发明名称 COOLING SYSTEM FOR TURBOMACHINE
摘要 <p><P>PROBLEM TO BE SOLVED: To provide a cooling system improving combined cycle efficiency and an increase in power output by reducing exhaust dilution losses and reducing the parasitic load by requiring fewer air circulation devices, and reducing the installation and start-up costs by requiring fewer air circulation devices and integrating the systems. <P>SOLUTION: Fluid communication of integrated cooling circuits cooling each of a plurality of compartments 105, 110 of a gas turbine device constituting a turbomachine 100 is established, and a cooling fluid comprising compartment air is circulated between the circuits. <P>COPYRIGHT: (C)2010,JPO&INPIT</p>
申请公布号 JP2010133408(A) 申请公布日期 2010.06.17
申请号 JP20090273092 申请日期 2009.12.01
申请人 GENERAL ELECTRIC CO 发明人 CHILLAR RAHUL J;SMITH RAUB W
分类号 F02C7/18;F01D25/30;F01K23/10;F02C6/18;F02C7/00 主分类号 F02C7/18
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