发明名称 TURBINE AIRFOIL WITH VARIABLE AND COMPOUND FILLET
摘要 A turbine airfoil may be a rotating blade having a single platform, or a stationary nozzle having a pair of platforms. The airfoil body has pressure and suction sidewalls extending between leading and trailing edges. A compound fillet is disposed between the airfoil body and at least one of the platforms. The compound fillet includes a concave first fillet having a first radius, and a concave second fillet having a second, greater radius. The second fillet extends from the leading edge downstream along the suction sidewall and terminates at a point upstream of the trailing edge. The second fillet may also extend downstream from the leading edge along the pressure sidewall.
申请公布号 US2006275112(A1) 申请公布日期 2006.12.07
申请号 US20050160010 申请日期 2005.06.06
申请人 GENERAL ELECTRIC COMPANY 发明人 LEE CHING-PANG;GUENTERT JOSEPH M.;BAILEY JAMES R.
分类号 F01D9/00 主分类号 F01D9/00
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