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Fault diagnosis during testing of turbine unit

机译:涡轮机组测试期间的故障诊断

摘要

A method of fault diagnosis during testing of a turbine unit includes a) obtaining measurement data from turbine sensors and testing sensors, b) calculating at least one parameter value based on measurement data, c) determining a deviation of the measurement data and the at least one parameter value by comparing the measurement data and the at least one parameter value with predetermined reference data, and d) matching the determined deviation to a plurality of predetermined fault signatures in order to detect a fault. The plurality of predetermined fault signatures includes a first set of fault signatures and a second set of fault signatures, the first set of fault signatures corresponding to turbine sensor faults and/or testing sensor faults and assumed fault-free turbine components, the second set of fault signatures corresponding to turbine component faults and assumed fault-free turbine sensors and testing sensors.
机译:在涡轮机单元的测试期间的故障诊断方法包括a)从涡轮传感器和测试传感器获得测量数据,b)基于测量数据计算至少一个参数值,c)确定测量数据的偏差和至少 通过将测量数据和至少一个参数值与预定参考数据的至少一个参数值进行比较来匹配所确定的偏差,以检测故障,使得确定的偏差与多个预定故障签名匹配。 多个预定故障签名包括第一组故障签名和第二组故障签名,第一组故障签名对应于涡轮传感器故障和/或测试传感器故障,并假设无故障涡轮机组件,第二组 对应于涡轮部件故障的故障签名,并假设无故障涡轮机传感器和测试传感器。

著录项

  • 公开/公告号US11187621B2

    专利类型

  • 公开/公告日2021-11-30

    原文格式PDF

  • 申请/专利权人 SIEMENS ENERGY GLOBAL GMBH & CO. KG;

    申请/专利号US201716091882

  • 发明设计人 LALITH FERNANDO;

    申请日2017-04-21

  • 分类号G01M15/14;G01M15/02;

  • 国家 US

  • 入库时间 2024-06-14 22:22:14

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