发明名称 Turbulator for a turbine airfoil cooling passage
摘要 A turbulator used in a turbine blade of a gas turbine engine, the turbulators arranged along a wall of the cooling air passage in an inverted V-shape with a diffusion slot between adjacent turbulators. The turbulators have a frontal surface and a top surface that are both substantially flat, and in which both have an increasing width and height in the direction from the passage side wall toward the slot. The turbulators have an end face forming the slot that is substantially flat, and because of the slanted angle of the adjacent turbulators forms the divergent opening or slot between adjacent end faces.
申请公布号 US7637720(B1) 申请公布日期 2009.12.29
申请号 US20060600446 申请日期 2006.11.16
申请人 FLORIDA TURBINE TECHNOLOGIES, INC. 发明人 LIANG GEORGE
分类号 F01D5/18 主分类号 F01D5/18
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