Invention Application
- Patent Title: Turbine blade with recessed squealer tip and shelf
- Patent Title (中): 涡轮叶片具有凹陷的尖叫和架子
-
Application No.: US10408293Application Date: 2003-04-07
-
Publication No.: US20040197190A1Publication Date: 2004-10-07
- Inventor: Philip Francis Stec , Daniel Edward Demers , Richard Ludwig Schmidt
- Main IPC: F01D005/08
- IPC: F01D005/08

Abstract:
A turbine blade squealer tip has a continuous squealer tip wall extending radially outwardly from and continuously around a tip cap. A recessed tip wall portion of the tip wall is recessed inboard from a pressure side of an airfoil outer wall of an airfoil of the blade forming a tip shelf therebetween. A plurality of film cooling shelf holes are disposed through the tip shelf to an internal cooling circuit of the blade and are spaced away from a junction between the recessed tip wall portion and the tip shelf. The exemplary embodiment of the airfoil includes shelf hole centerlines of the holes passing through pierce points in the shelf. At least a majority of the shelf hole centerlines are angled in outboard directions away from and outboard of the squealer tip wall. A majority of centerlines are angled away from vertical lines passing through the pierce points at first component angles in a range between 2 degrees and 16 degrees.
Public/Granted literature
- US06991430B2 Turbine blade with recessed squealer tip and shelf Public/Granted day:2006-01-31
Information query