发明授权
US5235805A Gas turbine engine combustion chamber with oxidizer intake flow control
失效
燃气涡轮发动机燃烧室与氧化剂进气流量控制
- 专利标题: Gas turbine engine combustion chamber with oxidizer intake flow control
- 专利标题(中): 燃气涡轮发动机燃烧室与氧化剂进气流量控制
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申请号: US851167申请日: 1992-03-12
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公开(公告)号: US5235805A公开(公告)日: 1993-08-17
- 发明人: Gerard Y. G. Barbier , Xavier M. H. Bardey , Michel A. A. Desaulty , Serge M. Meunier
- 申请人: Gerard Y. G. Barbier , Xavier M. H. Bardey , Michel A. A. Desaulty , Serge M. Meunier
- 申请人地址: FRX Valin
- 专利权人: Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "S.N.E.C.M.A."
- 当前专利权人: Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "S.N.E.C.M.A."
- 当前专利权人地址: FRX Valin
- 优先权: FRX9103374 19910320
- 主分类号: F23R3/04
- IPC分类号: F23R3/04 ; F23R3/26
摘要:
An oxidizer intake flow control system is disclosed for a gas turbine engine combustion chamber. The chamber has an oxidizer intake assembly which extends through the wall of the chamber such that an inlet aperture of the oxidizer intake and an exhaust aperture of the oxidizer intake are located on opposite sides of the wall defining the combustion chamber. An oxidizer intake sleeve defines a central passage through which oxidizer may pass into the combustion chamber. The intake passage extends along a central axis and the intake assembly is attached to the wall of the combustion chamber such that it is rotatable about this central axis. The inlet aperture and/or the exhaust aperture is located in a plane extending non-perpendicularly to the central axis. The combustion chamber may have several oxidizer intake assemblies extending through the combustion chamber walls. The intake assemblies may be interconnected such that they may be simultaneously rotated with respect to the combustion chamber wall.
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