发明名称 S-SHAPED TRIP STRIPS IN INTERNALLY COOLED COMPONENTS
摘要 A component for a gas turbine engine is provided. The component includes an internal cooling passage disposed within the component, and an s-shaped trip strip formed on a surface of the internal cooling passage.
申请公布号 US2016237849(A1) 申请公布日期 2016.08.18
申请号 US201514622062 申请日期 2015.02.13
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 King Christopher;Pietraszkiewicz Edward F.
分类号 F01D25/12;F02C7/18;F02C7/24;F01D5/18 主分类号 F01D25/12
代理机构 代理人
主权项 1. A component for a gas turbine engine, comprising: an internal cooling passage disposed within the component; and an s-shaped trip strip formed on a surface of the internal cooling passage.
地址 Hartford CT US