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System and method for turbomachinery vane prognostics and diagnostics

机译:用于涡轮机械叶片预测和诊断的系统和方法

摘要

One embodiment includes a system including an actuation system of a gas turbine system including an actuator, a positioner including one or more sensors, a motor, and a controller communicably coupled to the positioner and the motor. The actuator is coupled to one or more inlet guide vanes (IGVs) or variable stator vanes (VSVs) and configured to move the IGVs or VSVs, the positioner is configured to position the actuator so that the actuator moves the IGVs or VSVs to a desired angle, the motor is configured to drive the actuator, and the controller is configured to establish one or more baselines for one or more types of data obtained by the sensors at initialization of the gas turbine system, derive a deviation from the baselines, and perform a preventative action if a deviation that meets or exceeds a threshold is derived.
机译:一个实施例包括一种系统,该系统包括燃气涡轮机系统的致动系统,该燃气涡轮机系统包括致动器,包括一个或多个传感器的定位器,电动机以及可通信地耦合到定位器和电动机的控制器。致动器联接至一个或多个入口导向叶片(IGV)或可变定子叶片(VSV),并被配置为移动IGV或VSV,定位器被配置为定位致动器,使得致动器将IGV或VSV移动至期望的位置。角度,电机配置为驱动执行器,控制器配置为为燃气轮机系统初始化时传感器获取的一种或多种类型的数据建立一个或多个基准,得出与基准的偏差,并执行如果得出的偏差达到或超过阈值,则采取预防措施。

著录项

  • 公开/公告号US10443509B2

    专利类型

  • 公开/公告日2019-10-15

    原文格式PDF

  • 申请/专利权人 GENERAL ELECTRIC COMPANY;

    申请/专利号US201414530109

  • 发明设计人 CYRON FRANK KAY;JOHN CARVER MATERS;

    申请日2014-10-31

  • 分类号F02C9/20;F01D9/04;F01D17/08;F01D17/04;F01D21/12;F01D21/14;F01D17/16;

  • 国家 US

  • 入库时间 2022-08-21 12:16:53

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