发明名称 Aerodynamic pylon fuel injector system for combustors
摘要 A combustor system includes a pylon fuel injection system (40) coupled to a combustion chamber (12, 18) and configured to inject fuel to the combustion chamber (12, 18). The pylon fuel injection system (40) includes a plurality of radial elements (42), each radial element (42) having a plurality of first Coanda type fuel injection slots (46). A plurality of transverse elements (44) are provided to each radial element (42). Each transverse element (44) includes a plurality of second Coanda type fuel injection slots (50).
申请公布号 EP2295860(A3) 申请公布日期 2014.10.01
申请号 EP20100171758 申请日期 2010.08.03
申请人 GENERAL ELECTRIC COMPANY 发明人 BUNKER, RONALD SCOTT
分类号 F23D14/64;F23R3/20;F23R3/28 主分类号 F23D14/64
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