| 摘要 |
<p>SYSTEM AND METHOD FOR CONTROLLING TEMPERATURE OF AIR AT AN INLET OF A GAS TURBINE A system for controlling a temperature of air at an inlet of a gas turbine is presented. The system includes an ejector operatively coupled to a heat recovery steam generator and configured to generate an intermediate pressure refrigerant by using a high pressure refrigerant. Also, the system includes a condenser operatively coupled to the ejector and configured to extract heat from the intermediate pressure refrigerant. Further, the system includes an expanding unit operatively coupled to the condenser and configured to expand the intermediate pressure refrigerant to generate a low pressure refrigerant. In addition, the system includes a heat exchanging unit configured to receive the low pressure refrigerant from the expanding unit, the high pressure refrigerant from the heat recovery steam generator, or both, and control the temperature of the inlet air based on the received low pressure refrigerant, the received high pressure refrigerant, or both. FIG. 1</p> |
