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
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
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