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System and method for turbomachinery rotor and blade prognostics and diagnostics

机译:用于涡轮机械转子和叶片的预测和诊断的系统和方法

摘要

Systems and methods include actuation system of turbomachinery that include an actuator configured to control pitch of vanes of the turbomachinery and a positioner configured to position the actuator to control the pitch. The actuation system also includes a controller system communicably coupled to the positioner. The controller system is configured to drive the positioner based at least in part on a set point of the turbomachinery and obtain data from the positioner indicating an amount of force used for a target pitch. Using the data, the controlling system derives an operating condition for the turbomachinery and controls the turbomachinery based at least in part on the operating condition of the turbomachinery.
机译:系统和方法包括涡轮机械的致动系统,其包括构造成控制涡轮机械的叶片的桨距的致动器和构造成定位致动器以控制桨距的定位器。致动系统还包括可通信地耦合到定位器的控制器系统。控制器系统构造成至少部分地基于涡轮机械的设定点来驱动定位器,并且从定位器获得指示用于目标俯仰的力的量的数据。使用该数据,控制系统至少部分地基于涡轮机的运行状况来导出涡轮机的运行状况并控制涡轮机。

著录项

  • 公开/公告号US10519964B2

    专利类型

  • 公开/公告日2019-12-31

    原文格式PDF

  • 申请/专利权人 GENERAL ELECTRIC COMPANY;

    申请/专利号US201615371014

  • 发明设计人 SETH HARMON CHAPMAN;HUA ZHANG;

    申请日2016-12-06

  • 分类号F04D27/02;F01D17/12;F02C7/042;F02C7/057;F04D27;F01D9/04;F04D29/56;G05B19/402;

  • 国家 US

  • 入库时间 2022-08-21 11:27:12

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