in the aeronautic sector, lightweight materials such as Carbon Fiber Reinforced Polymers (CFRPs) and Ti-6Al-4V alloys are being used. These materials, with excellent weight-to-strength ratios, are widely used for structural applications in aircraft manufacturing. To date, several studies have been published showing that the use of metalworking fluids (MWFs), special tool geometries, or advanced machining techniques is required to ensure a surface quality that meets aerospace component standards. Conventional MWFs pose a number of environmental and worker health hazards and also degrade the mechanical properties of CFRPs due to water absorption in the composite. Therefore, a transition to more environmentally friendly cooling/lubrication techniques that prevent moisture problems in the composite is needed. This research shows that lubricated LCO₂ is a viable option to improve the quality of drilled CFRP and titanium aerospace components compared to dry machining, while maintaining clean work areas. The results show that the best combination of tool geometry and cooling conditions for machining both materials is drilling with Brad point drills and lubricated LCO₂. Drilling under these conditions resulted in a 90 % improvement in fiber pull-out volume compared to dry machined CFRP holes. In addition, a 33 % reduction in burr height and a 15 % improvement in surface roughness were observed compared to dry drilling of titanium.