Invention Grant
- Patent Title: Annular combustion chamber of a turbomachine
- Patent Title (中): 涡轮机的环形燃烧室
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Application No.: US14124511Application Date: 2012-06-04
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Publication No.: US08925331B2Publication Date: 2015-01-06
- Inventor: Bernard Carrere , Nicolas Savary
- Applicant: Bernard Carrere , Nicolas Savary
- Applicant Address: FR Bordes
- Assignee: Turbomeca
- Current Assignee: Turbomeca
- Current Assignee Address: FR Bordes
- Agency: Oblon, Spivak, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR1154984 20110608
- International Application: PCT/FR2012/051240 WO 20120604
- International Announcement: WO2012/168636 WO 20121213
- Main IPC: F23R3/60
- IPC: F23R3/60 ; F23R3/00

Abstract:
An annular combustion chamber for a turbomachine presenting an axial direction, a radial direction, and an azimuth direction, the combustion chamber including a first annular wall and a second annular wall, each annular wall defining at least a portion of an enclosure of the combustion chamber. The first annular wall and the second annular wall present complementary assembly mechanisms that co-operate by engagement in azimuth.
Public/Granted literature
- US20140109595A1 ANNULAR COMBUSTION CHAMBER OF A TURBOMACHINE Public/Granted day:2014-04-24
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