| 摘要 |
PROBLEM TO BE SOLVED: To provide an inlet air cooling and filtering system (100) for a gas turbine. SOLUTION: The inlet air cooling and filtering system (100) for a gas turbine includes a first-step spraying array (110) with the first number of spraying nozzle pairs (120), and a second-step spraying array (130) with the second number of spraying nozzle pairs (120), and a drift eliminator (140). COPYRIGHT: (C)2008,JPO&INPIT
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