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18 条记录 (耗时 0.016 秒)

    Cyclone combustor
    1.
    发明授权
    Cyclone combustor 有权
    旋风燃烧器

    公开(公告)号：US06543231B2

    公开(公告)日：2003-04-08

    申请号：US09903636

    申请日：2001-07-13

    申请人： Peter John Stuttaford ,  Aleksandar Kojovic

    发明人： Peter John Stuttaford ,  Aleksandar Kojovic

    IPC分类号： F02C300

    CPC分类号： F23R3/346 ,  F23D2900/00014 ,  F23R3/286 ,  F23R3/58 ,  F23R2900/03044

    摘要： A cyclone combustor of the present invention uses a novel pre-mixture injection scheme to optimize performance. The cyclone combustor includes a cylindrical combustor can and three fuel/air premixing tubes entering the combustor can radially, with a tangential offset. The tangential offset is designed to provide an optimized circulation in the combustor can for improvement of liner life span, flame stability and engine turn-down. The ignition and pilot fuel systems are placed to take advantage of the premixing tube entry locations and the tangential direction of the mixture flow momentum in the combustor can. The special combination of the parallel axes of the combustor can and the mixing tubes provides a right angle between an outlet section and the major tube section of each premixing tube. The cyclone combustor of the present invention can meet the requirements for low NOx and CO emissions.

    摘要翻译： 本发明的旋风式燃烧器采用新颖的预混合喷射方案来优化性能。 旋风燃烧器包括圆柱形燃烧器罐和三个燃料/空气预混合管，其径向进入燃烧室，具有切向偏移。 切向偏移被设计成在燃烧室中提供优化的循环，以改善衬套使用寿命，火焰稳定性和发动机熄灯。 点火和引燃燃料系统被放置以利用预混合管入口位置和燃烧器罐中混合物流动动量的切向。 燃烧器罐的平行轴和混合管的特殊组合在出口部分和每个预混合管的主管部分之间提供直角。 本发明的旋风式燃烧器可以满足低NOx和CO排放的要求。

    Apparatus for adjusting combustor cycle
    2.
    发明授权
    Apparatus for adjusting combustor cycle 有权
    用于调节燃烧器循环的装置

    公开(公告)号：US06609362B2

    公开(公告)日：2003-08-26

    申请号：US09903641

    申请日：2001-07-13

    申请人： Peter John Stuttaford ,  Aleksandar Kojovic

    发明人： Peter John Stuttaford ,  Aleksandar Kojovic

    IPC分类号： F23R306

    CPC分类号： F23R3/005 ,  F02C7/08 ,  F05D2260/201 ,  F23R3/26 ,  F23R2900/00016 ,  F23R2900/03044

    摘要： A method of combustor cycle air flow adjustment for a gas turbine engine according to the present invention solves the problem of a higher flame temperature in the combustor, thereby affecting the emission levels when a heat-recuperated air flow cycle is used to increase the compressed air temperature. In low emission combustors this impact is severe because emission levels are significantly dependent on the primary combustion zone flame temperature. The method of the present invention includes a step of changing a geometry of an air flow passage and thereby changing distribution of a total air mass flow between an air mass flow for combustion and an air mass flow for cooling in order to ensure that flame temperature in a primary combustion zone of a combustor are maintained substantially the same whether the gas turbine engine is manufactured to operate as a simple air flow cycle engine or as a heat-recuperated air flow cycle engine. In an embodiment of the present invention, the changing of the geometry of the air flow passage by changing the number and size of perforations in an impingement cooling skin so that with minimal changes the impingement cooling skin serves duel purposes both as a cooling device for cooling the combustor wall and as a valve means for combustor cycle air flow adjustment, which makes the method simple and economical.

    摘要翻译： 根据本发明的用于燃气涡轮发动机的燃烧器循环空气流量调节方法解决了燃烧器中火焰温度较高的问题，从而当使用热回收空气流循环来增加压缩空气时影响排放水平 温度。 在低排放燃烧器中，这种影响是严重的，因为排放水平显着取决于主燃烧区火焰温度。 本发明的方法包括改变空气流路的几何形状，从而改变用于燃烧的空气质量流与冷却空气质量流之间的总空气质量流的分布，以确保火焰温度在 无论燃气涡轮发动机是否被制造成作为简单的气流循环发动机或作为热回收空气流循环发动机来操作，燃烧器的主燃烧区域保持基本相同。 在本发明的一个实施例中，通过改变冲击冷却皮肤中的穿孔的数量和尺寸来改变空气流动通道的几何形状，使得在最小变化的情况下，冲击冷却皮肤作为用于冷却的冷却装置的决斗 燃烧器壁和用于燃烧器循环空气流量调节的阀装置，这使得该方法简单和经济。

