发明名称 TURBOMACHINE NOZZLE
摘要 A turbomachine includes a compressor, a turbine, a combustor operatively coupled to the compressor and the turbine, and an injection nozzle assembly mounted in the combustor. The injection nozzle assembly includes a swirler member provided with a hub portion having an internal surface. The injection nozzle assembly also includes a nozzle section, and a nozzle tip member fluidly coupled to the nozzle section and the swirler member. The nozzle tip member includes a body having a first end section that extends from the nozzle section to a second end section arranged in the hub portion of the swirler member. The nozzle tip member includes an external surface, and a discharge port. At least one of the external surface of the nozzle tip member and the internal surface of the swirler member hub portion is provided with a plurality of grooves.
申请公布号 US2011162377(A1) 申请公布日期 2011.07.07
申请号 US20100683102 申请日期 2010.01.06
申请人 GENERAL ELECTRIC COMPANY 发明人 BENJAMIN MARC LIONEL;ROMIG BRYAN WESLEY;SIMONS DERRICK WALTER;STOIA LUCAS JOHN
分类号 F02C7/22 主分类号 F02C7/22
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