- 专利标题: Injection system for a turbine engine combustion chamber configured for direct injection of two coaxial fuel flows
-
申请号: US14750347申请日: 2015-06-25
-
公开(公告)号: US09989256B2公开(公告)日: 2018-06-05
- 发明人: Denis Jean Maurice Sandelis , Romain Nicolas Lunel
- 申请人: SNECMA
- 申请人地址: FR Paris
- 专利权人: SNECMA
- 当前专利权人: SNECMA
- 当前专利权人地址: FR Paris
- 代理机构: Oblon, McClelland, Maier & Neustadt, L.L.P.
- 优先权: FR1455906 20140625
- 主分类号: F23R3/14
- IPC分类号: F23R3/14 ; F23R3/36 ; F23R3/28 ; F23C7/00 ; F23R3/34 ; F02C7/22
摘要:
An injection system for a turbine engine combustion chamber is provided. The injection system includes a first annular deflector surrounded by the bowl of the injection system and extending in the downstream direction from the downstream transverse surface that delimits the downstream side of the swirler. The first deflector has a free downstream end offset in the upstream direction from a downstream end of the bowl, so as to guide an air film output from the first orifices formed through the bowl. The internal radius of the cross section of the first annular deflector increases from the downstream transverse surface as far as the downstream end of the first annular deflector.
公开/授权文献
信息查询