发明名称 SWIRLER MOUNT INTERFACE FOR GAS TURBINE ENGINE COMBUSTOR
摘要 A swirler is provided for a gas turbine engine. The swirler includes a swirler body with a threaded section and a multiple of circumferentially arranged tabs operable to flex radially outward. The multiple of circumferentially arranged tabs are radially displaced from the threaded section.
申请公布号 WO2015017002(A2) 申请公布日期 2015.02.05
申请号 WO2014US38198 申请日期 2014.05.15
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 DRAKE, CHRISTOPHER;MAX, SETH A.;HARRIS, MEGGAN
分类号 F02C7/22;F23R3/28 主分类号 F02C7/22
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