Blocked nozzle detection and remedial method and system
    1.
    发明授权
    Blocked nozzle detection and remedial method and system 有权
    堵塞喷嘴检测及补救方法及系统

    公开(公告)号:US08676391B2

    公开(公告)日:2014-03-18

    申请号:US13091525

    申请日:2011-04-21

    IPC分类号: G05D11/00

    摘要: System and method for controlling a stuck nozzle system installed between first and second turbines connected in series to a compressor. The method includes determining whether the nozzle system is stuck; instructing the first turbine to increase a minimum speed reference when the nozzle system is stuck; verifying whether the nozzle system continues to be stuck; instructing the compressor to increase an inlet bleed heat (IBH) flow from a current value to a maximum value when the nozzle system is stuck; verifying whether the nozzle system continues to be stuck; and instructing the compressor to increase an inlet guide vanes (IGV) angle from a current value to a maximum value when the nozzle system is stuck.

    摘要翻译: 用于控制安装在与压缩机串联连接的第一和第二涡轮机之间的卡住喷嘴系统的系统和方法。 该方法包括确定喷嘴系统是否卡住; 指示第一涡轮机在喷嘴系统卡住时增加最小速度参考值; 验证喷嘴系统是否继续卡住; 指示当喷嘴系统被卡住时,压缩机将入口放热(IBH)流从当前值增加到最大值; 验证喷嘴系统是否继续卡住; 并且当喷嘴系统被卡住时,指示压缩机将入口导叶(IGV)角从当前值增加到最大值。

    BLOCKED NOZZLE DETECTION AND REMEDIAL METHOD AND SYSTEM
    2.
    发明申请
    BLOCKED NOZZLE DETECTION AND REMEDIAL METHOD AND SYSTEM 有权
    阻塞式喷嘴检测和补救方法与系统

    公开(公告)号:US20110270447A1

    公开(公告)日:2011-11-03

    申请号:US13091525

    申请日:2011-04-21

    IPC分类号: G05D7/00

    摘要: System and method for controlling a stuck nozzle system installed between first and second turbines connected in series to a compressor. The method includes determining whether the nozzle system is stuck; instructing the first turbine to increase a minimum speed reference when the nozzle system is stuck; verifying whether the nozzle system continues to be stuck; instructing the compressor to increase an inlet bleed heat (IBH) flow from a current value to a maximum value when the nozzle system is stuck; verifying whether the nozzle system continues to be stuck; and instructing the compressor to increase an inlet guide vanes (IGV) angle from a current value to a maximum value when the nozzle system is stuck.

    摘要翻译: 用于控制安装在与压缩机串联连接的第一和第二涡轮机之间的卡住喷嘴系统的系统和方法。 该方法包括确定喷嘴系统是否卡住; 指示第一涡轮机在喷嘴系统卡住时增加最小速度参考值; 验证喷嘴系统是否继续卡住; 指示当喷嘴系统被卡住时,压缩机将入口放热(IBH)流从当前值增加到最大值; 验证喷嘴系统是否继续卡住; 并且当喷嘴系统被卡住时,指示压缩机将入口导叶(IGV)角从当前值增加到最大值。