发明名称 COOLING MODULE DESIGN AND METHOD FOR COOLING COMPONENTS OF A GAS TURBINE SYSTEM
摘要 A cooling arrangement in a gas turbine system (120). The arrangement includes a plurality of flow network units (208) to transfer heat to cooling fluid, at least one unit including first (218), second (220), and third (222) flow sections between openings (64a) in a first wall (66) and an opening in a second wall (68) to pass cooling fluid through the walls. The first section includes first flow paths, between the openings in the first wall and the second section, extending to the second section. The third section includes third flow paths, between the second section and the opening in the second wall, to effect flow of cooling fluid. The second section includes one or more cooling fluid flow paths between the first section and the third section. The number of flow paths in the second section is fewer than the number of first flow paths and fewer than the number of third flow paths.
申请公布号 US2012201674(A1) 申请公布日期 2012.08.09
申请号 US201113023716 申请日期 2011.02.09
申请人 发明人 LEE CHING-PANG;ZUNIGA HUMBERTO A.;MORRISON JAY A.;KOLSRUD BREDE J.;MARRA JOHN J.
分类号 F01D5/18 主分类号 F01D5/18
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