Invention Grant
- Patent Title: Turbine blade with trailing edge tip corner cooling
- Patent Title (中): 涡轮叶片具有后缘尖角冷却
-
Application No.: US11900037Application Date: 2007-09-07
-
Publication No.: US08011889B1Publication Date: 2011-09-06
- Inventor: George Liang
- Applicant: George Liang
- Applicant Address: US FL Jupiter
- Assignee: Florida Turbine Technologies, Inc.
- Current Assignee: Florida Turbine Technologies, Inc.
- Current Assignee Address: US FL Jupiter
- Agent John Ryznic
- Main IPC: F01D5/20
- IPC: F01D5/20

Abstract:
A turbine blade for use in an industrial gas turbine engine, especially for the first stage turbine blade, in which the blade includes a squealer tip with a pressure side tip rail extending all the way top the trailing edge of the tip and a suction side tip rail with a cut back adjacent to the trailing edge to form a cooling air flow path from the squealer pocket and up and over the cut back in the suction side tip rail. The floor of the squealer pocket includes a series of skewed trip strips in the location of the cut back in the tip end, the trip strips being skewed in a direction to direct the cooling air toward the cut back. Rows of film cooling holes extend along the pressure and suction sides of the blade just below the tip rails to provide cooling for the tip rails. Tip cooling holes are located on the squealer pocket floor upstream from the trip strips and along the tip rail walls to provide cooling within the pocket. The skew trip strips begin just upstream from the cut back and extend along the pocket toward the tip end, extending substantially from the pressure side tip rail to the suction side tip rail.
Public/Granted literature
- US2220507A Method for refining organic acids obtained from oxidized hydrocarbons Public/Granted day:1940-11-05
Information query
IPC分类: