发明名称 AIRFOIL AND METHOD FOR MANAGING PRESSURE AT TIP OF AIRFOIL
摘要 An airfoil includes a squealer tip at an outer radial end of the airfoil. A squealer tip pocket of the squealer tip has a convex side and a concave side, and a tip plate. A divider extends across the tip plate from the concave side to the convex side to divide the squealer tip pocket into a first pocket and a second pocket. At least one cooling passage through the tip plate in the second pocket provides fluid communication through the tip plate from an interior of the airfoil to the second pocket. The first pocket is fluidically disconnected from the interior of the airfoil.
申请公布号 US2016258302(A1) 申请公布日期 2016.09.08
申请号 US201514639374 申请日期 2015.03.05
申请人 General Electric Company 发明人 Benson Adebukola Oluwaseun;De Bellis Lisa;Zhang Xiuzhang James
分类号 F01D5/20;F01D5/02;F01D5/30;F01D5/18 主分类号 F01D5/20
代理机构 代理人
主权项 1. An airfoil comprising: a squealer tip at an outer radial end of the airfoil, a squealer tip pocket of the squealer tip having a convex side and a concave side; a tip plate at the squealer tip; a divider that extends across the tip plate from the concave side to the convex side to divide the squealer tip pocket into a first pocket and a second pocket; and, at least one cooling passage through the tip plate in the second pocket to provide fluid communication through the tip plate from an interior of the airfoil to the second pocket; wherein the first pocket is fluidically disconnected from the interior of the airfoil.
地址 Schenectady NY US