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Method for non-intrusive on-line detection of turbine blade condition

机译:涡轮叶片状态的非侵入式在线检测方法

摘要

A system for on-line detection of incipient cracks in turbine blades to serve as early warning system for turbine blade failure. The system of non-intrusive detection of turbine blade condition of the invention is simple and cost effective and would enable assessing the health of the turbine blade during plant operation, which is extremely important for the safe operation of the turbine in an operating power plant. The present method and system of identifying the presence of modulated blade passing frequency (BPF) for blade vibration that is not correlatable to the change in the operating condition and would thus be indicative of presence of cracked blades with incipient cracking. It is capable for verifying the Campbell diagram and ascertain the margin available between the natural frequency of the blade/stage and the steam excitation frequencies/engine orders.
机译:一种用于在线检测涡轮叶片中的初期裂纹的系统,可作为涡轮叶片故障的预警系统。本发明的非侵入式检测涡轮叶片状况的系统简单且成本有效,并且将能够评估在工厂运行期间涡轮叶片的健康状况,这对于在运转的发电厂中涡轮的安全运行极为重要。本发明的方法和系统为叶片振动识别调制叶片通过频率(BPF)的存在,该频率与工作条件的变化不相关,因此将指示存在裂纹并出现初期裂纹。它能够验证坎贝尔图并确定叶片/级的固有频率与蒸汽激励频率/发动机阶数之间的可用余量。

著录项

  • 公开/公告号US9557210B2

    专利类型

  • 公开/公告日2017-01-31

    原文格式PDF

  • 申请/专利权人 ASWATHANARAYAN RAMA RAO;

    申请/专利号US20070525358

  • 发明设计人 ASWATHANARAYAN RAMA RAO;

    申请日2007-02-02

  • 分类号G06F19/00;G01H17/00;G01H11/00;G01H1/00;

  • 国家 US

  • 入库时间 2022-08-21 13:41:59

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