发明名称 METHOD AND DEVICE FOR BURNING FUEL IN GAS TURBINE ENGINE
摘要 <p><P>PROBLEM TO BE SOLVED: To promote stabler flame formation since diffusion fuel may be concentrated on the downstream side of a fuel injection nozzle, and thereby, the diffusion fuel flame may be extinguished exceeding a rich flame extinguishment region when starting a turbine by using the diffusion fuel. <P>SOLUTION: A fuel nozzle assembly 402 comprises a main body 406 including a centerline, a first passage penetrated through the main body 406 along the centerline, and a nozzle tip 500 jointed to the downstream side end of the first passage. The nozzle tip 500 has a radius extended from the center to the outer surface. The nozzle tip 500 includes a downstream face and a plurality of outlet passages each of which includes an opening defined within the downstream face. Each of the openings includes X-, Y- and Z-axes defined with respect to the tangential line, the radius and the centerline. Each of the plurality of outlet passages forms a discharge angle of larger than 30°with respect to the Z-axis in an X-Y plane. <P>COPYRIGHT: (C)2009,JPO&INPIT</p>
申请公布号 JP2009047410(A) 申请公布日期 2009.03.05
申请号 JP20080206498 申请日期 2008.08.11
申请人 GENERAL ELECTRIC CO <GE> 发明人 ROMOSER CAREY EDWARD
分类号 F23R3/34;F02C7/22;F02C7/26;F02C9/28;F23R3/00;F23R3/20;F23R3/28;F23R3/46 主分类号 F23R3/34
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