发明名称 FUEL SUPPLY SYSTEM FOR A GAS TURBINE ENGINE
摘要 In one aspect, a fuel supply system may include a fuel injector (100) 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 may also define a by-pass fuel circuit (230) connected between the primary circuit and the secondary circuit and/or the main circuit. The system may also include a primary fuel manifold configured to be fluidly connected to the primary pilot fuel nozzle via the primary fuel circuit. Moreover, the system may include a by-pass valve provided in operative association with the by-pass fuel circuit. The by-pass valve may be configured to be opened such that a portion of the fuel flowing through the primary circuit from the primary fuel manifold is directed to the secondary circuit and/or the main circuit.
申请公布号 EP3029374(A1) 申请公布日期 2016.06.08
申请号 EP20150197254 申请日期 2015.12.01
申请人 GENERAL ELECTRIC COMPANY 发明人 PATEL, NAYAN VINODBHAI;MANCINI, ALFRED ALBERT;THOMSEN, DUANE DOUGLAS
分类号 F23K5/06;F02C7/232;F02C7/262;F02C9/34 主分类号 F23K5/06
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