    Method of combustor cycle airflow adjustment
    3.
    发明授权
    Method of combustor cycle airflow adjustment 有权
    燃烧器循环气流调节方法

    公开(公告)号：US06745571B2

    公开(公告)日：2004-06-08

    申请号：US10421751

    申请日：2003-04-24

    申请人： Peter John Stuttaford ,  Aleksandar Kojovic

    发明人： Peter John Stuttaford ,  Aleksandar Kojovic

    IPC分类号： F23R306

    CPC分类号： F23R3/005 ,  F02C7/08 ,  F05D2260/201 ,  F23R3/26 ,  F23R2900/00016 ,  F23R2900/03044

    摘要： A method of combustor cycle air flow adjustment for a gas turbine engine according to the present invention solves the problem of a higher flame temperature in the combustor, thereby affecting the emission levels when a heat-recuperated air flow cycle is used to increase the compressed air temperature. In low emission combustors this impact is severe because emission levels are significantly dependent on the primary combustion zone flame temperature. The method of the present invention includes a step of changing a geometry of an air flow passage and thereby changing distribution of a total air mass flow between an air mass flow for combustion and an air mass flow for cooling in order to ensure that flame temperature in a primary combustion zone of a combustor are maintained substantially the same whether the gas turbine engine is manufactured to operate as a simple air flow cycle engine or as a heat-recuperated air flow cycle engine. In an embodiment of the present invention, the changing of the geometry of the air flow passage by changing the number and size of perforations in an impingement cooling skin so that with minimal changes the impingement cooling skin serves duel purposes both as a cooling device for cooling the combustor wall and as a valve means for combustor cycle air flow adjustment, which makes the method simple and economical.

    摘要翻译： 根据本发明的用于燃气涡轮发动机的燃烧器循环空气流量调节方法解决了燃烧器中火焰温度较高的问题，从而当使用热回收空气流循环来增加压缩空气时影响排放水平 温度。 在低排放燃烧器中，这种影响是严重的，因为排放水平显着取决于主燃烧区火焰温度。 本发明的方法包括改变空气流路的几何形状，从而改变用于燃烧的空气质量流与冷却空气质量流之间的总空气质量流的分布，以确保火焰温度在 无论燃气涡轮发动机是否被制造成作为简单的气流循环发动机或作为热回收空气流循环发动机来操作，燃烧器的主燃烧区域保持基本相同。 在本发明的一个实施例中，通过改变冲击冷却皮肤中的穿孔的数量和尺寸来改变空气流动通道的几何形状，使得在最小变化的情况下，冲击冷却皮肤作为用于冷却的冷却装置的决斗 燃烧器壁和用于燃烧器循环空气流量调节的阀装置，这使得该方法简单和经济。

    FUEL MANIFOLD WITH JUMPER TUBES
    4.
    发明申请
    FUEL MANIFOLD WITH JUMPER TUBES 有权
    燃油管与喷枪管

    公开(公告)号：US20130152590A1

    公开(公告)日：2013-06-20

    申请号：US13331752

    申请日：2011-12-20

    申请人： Aleksandar Kojovic ,  Saeid Oskooel ,  Bryan Bond

    发明人： Aleksandar Kojovic ,  Saeid Oskooel ,  Bryan Bond

    IPC分类号： F23R3/28

    CPC分类号： F23R3/20 ,  F02C7/222 ,  F05D2300/501 ,  F23R3/283

    摘要： A gas turbine engine fuel delivery system which includes an external fuel manifold fastened to the outer surface of a casing surrounding the combustor of the engine and which includes a plurality of inlet manifold tubes circumferentially disposed in serial flow communication. A plurality of fuel nozzles are mounted to the casing and are axially spaced apart from the fuel manifold on the outer surface of the casing. A plurality of jumper tubes are disposed outside the casing and feed fuel flow from the fuel manifold to the fuel nozzles. The jumper tubes have a rigidity that is less than that of the inlet manifold tubes of the fuel manifold such that the jumper tubes elastically deflect under load.

    摘要翻译： 一种燃气涡轮发动机燃料输送系统，其包括紧固在围绕发动机的燃烧器的壳体的外表面的外部燃料歧管，并且包括多个沿串联流动连通的周向设置的入口歧管管。 多个燃料喷嘴安装到壳体上并且与壳体的外表面上的燃料歧管轴向间隔开。 多个跨接管设置在壳体外部，并且将燃料流从燃料歧管送到燃料喷嘴。 跳线管具有小于燃料歧管的入口歧管管的刚度，使得跳线管在负载下弹性偏转。