发明申请
US20060059915A1 Effervescence injector for an aero-mechanical system for injecting air/fuel mixture into a turbomachine combustion chamber
有权
用于将空气/燃料混合物喷射到涡轮机燃烧室中的航空机械系统的气泡注射器
- 专利标题: Effervescence injector for an aero-mechanical system for injecting air/fuel mixture into a turbomachine combustion chamber
- 专利标题(中): 用于将空气/燃料混合物喷射到涡轮机燃烧室中的航空机械系统的气泡注射器
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申请号: US11232002申请日: 2005-09-22
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公开(公告)号: US20060059915A1公开(公告)日: 2006-03-23
- 发明人: Victor Furletov , Thomas Noel , Gilles Rollin , Alexander Vasilev , Victor Yagodkin
- 申请人: Victor Furletov , Thomas Noel , Gilles Rollin , Alexander Vasilev , Victor Yagodkin
- 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
- 优先权: FR0410051 20040923
- 主分类号: F02C7/22
- IPC分类号: F02C7/22
摘要:
A fuel injector for an aero-mechanical injection system for injecting an air/fuel mixture into a turbomachine combustion chamber, the injector comprising a main tubular structure of axis XX′ opening out at a downstream end for delivering the air/fuel mixture, a tubular fuel duct that is disposed inside the main structure and that opens out into the main structure via a fuel atomizer plug so as to introduce fuel into the main structure at a pressure PC into the main structure, at least one air feed channel that opens out into the main structure so as to introduce air at a pressure PA therein, and means for injecting into the fuel duct a gas at a pressure PG that is greater than PA and greater than or equal to PC so as to create effervescence in the fuel on being introduced into the main structure.
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