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Comparison of Sensors Signal Quality when Drilling Inconel 718

机译:钻Inconel 718时传感器信号质量的比较

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Aero engines clearly differ from other propulsion systems used in general mechanical engineering particularly through the materials used and the extreme stresses that occur during operation. Boltholes 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. Additional challenges occur during the implementation of monitoring systems in production. Here, the monitoring solution is judged predominantly by its robustness, its reliability against false alarms and its level of integration in the machine tool. A high level of integration can be achieved by using internal data, provided by the components of the machine tools themselves. The paper describes a new approach in real-time monitoring for drilling boltholes. In an experimental setup, process data origination from the NC of a Sinumeric 840D, collected by an OPC-Server had been processed. Comparing OPC data logging, DAU data logging and profibus data logging with respect to data quality, sample rate and real-time behaviour, profibus data logging appears to be the favourable choice. Compared to the price of many dedicated external sensors, all three methods to log internal data provide data access with small investments on a high level of integration. The experimental results indicate that OPC-data are suitable for tool wear monitoring and surface quality evaluation after drilling with solid carbide drills and face cutting reamers in Inconel718 workpieces.
机译:航空发动机与通用机械工程中使用的其他推进系统明显不同,特别是通过使用的材料和运行过程中产生的极端应力。旋转涡轮和压缩机盘上的螺栓孔是喷气发动机承受的最大应力几何特征之一。对于喷气发动机组件制造商而言,在产品制造的早期阶段评估它们的质量非常重要。迄今为止,在个别情况下,在制孔中使用了可商购的监控系统是成功的。缺乏有效性的主要原因是,一个生产批次内的材料差异很大,所用材料的整体机械加工难度大,批量很小,这使得“示教”操作无效。在生产中实施监视系统期间,还会遇到其他挑战。在此,监控解决方案主要由其坚固性,对误报的可靠性以及其在机床中的集成度来判断。通过使用由机床本身的组件提供的内部数据,可以实现高度集成。本文介绍了一种实时监测钻孔螺栓孔的新方法。在实验设置中,已经处理了由OPC服务器收集的源自Sinumeric 840D的NC的过程数据。比较OPC数据记录,DAU数据记录和profibus数据记录在数据质量,采样率和实时行为方面,profibus数据记录似乎是首选。与许多专用外部传感器的价格相比,这三种记录内部数据的方法都可以在高度集成的情况下以少量投资提供数据访问。实验结果表明,OPC数据适用于在Inconel718工件上用整体硬质合金钻头和端面切削铰刀钻孔后的刀具磨损监测和表面质量评估。

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