发明申请
US20130025293A1 TEMPERATURE MIXING ENHANCEMENT WITH LOCALLY CO-SWIRLING QUENCH JET PATTERN FOR GAS TURBINE ENGINE COMBUSTOR
有权
燃气涡轮发动机燃烧器的本地混合燃油喷射模式的温度混合增强
- 专利标题： TEMPERATURE MIXING ENHANCEMENT WITH LOCALLY CO-SWIRLING QUENCH JET PATTERN FOR GAS TURBINE ENGINE COMBUSTOR
- 专利标题（中）： 燃气涡轮发动机燃烧器的本地混合燃油喷射模式的温度混合增强
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申请号： US13194182申请日： 2011-07-29
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公开(公告)号： US20130025293A1公开(公告)日： 2013-01-31
- 发明人: Won-Wook Kim , James B. Hoke , Timothy S. Snyder
- 申请人： Won-Wook Kim , James B. Hoke , Timothy S. Snyder
- 主分类号： F02C1/06
- IPC分类号： F02C1/06 ; F23R3/20 ; F23R3/06
摘要：
A combustor for a turbine engine includes a first liner defined about an axis with a first row of first combustion air holes, one of the first combustion air holes is defined along each of a multiple of fuel injector zero pitch lines. A second liner defined about the axis with a second row of second combustion air holes, each of the second combustion air holes circumferentially offset relative to each of the multiple of fuel injector zero pitch lines.
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