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Monitoring and control of manufacturing process to assist the surface workpiece quality when drilling

机译:监控和控制制造过程,钻孔时辅助表面工件质量

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There is a variety of reasons for the installation of a monitoring system in a manufacturing process. Hole-making mainly drilling is one of the most common operation used and usually is carried out as one of the last steps in the production process. Holes in rotating turbine and compressor disks are among the most highly-stressed geometric features of jet-engines. For manufacturers of jet-engine components it is important to assess the quality of these at an early stage in the manufacturing of the product. The use of commercially available monitoring systems in hole-making has been successful in individual cases so far. Major reasons for this lack of effectiveness are the large material variations within one production batch, the overall difficult machinability of the materials applied, the small lot size which makes "teach-in" operations ineffective. The paper describes a design of adaptive control system for drilling process of aerospace critical components. The proposed system is directed towards the real time control of selected surface roughness parameter. Proposed model for monitoring and control consists of two subsystems: surface roughness prediction subsystem and decision making subsystem. The artificial neural network was employed to calculate surface roughness parameters throughout process monitoring indices such as torque M_z, force F_z, power P and cutting conditions feed f, cutting speed v_c. Due to ability to predict nonlinear behaviour and quickly calculate future values, artificial neural networks are ideal for both predictive and adaptive controllers. Test samples were nickel based super alloy Udimet 720 used in discs for gas turbine engines. The experimental results show that predicted values of surface roughness are very close to the values measured experimentally. Advantages of the proposed subsystem for surface roughness prediction are simplicity, computational power and speed, capacity and ability to learn from system changes as they become.
机译:在制造过程中安装监控系统存在多种原因。钻孔主要是钻探是最常见的操作之一,通常是生产过程中最后一个步骤之一。旋转涡轮机和压缩机盘中的孔是喷气发动机最高兴的几何特征之一。对于喷射发动机组件的制造商来说,在制造产品的早期评估这些产品的质量非常重要。到目前为止,在单个情况下,使用商业上可获得的监控系统在单个情况下取得了成功。这种缺乏有效性的主要原因是一种生产批次内的大物质变化,所施加的材料的整体困难可加工性,少量尺寸,使“教学”操作无效。本文介绍了航空临界临界部件钻井过程自适应控制系统的设计。所提出的系统旨在朝向所选表面粗糙度参数的实时控制。提出的监控和控制模型包括两个子系统:表面粗糙度预测子系统和决策子系统。使用人工神经网络在整个过程监测指标中计算表面粗糙度参数,例如扭矩M_Z,力F_Z,功率P和切割条件FEVER F,切割速度V_C。由于预测非线性行为并快速计算未来值的能力,人工神经网络对于预测性和自适应控制器来说是理想的。试验样品是基于镍的超合物UDIMET 720,用于燃气轮机发动机的盘。实验结果表明,预测的表面粗糙度值非常接近实验测量的值。所提出的表面粗糙度预测的子系统的优点是简单,计算能力和速度,容量以及从系统变化中学习的能力和能力。

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