发明授权
- 专利标题: Fuel/oxidizer premixing combustion chamber
- 专利标题(中): 燃料/氧化剂预混合燃烧室
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申请号: US44388申请日: 1993-04-08
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公开(公告)号: US5341645A公开(公告)日: 1994-08-30
- 发明人: Denis R. H. Ansart , Michel A. A. Desaulty , Denis J. M. Sandelis
- 申请人: Denis R. H. Ansart , Michel A. A. Desaulty , Denis J. M. Sandelis
- 申请人地址: FRX Paris
- 专利权人: Societe National d'Etude et de Construction de Moteurs d'Aviation (S.N.E.C.M.A.)
- 当前专利权人: Societe National d'Etude et de Construction de Moteurs d'Aviation (S.N.E.C.M.A.)
- 当前专利权人地址: FRX Paris
- 优先权: FRX9204281 19920408
- 主分类号: F23R3/20
- IPC分类号: F23R3/20 ; F23R3/30 ; F02C1/00 ; F02G3/00
摘要:
A fuel/oxidizer pre-mixing combustion chamber for a turbojet engine is disclosed in which the pre-mixing device is incorporated into the upstream end wall structure of the combustion chamber. The upstream end portion of the combustion chamber, which is in communication with the oxidizer, has a plurality of generally radially extending, "V"-shaped members oriented such that the vertex of the "V" shape faces in an upstream direction. These members extend generally radially between the inner and outer walls which define the boundaries of the combustion chamber. The members define upstream edges and downstream edges which are axially the upstream edges. Fuel injectors extend radially inwardly between these members and are axially positioned between the locations of the upstream and downstream edges so as to spray fuel onto the adjacent sides of each of the members. The downstream edges of the members are circumferentially spaced apart so as to define a passage which is in communication with the oxidizer source and the combustion chamber.
公开/授权文献
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