首页> 外文会议>International Conference on Condition Monitoring and Machinery Failure Prevention Technologies >Evaluation of a Condition Monitoring Method's Fault Detection Reliability for Condition-Based Maintenance Applications
【24h】

Evaluation of a Condition Monitoring Method's Fault Detection Reliability for Condition-Based Maintenance Applications

机译:基于条件的维护应用程序的情况监测方法的故障检测可靠性评估

获取原文
获取外文期刊封面目录资料

摘要

When implementing Condition-Based Maintenance (CBM) for safety-critical systems such as aircraft, it is necessary to demonstrate the effectivity of the applied Condition Monitoring System (CMS) in detecting potential faults before failure. A quantitative fault detection reliability assessment for a given monitoring method and fault type, adapted from the field of Non-Destructive Testing (NDT), is proposed. It involves first modeling the relationship between the Condition Indicator values obtained with the CMS, for example vibration levels, and the corresponding fault severity in a signal response model. After defining an acceptable Probability of False Alarm (PoFA), the Probability of Detection (PoD) of the fault can be computed from the signal response model as a function of fault severity. Vibration monitoring presents particular challenges with regard to fault detection reliability, due to the high variability often encountered in vibration measurements. Further, a large number of individual Condition Indicators are typically computed from a vibration measurement and used for diagnostics. To systematically compare the detection performance of various indicators and to identify those indicators with the most significant response to a given fault, a discriminability measure derived from the signal response model is introduced. The fault detection reliability evaluation is demonstrated with vibration monitoring data from a series of Seeded Fault Tests (SFT) on helicopter tail rotor drive shaft bearings. Multiple bearings were first tested in an undamaged state, and then retested after the insertion of a local defect on the bearing inner ring race. The size of the defects was artificially increased in several steps, to obtain data over a range of fault severities. The evaluation shows that a Condition Indicator intended to detect bearing inner race faults indeed exhibits the most significant signal response, and achieves a high PoD at small defect sizes.
机译:当为诸如飞机的安全关键系统实施基于条件的维护(CBM)时,有必要展示应用的状态监测系统(CMS)在失败前检测潜在故障的有效性。提出了一种定量的故障检测可靠性评估,用于给定的监测方法和故障类型,从非破坏性测试(NDT)的领域适应。它涉及首先建模在信号响应模型中的CMS,例如振动水平获得的条件指示符之间的关系,以及信号响应模型中的相应故障严重性。在定义假警报(POFA)的可接受概率之后,可以根据故障严重性的函数从信号响应模型计算故障的检测(POD)的概率。由于在振动测量中通常遇到的高可变性,振动监测对故障检测可靠性方面具有特殊挑战。此外,通常从振动测量计算大量单独的条件指示符并用于诊断。为了系统地比较各种指示器的检测性能并识别这些指标对给定故障的最显着响应,引入了从信号响应模型导出的可辨别性测量。故障检测可靠性评估通过从直升机尾转子驱动轴轴承的一系列种子故障测试(SFT)的振动监测数据进行了说明。首先在未损坏的状态下测试多个轴承,然后在插入轴承内圈血上的局部缺陷后重新测试。缺陷的大小在几个步骤中是人为地增加的,以获得一系列故障严重程度的数据。评估表明,旨在检测轴承内部竞争故障的条件指示器确实表现出最显着的信号响应,并以小缺陷尺寸实现高荚。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号