发明名称 GAS TURBINE INLET SYSTEM AND RELATED METHOD FOR COOLING GAS TURBINE INLET AIR
摘要 An inlet air conditioning system for a gas turbine includes an inlet duct for the with an air flow path to provide inlet air to the gas turbine; evaporative cooling media disposed in the air flow path; a water chiller; and a circulation pump that circulates water through the water chiller and the evaporative media in series. The chiller is configured to chill the water to below ambient wet-bulb temperature before the water is circulated to the evaporative cooling media. A power plant includes a gas turbine including a compressor, a combustion system, and a turbine section; a load; and the inlet air conditioning system.
申请公布号 US2015121881(A1) 申请公布日期 2015.05.07
申请号 US201314071122 申请日期 2013.11.04
申请人 General Electric Company 发明人 ZHANG Jianmin;KIPPEL Brad Aaron
分类号 F02C7/143 主分类号 F02C7/143
代理机构 代理人
主权项 1. An inlet air conditioning system for a gas turbine, the system comprising: an inlet duct for the gas turbine, the inlet duct comprising an air flow path to provide inlet air to the gas turbine; evaporative cooling media disposed in the air flow path; a water chiller; and a circulation pump that circulates water through the water chiller and the evaporative cooling media in series, wherein the chiller is configured to chill the water to below ambient wet-bulb temperature before the water is circulated to the evaporative cooling media.
地址 Schenectady NY US