GAS TURBINE ENGINE COMPONENT COOLING PASSAGE TURBULATOR
摘要
A gas turbine engine component includes opposing walls that provide an interior cooling passage. One of the walls has a turbulator with a hook that is enclosed within the walls.
申请公布号
WO2015077017(A1)
申请公布日期
2015.05.28
申请号
WO2014US64011
申请日期
2014.11.05
申请人
UNITED TECHNOLOGIES CORPORATION
发明人
SNYDER, BROOKS E.;SLAVENS, THOMAS N.;LORICCO, NICHOLAS M.;AUXIER, JAMES T.
