发明名称 INJECTOR WITH INTEGRATED RESONATOR
摘要 The system may include a turbine engine. The turbine engine may include a fuel nozzle. The fuel nozzle may include an air path. The fuel nozzle may also include a fuel path such that the fuel nozzle is in communication with a combustion zone of the turbine engine. Furthermore, the fuel nozzle may include a resonator. The resonator may be disposed in the fuel nozzle directly adjacent to the combustion zone.
申请公布号 US2011179795(A1) 申请公布日期 2011.07.28
申请号 US20090499777 申请日期 2009.07.08
申请人 GENERAL ELECTRIC COMPANY 发明人 JOHNSON THOMAS EDWARD;ZIMINSKY WILLY STEVE;YORK WILLIAM DAVID;STEVENSON CHRISTIAN XAVIER
分类号 F02C7/24 主分类号 F02C7/24
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