发明授权
- 专利标题: Aerodynamic fuel injection system for a gas turbine engine
- 专利标题(中): 用于燃气涡轮发动机的气动燃料喷射系统
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申请号: US939084申请日: 1997-09-26
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公开(公告)号: US6035645A公开(公告)日: 2000-03-14
- 发明人: Mehdi Bensaadi , Michel Andre Albert Desaulty , Sebastien Pierre Jean Pitrou , Pierre Marie Victor Emile Schroer
- 申请人: Mehdi Bensaadi , Michel Andre Albert Desaulty , Sebastien Pierre Jean Pitrou , Pierre Marie Victor Emile Schroer
- 申请人地址: FRX
- 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
- 优先权: FRX9611702 19960926
- 主分类号: F02C7/232
- IPC分类号: F02C7/232 ; F02C7/22 ; F23R3/14 ; F23R3/22 ; F23R3/26 ; F23R3/28
摘要:
A fuel injection system is disclosed for a gas turbine engine having a fuel injector issuing a primary fuel flow during all operating modes of the gas turbine engine and a secondary fuel flow when operating parameters of the gas turbine engine exceed predetermined values. The fuel injection system includes a first air swirler, a second air swirler located rearwardly of the first air swirler and a venturi having a wall with a converging-diverging inner wall surface forming a venturi throat, the venturi being located such that the wall separates first and second air flows issuing from the first and second air swirlers and such that the primary fuel flow emanating from the fuel injector in a conical configuration does not impact against the inner wall surface of the venturi.
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