发明授权
- 专利标题: Air-fuel injection system for a turbojet engine
- 专利标题(中): 涡轮喷气发动机的空气燃料喷射系统
-
申请号: US79149申请日: 1987-07-29
-
公开(公告)号: US4809512A公开(公告)日: 1989-03-07
- 发明人: Gerard Y. G. Barbier , Gerard J. P. Bayle-Laboure , Michael A. A. Desaulty , Rodolphe Martinez , Jerome Perigne
- 申请人: Gerard Y. G. Barbier , Gerard J. P. Bayle-Laboure , Michael A. A. Desaulty , Rodolphe Martinez , Jerome Perigne
- 申请人地址: FRX Paris
- 专利权人: Societe Nationale d'Etude et de Construction de Moteurs d-Aviation (SNECMA)
- 当前专利权人: Societe Nationale d'Etude et de Construction de Moteurs d-Aviation (SNECMA)
- 当前专利权人地址: FRX Paris
- 优先权: FRX8611011 19860730
- 主分类号: F23R3/26
- IPC分类号: F23R3/26 ; F02C1/00
摘要:
An improved swirler system for a turbojet engine combustion chamber is disclosed in which stationary first vanes and moveable second vanes are oriented at different angles with respect to a radius of the fuel injector system. The different angles allow the angle of the incoming air to be adjusted between full power and idle conditions so as to vary the conial shape of the atomized air-fuel mixture according to the operating conditions of the engine. Radial and axial inlet duct portions serve to attenuate the wakes of the air flow generated by the vanes prior to the air passing into the combustion chamber.
公开/授权文献
信息查询