公开(公告)号：US5437159A

公开(公告)日：1995-08-01

申请号：US260727

申请日：1994-06-15

申请人： Denis R. H. Ansart ,  Jacques L. M. Maunand

发明人： Denis R. H. Ansart ,  Jacques L. M. Maunand

IPC分类号： F23R3/20 ,  F23R3/28

CPC分类号： F23R3/28 ,  F23R3/20

摘要： A fuel injection system for a gas turbine engine combustion chamber is disclosed having a sleeve defining a passageway extending along a longitudinal axis of a combustion zone, a first fuel injector orifice to inject fuel into the passageway, and second fuel injector holes arranged in a plurality of substantially linear arrays extending radially from the sleeve and angularly equidistantly spaced from each other, the second fuel injection holes located in a plane extending substantially perpendicular to the longitudinal axis of the combustion chamber such that the plane is located axially between an upstream end wall of the combustion chamber and the downstream end of the sleeve. The system also includes a flameholder having a plurality of flameholder arms extend axially from second fuel injection arms such that the downstream ends of the flameholder arms extend to at least the downstream end of the sleeve and extend generally radially from the sleeve such that the flameholder arms are circumferentially located between the angularly spaced apart linear arrays of fuel injection holes.

摘要翻译： 公开了一种用于燃气涡轮发动机燃烧室的燃料喷射系统，其具有限定沿着燃烧区的纵向轴线延伸的通道的套筒，用于将燃料喷射到通道中的第一燃料喷射器孔，以及多个排列成多个的第二燃料喷射器孔 基本上线性的阵列从套管径向延伸并且彼此角度等距离地间隔开，第二燃料喷射孔位于基本上垂直于燃烧室的纵向轴线延伸的平面中，使得平面轴向位于 燃烧室和套筒的下游端。 该系统还包括具有多个从第二燃料喷射臂轴向延伸的火焰稳定器臂的火焰稳定器臂，使得火焰稳定器臂的下游端部至少延伸到套筒的下游端并且大致径向地从套筒延伸，使得火焰控制器臂 周向地位于燃料喷射孔的角度间隔开的线性阵列之间。

公开(公告)号：US5285630A

公开(公告)日：1994-02-15

申请号：US978819

申请日：1992-11-19

申请人： Denis R. H. Ansart ,  Gerard J. P. Bayle Laboure ,  Jacques L. M. Maunand ,  Denis J. M. Sandelis

发明人： Denis R. H. Ansart ,  Gerard J. P. Bayle Laboure ,  Jacques L. M. Maunand ,  Denis J. M. Sandelis

IPC分类号： F23R3/04 ,  F23R3/26 ,  F02C9/16

CPC分类号： F23R3/26 ,  F23R3/04 ,  Y02T50/675

摘要： A system for reducing nitrogen oxide emissions from a gas turbine engine is disclosed in which a portion of air in the air compressor is tapped and supplied to an inlet which introduces at least a portion of the tapped air into the primary zone of the combustion chamber. A control device is disposed between the tap and the inlet to control the air flow passing to the inlet. The inlet is located so as to inject the tapped air into the combustion chamber primary zone at the intersection of adjacent fuel sprays. The control device, which may be an adjustable flap valve or a three-way valve, may also be operatively connected to the throttle control for the gas turbine engine such that the control allows the maximum amount of air to pass into the combustion chamber under full power conditions. The control device is preferably mounted outside the engine casing enclosing the combustion chamber to allow easy access for assembly and maintenance.

摘要翻译： 本发明涉及一种涡轮发动机，其包括由相同空气流连续进给的压缩机（1），燃烧室（2）和涡轮机（3），并且还包括适于减少所述氮气氧化物形成的装置 燃烧室。 该装置包括用于取出由压缩机（1）输送的空气的一部分的装置（9a，9b），用于引入在从两个相邻碗排出的燃料锥体的交点处获取的一部分空气的装置（21） 以及用于控制作为发动机转速的函数的在燃料圆锥的交点处引入的空气流的控制装置（10）。