发明名称 FUEL LANCE COOLING FOR A GAS TURBINE WITH SEQUENTIAL COMBUSTION
摘要 The present invention relates to a fuel lancet (21, 32, 38, 49) to inject gas and/or liquid fuel. The fuel lancet (21, 32, 38, 49) comprises at least one finger (22, 35, 29, 52), and the at least one finger (22, 35, 39, 52) has a streamlined body. The body has two side surfaces and a plurality of nozzles (27, 36, 44, 53) are disposed along the edges (24, 41, 62) of a rear end. Moreover, means (28, 37, 45, 54) for improving mixing quality and reducing a loss of pressure are provided to the edge area of the body.
申请公布号 KR20160060565(A) 申请公布日期 2016.05.30
申请号 KR20150161568 申请日期 2015.11.18
申请人 GENERAL ELECTRIC TECHNOLOGY GMBH 发明人 GAO XIANFENG;BENZ URS;THEUER ANDRE;DUESING MICHAEL
分类号 F23R3/28;F23D14/22;F23D14/32;F23R3/34 主分类号 F23R3/28
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