发明名称 Inlet air conditioning system for a turbomachine
摘要 <p>An embodiment of the present invention provides an air conditioning system (115) located upstream of the inlet system (100) for a gas turbine. The air conditioning system (115) may comprise at least one conditioning module (145) for adjusting the temperature of the airstream. The at least one conditioning module (145) may have a plurality of forms including at least one of the following systems: a chiller, an evaporative cooler; a spray cooler, or combinations thereof The specific form of the at least one conditioning module (145) may be determined in part by the configuration of the gas turbine.</p>
申请公布号 EP2154351(A2) 申请公布日期 2010.02.17
申请号 EP20090167380 申请日期 2009.08.06
申请人 US 发明人 US;US;US
分类号 F02C7/04;F02C7/143 主分类号 F02C7/04
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