发明名称 |
Combustor Nozzle/Premixer with Curved Sections |
摘要 |
An apparatus for premixing fuel and air prior to combustion in a gas turbine engine includes an annular fuel passage receiving fuel from a fuel source. The annular fuel passage includes a fuel plenum and has a wave shape with a peak section surrounded by trough sections. An annular air passage surrounds the annular fuel passage. The annular air passage receives air to be mixed with the fuel in the fuel passage for downstream combustion. A plurality of swirler vanes are disposed in the annular air passage adjacent the fuel plenum.
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申请公布号 |
US2013180248(A1) |
申请公布日期 |
2013.07.18 |
申请号 |
US201213352814 |
申请日期 |
2012.01.18 |
申请人 |
PARSANIA NISHANT GOVINDBHAI;SINGH AJAY PRATAP |
发明人 |
PARSANIA NISHANT GOVINDBHAI;SINGH AJAY PRATAP |
分类号 |
F23R3/30 |
主分类号 |
F23R3/30 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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