Invention Grant
- Patent Title: Compressor casing comprising cavities having an optimised upstream shape
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Application No.: US14391080Application Date: 2013-04-15
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Publication No.: US09638213B2Publication Date: 2017-05-02
- Inventor: Thierry Jean-Jacques Obrecht , Olivier Stephane Domercq
- Applicant: SNECMA
- Applicant Address: FR Paris
- Assignee: SNECMA
- Current Assignee: SNECMA
- Current Assignee Address: FR Paris
- Agency: Oblon, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR1201160 20120419
- International Application: PCT/FR2013/050829 WO 20130415
- International Announcement: WO2013/156726 WO 20131024
- Main IPC: F04D29/54
- IPC: F04D29/54 ; F04D27/02 ; F04D29/16 ; F04D29/52 ; F04D29/68 ; F04D17/10 ; F04D19/00 ; F04D29/42

Abstract:
A casing for a turbine engine compressor, including: cavities in a thickness of the casing, extending in parallel to one another from an inner face of the casing along a circumference thereof, the cavities not being in communication with one another. The cavities, which are elongate and extend along a main direction of orientation between two side walls, are closed upstream and downstream by upstream and downstream faces respectively, and an upstream border and a downstream border are formed at the intersections between same and the inner face of the casing. The upstream border of the cavities takes a form of a wavy line including at least two alternate undulations over a length thereof between the side walls.
Public/Granted literature
- US20150078889A1 COMPRESSOR CASING COMPRISING CAVITIES HAVING AN OPTIMISED UPSTREAM SHAPE Public/Granted day:2015-03-19
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