发明名称 DILUTION PASSAGE ARRANGEMENT FOR GAS TURBINE ENGINE COMBUSTOR
摘要 A liner panel is provided for use in a combustor of a gas turbine engine. The liner panel includes a major dilution passage having a lip and a first seal boss. The liner panel also includes a minor dilution passage having a second seal boss adjacent the first seal boss.
申请公布号 WO2015147932(A3) 申请公布日期 2015.11.26
申请号 WO2014US71615 申请日期 2014.12.19
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 EASTWOOD, JONATHAN J.;MOURA, DENNIS M.;BOULDIN, LEE E.;PACHECO-TOUGAS, MONICA
分类号 F23R3/02;F23M5/00;F23R3/04;F23R3/26 主分类号 F23R3/02
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