Method and system for active tip clearance control in turbines
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    发明申请
    Method and system for active tip clearance control in turbines 失效
    涡轮机主动顶盖间隙控制方法及系统

    公开(公告)号:US20050149274A1

    公开(公告)日:2005-07-07

    申请号:US10748812

    申请日:2003-12-30

    摘要: A system for controlling blade tip clearance in a turbine. The system includes a stator including a shroud having a plurality of shroud segments and a rotor including a blade rotatable within the shroud. An actuator assembly is positioned radially around the shroud and includes a plurality of actuators. A sensor senses a turbine parameter and generates a sensor signal representative of the turbine parameter. A modeling module generates a tip clearance prediction in response to turbine cycle parameters. A controller receives the sensor signal and the tip clearance prediction and generates at least one command signal. The actuators include at least one actuator receiving the command signal and adjusts a position of at least one of the shroud segments in response to the command signal.

    摘要翻译: 一种用于控制涡轮机叶片顶端间隙的系统。 该系统包括定子,其包括具有多个护罩段的护罩和包括可在护罩内旋转的刀片的转子。 致动器组件围绕护罩径向定位,并且包括多个致动器。 传感器感测涡轮参数并产生代表涡轮机参数的传感器信号。 建模模块响应于涡轮循环参数产生尖端间隙预测。 控制器接收传感器信号和尖端间隙预测,并产生至少一个命令信号。 致动器包括响应于命令信号接收命令信号并调节至少一个护罩段的位置的至少一个致动器。