Invention Grant
- Patent Title: Cooled vane of a high-pressure turbine
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Application No.: US14427295Application Date: 2013-09-12
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Publication No.: US09657579B2Publication Date: 2017-05-23
- Inventor: Erwan Daniel Botrel , Charlotte Marie Dujol
- Applicant: SNECMA
- Applicant Address: FR Paris
- Assignee: SNECMA
- Current Assignee: SNECMA
- Current Assignee Address: FR Paris
- Agency: Blakely Sokoloff Taylor & Zafman LLP
- Priority: FR1258626 20120913
- International Application: PCT/FR2013/052102 WO 20130912
- International Announcement: WO2014/041311 WO 20140320
- Main IPC: F01D5/08
- IPC: F01D5/08 ; F01D5/18

Abstract:
The invention relates to a movable vane of a turbomachine comprising a blade (12) with inner cooling cavities and a root (11) by which means the vane can be mounted on a rotor disk, the root comprising at least two channels (11a) communicating with said inner cavities and leading to the base (11b) thereof, said base comprising at least two openings (11b1, 11b2) through which the channels open up, and a calibrating plate (20) provided with calibrated perforations (21, 22) corresponding to said openings being attached to the base (11b) of the root. The vane is characterized in that a mechanical means (25, 26; 11m1, 11m2) forming a sealing barrier between the two openings is arranged between the plate and the base of the root.
Public/Granted literature
- US20150240649A1 COOLED VANE OF A HIGH-PRESSURE TURBINE Public/Granted day:2015-08-27
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