发明申请
- 专利标题: METHODS AND SYSTEMS FOR COOLING A TRANSITION NOZZLE
- 专利标题(中): 用于冷却过渡喷嘴的方法和系统
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申请号: US13342475申请日: 2012-01-03
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公开(公告)号: US20130167543A1公开(公告)日: 2013-07-04
- 发明人: Kevin Weston McMahan , Ronald James Chila , David Richard Johns
- 申请人: Kevin Weston McMahan , Ronald James Chila , David Richard Johns
- 主分类号: F23R3/42
- IPC分类号: F23R3/42 ; B23P17/00
摘要:
A transition nozzle for use with a turbine assembly is provided. The transition nozzle includes a liner defining a combustion chamber therein, a wrapper circumscribing the liner such that a cooling duct is defined between the wrapper and the liner, a cooling fluid inlet configured to supply a cooling fluid to the cooling duct, and a plurality of ribs coupled between the liner and the wrapper such that a plurality of cooling channels are defined in the cooling duct.
公开/授权文献
- US09243506B2 Methods and systems for cooling a transition nozzle 公开/授权日:2016-01-26
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