共查询到16条相似文献,搜索用时 250 毫秒
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针对六自由度串联式关节机器人气囊抛光系统因刚度不足引起的加工振动以及引入中频误差的问题,以IRB 6700机器人作为研究对象,基于Ansys Workbench建立模态分析模型,并结合实验分析机器人气囊抛光系统工况频带内动态特性,实验与仿真结果共同表明,机器人气囊抛光系统在工况频带至少存在5阶模态,且共振时机器人末端抖动幅值为mm级,机器人加工严重受限。同时针对机器人气囊抛光系统先进光学元件抛光工艺应用,设计一种阻尼抑振气囊工具头,与普通气囊工具头进行定点抛光与整面抛光对比实验。结果表明:抑振气囊头定点抛光斑粗糙度与频谱幅值普遍低于普通气囊工具头,引入的中频误差较一般气囊工具头低40%,抛光优化效果显著。 相似文献
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气囊数控抛光是近年来一种新兴的先进光学制造技术,采用柔性的气囊作为抛光工具并以进动的方式进行加工。首先简要阐述了气囊抛光的抛光原理,然后针对平面和曲面光学零件,在自行研制的气囊抛光实验样机上进行了抛光实验。被抛光光学元件的材料去除是在抛光区内实现的。研究了进动角、气囊压缩量、气囊内部压力、气囊转速、抛光时间以及工件的曲率半径几种重要的工艺参数对平面工件和球面工件抛光接触区大小和形状影响情况的异同。在此基础上,总结了气囊抛光材料去除的影响规律。给出了几种重要工艺参数在平面工件和球面工件上取值范围。 相似文献
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为保证气囊抛光过程中抛光运动的高稳定性和均匀材料去除率,对气囊抛光非球面过程中气囊工具刚度的可控性进行了研究。通过分析气囊抛光大口径光学元件时工具的受力情况,计算了气囊工具的刚度,并分析了气囊抛光工具刚度对抛光时材料去除的影响及气囊工具刚度的影响因素。设计了气囊工具刚度控制算法并进行模拟试验,仿真结果表明,在刚度标准值根据加工要求设定以后,即可通过调节工件对气囊工具的反作用力,使得气囊抛光大口径光学元件过程中气囊工具刚度可控。 相似文献
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根据大口径非球面光学元件的实际加工需要,设计并制造可控气囊抛光系统,并对机构进行运动学仿真,仿真结果表明,气囊自转轴的运动空间可以满足大口径非球面光学元件的连续进动加工要求。为了证明所设计系统的可加工性,以直径320 mm的圆形平面光学元件进行加工实验。经过该气囊抛光工具24 h的抛光后,工件达到较好的面型精度,光学元件的表面粗糙度由0.272减小到0.068(=632.8 nm), PV值从1.671降低到0.905。对光学元件的实际加工实验结果表明:可控气囊抛光系统在加工过程中结构稳定性好,符合设计要求,可有效提高加工工件面型精度。 相似文献
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空间光学元件超精密气囊抛光的去除特性研究 总被引:1,自引:0,他引:1
为得到空间光学元件超光滑表面,对超精密气囊抛光方法的去除特性进行了理论和实验研究.以Preston方程为基础,应用运动学原理建立了气囊抛光"进动"运动的材料去除模型,针对抛光气囊工具的物理特性,按照Hertz接触理论对去除模型进行了修正;利用计算机仿真的方法,分析了几个主要工艺参数对"进动"抛光运动去除特性的影响规律,并在超精密光学数控抛光机上进行了正交实验;仿真和实验结果吻合较好,总结得到4点气囊抛光方法中重要的结论,给出了"进动"角与压缩量的取值范围,以此得到了面型精度RMS值为0.024λ(λ=0.6328 μm)的超光滑表面,为开展光学元件气囊抛光工艺研究提供依据. 相似文献
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针对非球面光学元件连续变曲率的特点,提出了一种基于平面抛光斑演变获取非球面磁流变抛光去除函数的技术思路。通过分析磁流变抛光机理,建立了磁流变抛光多因素耦合作用模型。基于该模型提出磁流变抛光去除函数获取的微分解耦方法,实现对抛光斑形成机制中的几何因素解耦,发现当工艺条件变化较小时,在空间中的特定点处,去除效率的变化量与工件浸入深度的改变量呈线性关系。实验观测的20个点中,有17处决定系数在90%以上,另外3处在80%以上,峰值去除率和体积去除率演变的决定系数分别达到92%和94%,实验验证了这一结论。 相似文献
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为了更加完善环带抛光技术并指导加工,根据Preston方程建立了材料去除量的理论模型。考虑到环带抛光技术中的诸影响因素,如抛光盘与工件之间的转速比、偏心距及压强分布等参数,建立材料去除量与各影响因素之间的相互关系的数学模型。理论分析和实验结果表明:材料的去除效率随转速比和偏心距增加而增大,转速比越接近于1时,磨削越均匀;工件露边时,工件露出部分材料的去除效率急剧下降。通过对该理论模型中的相关技术参数研究来完善环带抛光技术,有效地提高抛光的效率及稳定性。 相似文献
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工具定位精度和工艺合理性规划是影响自由曲面表面高质量制造的主要因素。研究了立足计算机控制的确定性制造概念。借助于多自由度机构平台,采取点对点的材料去除方式,针对具有非平缓变化曲率或陡度的自由曲面表面,设计工具结构、规划抛光路径,实施快速均匀抛光,为构建自由曲面计算机控制制造专家系统提供了支撑。 相似文献
