铸铝薄壁件高速钻深孔技术研究

为解决铸铝薄壁件进气机匣的深孔加工，针对麻花钻加工深孔的难点，在加工中心上研究了用枪钻和GT深孔麻花钻高速加工深孔的方案和工艺参数，并探讨了雾化高压气体强制排屑加工深孔的技术，获得了典型薄壁箱体零件的高速钻深孔的经验。     

复合涂层刀具钻削高温合金Inconel 718钻削性能研究

高温合金Inconel 718是一种典型的难加工材料,本文利用DEFORM-3D软件对无涂层、TiC单涂层和TiC/Al₂O₃复合涂层硬质合金刀具进行钻削高温合金Inconel 718的仿真分析,研究在不同钻削条件下复合涂层刀具的切削性能,并进行钻削实验进行验证。结果表明：TiC/Al₂O₃复合涂层刀具能有效降低钻削轴向力和钻削温度,其轴向力降低幅度最高为20%,钻削温度最高降低了35%。通过钻削实验验证了仿真模型的准确性,可为实际钻削加工高温镍基合金Inconel 718中选择涂层种类及钻削参数提供参考。     

低密实度基础月壤的钻进压力建模及试验验证

基于钻采过程中月壤颗粒的运动规律提出了一种钻具与月壤相互作用区域的等效方法,并由此从宏观角度建立了一种新型月壤钻进压力解析模型.通过70％密实度基础月壤地面钻采试验验证了该模型对低密实度月壤钻进压力的预测能力,得到了相关修正系数与钻进比之间的关系并分析了模型的可扩展性.该建模方法为复杂工况下钻具-土体相互作用建模提供了...     

Formation of interlayer gap and control of interlayer burr in dry drilling of stacked aluminum alloy plates

In aircraft assembly, interlayer burr formation in dry drilling of stacked metal materials is a common problem. Traditional manual deburring operation seriously affects the assembly qual-ity and assembly efficiency, is time-consuming and costly, and is not conducive to aircraft automatic assembly based on industrial robot. In this paper, the formation of drilling exit burr and the influ-ence of interlayer gap on interlayer burr formation were studied, and the mechanism of interlayer gap formation in drilling stacked aluminum alloy plates was investigated, a simplified mathematical model of interlayer gap based on the theory of plates and shells and finite element method was established. The relationship between interlayer gap and interlayer burr, as well as the effect of feed rate and pressing force on interlayer burr height and interlayer gap was discussed. The result shows that theoretical interlayer gap has a positive correlation with interlayer burr height and preloading pressing force is an effective method to control interlayer burr formation.     

碳纤维复合材料与钛合金结构制孔工艺研究

针对碳纤维复合材料(CFRP)与钛合金夹层结构钻削中存在的问题,进行了系统的工艺研究.主要从钻入侧的选取、钻削参数、制孔中存在的问题以及大直径孔加工工艺等几个方面进行试验研究,结果表明目前的钻削工艺需要改进.提出了适合实际操作的工艺方法,解决了夹层结构制孔中出现的问题,并对钻削刀具进行分析.     

纤维增强复合材料钻削分层的研磨检测

复合材料钻削分层缺陷是影响复合材料构件后续加工质量和效率的关键因素之一,针对该问题,设计不同钻深孔的分层缺陷产生与检测实验,揭示分层产生及演变历程。获得了孔出口三维分层形貌,分析了分层缺陷动态变化及影响。     

某型无人机碳纤维尾撑钻孔组合夹具设计与应用

结合设计图样及材料特性,研究了一种用于加工碳纤维尾撑的工艺及钻孔组合夹具,并阐述了其设计要点。     

Cutting force and specific energy for rotary ultrasonic drilling based on kinematics analysis of vibration effectiveness

Rotary ultrasonic drilling(RUD) has become an effective approach for machining advanced composites which are widely using in the field of aeronautics. The cutting kinematics and the corresponding material removal mechanisms are distinct in different drilling areas during RUD. However, these fundamentals have not been fully considered in the existing studies. In this research, two distinct forms of interaction induced by ultrasonic vibration were considered as impact-separation and vibratory lapp...     

Drilling load modeling and validation based on the filling rate of auger flute in planetary sampling

Some type of penetration into a subsurface is required in planetary sampling. Drilling and coring, due to its efficient penetrating and cuttings removal characteristics, has been widely applied in previous sampling missions. Given the complicated mechanical properties of a planetary regolith, suitable drilling parameters should be matched with different drilling formations properly. Otherwise, drilling faults caused by overloads could easily happen. Hence, it is necessary to estab-lish a drilling load model, which is able to reveal the relationships among drilling loads, an auger's structural parameters, soil's mechanical properties, and relevant drilling parameters. A concept for the filling rate of auger flute (FRAF) is proposed to describe drilling conditions. If the FRAF index under one group of drilling parameters is less than 1, this means that the auger flute currently removes cuttings smoothly. Otherwise, the auger will be choked with compressed cuttings. In dril-ling operations, the drilling loads on the auger mainly come from the conveyance action, while the drilling loads on the drill bit primarily come from the cutting action. Experiments in one typical lunar regolith simulant indicate that the estimated drilling loads based on the FRAF coincide with the test results quite well. Based on this drilling load model, drilling parameters have been opti-mized.     

New design of a compact aero-robotic drilling end effector: An experimental analysis

This paper presents the development of a normal adjustment cell (NAC) in aero-robotic drilling to improve the quality of vertical drilling, by using an intelligent double-eccentric disk nor-mal adjustment mechanism (2-EDNA), a spherical plain bearing and a floating compress module with sensors. After the surface normal vector is calculated based on the laser sensors’ feedback, the 2-EDNA concept is conceived specifically to address the deviation of the spindle from the sur-face normal at the drilling point. Following the angle calculation, depending on the actual initial position, two precise eccentric disks (PEDs) with an identical eccentric radius are used to rotate with the appropriate angles using two high-resolution DC servomotors. The two PEDs will carry the spindle to coincide with the surface normal, keeping the vertex of the drill bit still to avoid repeated adjustment and position compensation. A series of experiments was conducted on an aeronautical drilling robot platform with a precise NAC. The effect of normal adjustment on bore diameter, dril-ling force, burr size, drilling heat, and tool wear was analyzed. The results validate that using the NAC in robotic drilling results in greatly improved vertical drilling quality and is attainable in terms of intelligence and accuracy.