发明名称 |
TURBINE ENGINE FUEL NOZZLE AND TURBINE ENGINE |
摘要 |
PROBLEM TO BE SOLVED: To provide a fuel nozzle 100 for a turbine engine 10. SOLUTION: This fuel nozzle includes a one-piece housing to 124 connected to a one-piece venturi 128. The housing includes an annular fuel nozzle tip part and a plurality of openings adapted to discharge air radially outwardly from the fuel nozzle tip part. The venturi is connected to the housing to form a fuel chamber within the fuel nozzle tip part. A one-piece swirler 136 is connected with the venturi and extends radially inward from the venturi. The swirler can enhance mixing of fuel and air within the fuel chamber. COPYRIGHT: (C)2007,JPO&INPIT
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申请公布号 |
JP2007155318(A) |
申请公布日期 |
2007.06.21 |
申请号 |
JP20060324047 |
申请日期 |
2006.11.30 |
申请人 |
GENERAL ELECTRIC CO <GE> |
发明人 |
MCMASTERS MARIE ANN;GLYNN CHRISTOPHER CHARLES;BROUGHER BRIAN C |
分类号 |
F23R3/28;F23R3/14;F23R3/34 |
主分类号 |
F23R3/28 |
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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