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Modal Analysis of Replica Boss Hole During the Deburring Process in Aerospace Manufacturing Industry

机译:航空航天制造业去毛刺过程中复制凸台孔的模态分析

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摘要

The monitoring of surface finishing processes in aerospace manufacturing industry becomes one of key issues to maintain the overall quality of product or part. To date, the surface quality monitoring post machining processes such as deburring, use visual inspection, surface roughness test or laser gap gun. The whole manufacturing process then requires a considerable amount of time as the production line must be halted due to these measurements taking place. This study presents an online monitoring system to measure the chamfer quality of replica boss hole post-deburring process. Vibration signal was measured during the deburring process and the features that correlate to the deburring stages (passes) were extracted. This paper focuses on the validation of actual vibration signal with the modal analysis of work coupon (replica boss hole) to obtain the correlation between the vibration amplitude level on particular region and the mode shape of work coupon during the deburring process.
机译:航空航天制造业中表面处理过程的监控已成为保持产品或零件整体质量的关键问题之一。迄今为止,表面质量监测是在加工后的过程中进行的,例如去毛刺,使用目测,表面粗糙度测试或激光测距枪。由于进行这些测量,因此必须停止生产线,因此整个制造过程需要相当长的时间。这项研究提出了一个在线监测系统,以测量复制品凸台孔去毛刺过程中的倒角质量。在去毛刺过程中测量振动信号,并提取与去毛刺阶段(通过)相关的特征。本文着重于对实际振动信号的验证,通过对工作试样(复制凸台孔)的模态分析来获得去毛刺过程中特定区域的振动幅度水平与工作试样的振型之间的相关性。

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