Invention Grant
- Patent Title: Turbomachine combustion chamber having a perforated chamber end wall and with no deflector
- Patent Title (中): 涡轮机燃烧室具有穿孔室端壁并且没有偏转器
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Application No.: US13636873Application Date: 2011-03-23
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Publication No.: US09383106B2Publication Date: 2016-07-05
- Inventor: Thierry Cortes
- Applicant: Thierry Cortes
- Applicant Address: FR Paris
- Assignee: SNECMA
- Current Assignee: SNECMA
- Current Assignee Address: FR Paris
- Agency: Oblon, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR1052244 20100326
- International Application: PCT/FR2011/050622 WO 20110323
- International Announcement: WO2011/117543 WO 20110929
- Main IPC: F23R3/10
- IPC: F23R3/10 ; F23R3/04 ; F23R3/12 ; F23R3/06 ; F23R3/00 ; F23R3/50

Abstract:
An annular combustion chamber for a turbomachine, including an external wall and an internal wall which are oriented substantially axially relative to the rotation axis of the turbomachine, the combustion chamber being closed upstream by a chamber end wall oriented substantially radially, the chamber being supplied with compressed air coming from a compressor via a nozzle, the output direction of which is offset radially relative to the mid-axis of the combustion chamber, the chamber end wall including cooling air supply holes inclined to the direction normal to the chamber end wall. The number of holes oriented radially in the direction opposite to that where the outlet of the nozzle is located is greater than the number of holes oriented radially in the direction of the outlet of the nozzle.
Public/Granted literature
- US20130008166A1 TURBOMACHINE COMBUSTION CHAMBER HAVING A CENTRIFUGAL COMPRESSOR WITH NO DEFLECTOR Public/Granted day:2013-01-10
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