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Laplace-transform and Z-transform theories have been applied to analyze the tensile stress–strain curves of a co-woven-knitted (CWK) composite under quasi-static (0.001/s) and high strain rates (up to 2586/s) tension. The transform results were extended to characterize the tension failure and dynamic responses of the CWK composite in the frequency domain. Specifically, the Laplace-transform theory was employed to analyze the stress–strain curves of the CWK composite along 0°, 45° and 90° directions when the composite is assumed to be a continuous system, while the Z-transform theory was used for the discrete system for the composite. From the transformed results, it was found that the stress–strain curves of the CWK composite specimen under different strain rates tension have similar stability behaviours for the Laplace- and Z-transform. For the continuous system, few pole plots are distributed on the left side of the imaginary axis, which means the system is unstable. Nevertheless, the pole-plot distribution is stable before the post-critical deformation of the CWK composite. For the discrete system, most of the poles are located inside the unit circle before post-critical deformation, indicating the system is stable. From the stiffness–time history and fracture morphology, the stability of the pole-plot distribution corresponds to the stiffness stability and fracture uniformity. From continuous and discrete system analyses, it is found that the stress–time and strain-time histories of the CWK composite can be regarded as a digital signal system. Digital signal processing (DSP) methods can be extended to the investigation of the mechanical behaviour of composites. 相似文献
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Study of weighted space deconvolution algorithm in computer controlled optical surfacing formation 总被引:2,自引:0,他引:2
Theoretical and experimental research on the deconvolution algorithm of dwell time in the technology of computer controlled optical surfacing (CCOS) formation is made to get an ultra-smooth surface of space optical element. Based on the Preston equation, the convolution model of CCOS is deduced. Considering the morbidity problem of deconvolution algorithm and the actual situation of CCOS technology, the weighting spatial deconvolution algorithm is presented based on the non-periodic matrix model, which avoids solving morbidity resulting from the noise induced by measurement error. The discrete convolution equation is solved using conjugate gradient iterative method and the workload of iterative calculation in spatial domain is reduced effectively. Considering the edge effect of convolution algorithm, the method adopts a marginal factor to control the edge precision and attains a good effect. The simulated processing test shows that the convergence ratio of processed surface shape error reaches 80%. This algorithm is further verified through an experiment on a numerical control bonnet polishing machine, and an ultra- smooth glass surface with the root-mean-square (RMS) error of 0.0088 tim is achieved. The simulation and experimental results indicate that this algorithm is steady, convergent, and precise, and it can satisfy the solving requirement of actual dwell time. 相似文献