发明名称 FUEL NOZZLE FOR GAS TURBINE ENGINE AND METHOD FOR MANUFACTURING THE SAME
摘要 <p><P>PROBLEM TO BE SOLVED: To provide a secondary fuel nozzle assembly (200). <P>SOLUTION: This secondary fuel nozzle assembly (200) includes: a nozzle (204) including a center passage (214) and a plurality of passages (216, 218 and 220) aligned concentrically in the center passage; and a single structure head (300) coupled to the nozzle and having a plurality of inlets (328, 330, 332 and 334). Each of the plurality of inlets is in fluid-communication with at least one of the plurality of nozzle passages. <P>COPYRIGHT: (C)2009,JPO&INPIT</p>
申请公布号 JP2009030964(A) 申请公布日期 2009.02.12
申请号 JP20080190403 申请日期 2008.07.24
申请人 GENERAL ELECTRIC CO <GE> 发明人 NYBERG CHARLES RICHARD II;HESSLER WILLIAM KIRK
分类号 F23R3/28;F02C7/22;F23R3/10;F23R3/32;F23R3/34 主分类号 F23R3/28
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