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
EP3090145(A1)
申请公布日期
2016.11.09
申请号
EP20140863499
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.
