Invention Grant
- Patent Title: Turbine nozzle guide vane assembly in a turbomachine
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Application No.: US14115980Application Date: 2012-05-04
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Publication No.: US09599020B2Publication Date: 2017-03-21
- Inventor: Denis Jean Maurice Sandelis , Didier Hippolyte Hernandez
- Applicant: Denis Jean Maurice Sandelis , Didier Hippolyte Hernandez
- Applicant Address: FR Paris
- Assignee: SNECMA
- Current Assignee: SNECMA
- Current Assignee Address: FR Paris
- Agency: Oblon, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR1153928 20110506
- International Application: PCT/FR2012/051000 WO 20120504
- International Announcement: WO2012/153049 WO 20121115
- Main IPC: F01D9/04
- IPC: F01D9/04 ; F02C7/12 ; F01D9/02 ; F01D5/18 ; F01D5/30

Abstract:
A sectorized nozzle for a turbine engine turbine including an inner sectorized annular platform and an outer sectorized annular platform connected together by radial airfoils, at least one of the platforms including a plurality of orifices for passing air in a neighborhood of its upstream end, the orifices being distributed over the circumference of the platform and opening out at their ends remote from the airfoils into a circumferential annular cavity of the sector of the platform, which cavity is closed by a metal sheet fastened to the platform sector and pierced by orifices for feeding cooling air.
Public/Granted literature
- US20140116065A1 TURBINE NOZZLE GUIDE IN A TURBINE ENGING Public/Granted day:2014-05-01
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