SYSTEMS AND METHODS FOR TURBINE SYSTEM OPERATION IN LOW AMBIENT TEMPERATURES
    7.
    发明申请
    SYSTEMS AND METHODS FOR TURBINE SYSTEM OPERATION IN LOW AMBIENT TEMPERATURES 审中-公开
    低温环境下涡轮机系统运行的系统与方法

    公开(公告)号:US20160258327A1

    公开(公告)日:2016-09-08

    申请号:US14638972

    申请日:2015-03-04

    Abstract: A system includes a controller communicatively coupled to a compressor. The controller is configured to sense an exhaust temperature of a gas turbine system fluidly coupled to the compressor and derive a setpoint based on the sensed exhaust temperature. The controller is also configured to actuate an inlet bleed heat valve based on the derived setpoint and an ambient temperature. The inlet bleed heat valve directs a compressor fluid from the compressor into a fluid intake system fluidly coupled to the compressor upstream of the compressor and configured to intake a fluid.

    Abstract translation: 系统包括通信地耦合到压缩机的控制器。 控制器被配置为感测流体耦合到压缩机的燃气轮机系统的排气温度,并基于感测的排气温度导出设定点。 控制器还被配置为基于导出的设定点和环境温度来致动入口放气热阀。 入口放气热阀将来自压缩机的压缩机流体引导到在压缩机上游流体地联接到压缩机的压缩机的流体进气系统中,并配置成吸入流体。

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