发明授权
US08894363B2 Cooling module design and method for cooling components of a gas turbine system
有权
用于冷却燃气轮机系统组件的冷却模块设计和方法
- 专利标题： Cooling module design and method for cooling components of a gas turbine system
- 专利标题（中）： 用于冷却燃气轮机系统组件的冷却模块设计和方法
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申请号： US13023716申请日： 2011-02-09
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公开(公告)号： US08894363B2公开(公告)日： 2014-11-25
- 发明人: Ching-Pang Lee , Humberto A. Zuniga , Jay A. Morrison , Brede J. Kolsrud , John J. Marra
- 申请人： Ching-Pang Lee , Humberto A. Zuniga , Jay A. Morrison , Brede J. Kolsrud , John J. Marra
- 申请人地址： US FL Orlando US VA Chrlottesville
- 专利权人： Siemens Energy, Inc.,Mikro Systems, Inc.
- 当前专利权人： Siemens Energy, Inc.,Mikro Systems, Inc.
- 当前专利权人地址： US FL Orlando US VA Chrlottesville
- 主分类号： F01D5/18
- IPC分类号： F01D5/18
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.