发明名称 FUEL SUPPLY SYSTEM FOR GAS TURBINE ENGINE
摘要 PROBLEM TO BE SOLVED: To provide combustor operating conditions having a wide range, and a corresponding fuel supply system.SOLUTION: A fuel supply system may include a fuel injector 100B having a primary and a secondary pilot fuel nozzle 104, 106 in fluid communication with a primary and a secondary fuel circuit 204, 206, respectively, and a main fuel nozzle 108 in fluid communication with a main fuel circuit 208. The fuel injector 100B may also include a by-pass fuel circuit 230 connected between the primary circuit 204 and the secondary circuit 206 and/or the main circuit 208, and a by-pass valve 232 provided operably in association with the by-pass fuel circuit 230. The by-pass valve 232 is configured to be opened such that a portion of the fuel flowing through the primary fuel circuit 204 from the primary fuel manifold is directed to the secondary fuel circuit 206 and/or the main fuel circuit 208.SELECTED DRAWING: Figure 6
申请公布号 JP2016109129(A) 申请公布日期 2016.06.20
申请号 JP20150234386 申请日期 2015.12.01
申请人 GENERAL ELECTRIC CO <GE> 发明人 PATEL NAYAN VINODBHAI;MANCINI ALFRED ALBERT;THOMSEN DUANE DOUGLAS
分类号 F02C7/228;F02C7/22;F02C9/28;F02C9/40 主分类号 F02C7/228
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