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 |
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代理人 |
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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 |