Invention Grant
- Patent Title: Turbine vane with dusting hole at the base of the blade
- Patent Title (中): 涡轮叶片,叶片底部带有排尘孔
-
Application No.: US13256358Application Date: 2010-03-12
-
Publication No.: US08864444B2Publication Date: 2014-10-21
- Inventor: Serge Louis Antunes , Jacques Auguste Amedee Boury , Patrice Jean-Marc Rosset
- Applicant: Serge Louis Antunes , Jacques Auguste Amedee Boury , Patrice Jean-Marc Rosset
- Applicant Address: FR Paris
- Assignee: Snecma
- Current Assignee: Snecma
- Current Assignee Address: FR Paris
- Agency: Oblon, Spivak, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR0951615 20090313; FR0954375 20090626
- International Application: PCT/EP2010/053212 WO 20100312
- International Announcement: WO2010/103113 WO 20100916
- Main IPC: F01D5/18
- IPC: F01D5/18 ; F01D5/14 ; F01D9/02

Abstract:
A cooled turbine vane for a turbine engine, that includes a blade mounted on a platform carried by a base, the blade including one or more cavities formed therein for cooling air circulation, the cavity extending along the trailing edge and being supplied with cooling air by a supply duct connecting an air intake located in a lower portion of the base and the cavity of the trailing edge by defining a bend within the base. The duct includes, on an axis substantially radial relative to the air intake a bell-shaped niche located under the platform, the niche being open at a top thereof via a dusting hole extending through the platform and being defined at a foot of the base by walls extending substantially radially from the platform to close the platform laterally.
Public/Granted literature
- US20120014810A1 TURBINE VANE WITH DUSTING HOLE AT THE BASE OF THE BLADE Public/Granted day:2012-01-19
Information query