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1.发明授权公开(公告)号：US06560964B2
公开(公告)日：2003-05-13
申请号：US10091940
申请日：2002-03-06
IPC分类号： F23R328
CPC分类号： F23R3/14 , F23D11/107 , F23D2900/11101 , F23R3/30
摘要： A fuel nozzle for dispensing an atomized fluid spray into the combustion chamber of a gas turbine engine. The nozzle includes a body assembly with an inner fuel passage and an annular outer atomizing air passage. The inner fuel passage extends axially along a longitudinal axis to a first terminal end defining a first discharge orifice of the nozzle. The outer air passage extends coaxially with the inner fuel passage along the longitudinal axis to a second terminal end disposed concentrically with the first terminal end and defining a second discharge orifice oriented such that the discharge therefrom impinges on the fuel discharge from the first discharge orifice. An array of turning vanes is disposed within the outer air passage in a circular locus about the longitudinal axis. Each of the vanes is configured generally in the shape of an airfoil and has a pressure side and an opposing suction side. The vanes extend axially from a leading edge surface to a tapering trailing edge surface along a corresponding array of chordal axes, each of axes is disposed at a given turning angle to the longitudinal axis. The suction side of each vane is spaced-apart from a juxtaposing pressure side of an adjacent vane to define a corresponding one of a plurality of aligned air flow channels therebetween. Atomizing air is directed through the air flow channels to be issued from the second discharge orifice as a generally helical flow having a substantial uniform velocity profile.
摘要翻译： 一种用于将雾化的流体喷雾分配到燃气涡轮发动机的燃烧室中的燃料喷嘴。 喷嘴包括具有内部燃料通道和环形外部雾化空气通道的主体组件。 内部燃料通道沿着纵向轴线延伸到限定喷嘴的第一排出孔的第一终端。 外部空气通道沿着纵向轴线与内部燃料通道同轴地延伸到与第一终端同心设置的第二终端并且限定第二排放孔，其定向成使得其排出物从第一排放孔撞击燃料排放。 旋转叶片阵列围绕纵向轴线设置在外部空气通道内的圆形轨迹中。 每个叶片大体上构成翼型的形状，并且具有压力侧和相对的吸力侧。 叶片从前缘表面沿着相应的弦弦阵列轴向延伸到渐缩的后缘表面，每个轴线以相对于纵向轴线的给定转角设置。 每个叶片的吸入侧与相邻叶片的并置压力侧间隔开，以限定其间的多个对准的空气流动通道中的相应一个。 雾化空气被引导通过空气流动通道，以从第二排放孔排出，作为具有基本均匀速度分布的大致螺旋流。
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2.发明授权公开(公告)号：US06883332B2
公开(公告)日：2005-04-26
申请号：US10421560
申请日：2003-04-23
CPC分类号： F23D11/107 , F23D2900/11101 , F23R3/14 , F23R3/30
摘要： A fuel nozzle for dispensing an atomized fluid spray into the combustion chamber of a gas turbine engine. The nozzle includes a body assembly with an inner fuel passage and an annular outer atomizing air passage. An array of turning vanes is disposed within the outer fuel passage. Each of the vanes is configured generally in the shape of an airfoil in having a pressure side and an opposing suction side, the suction side of each vane being spaced-apart from a juxtaposing pressure side of an adjacent vane to define a corresponding one of a plurality of aligned air flow channels therebetween. Fuel is directed through the fuel flow channels to be issued from the nozzle as a generally helical flow having a substantial uniform velocity profile.
摘要翻译： 一种用于将雾化的流体喷雾分配到燃气涡轮发动机的燃烧室中的燃料喷嘴。 喷嘴包括具有内部燃料通道和环形外部雾化空气通道的主体组件。 转向叶片阵列设置在外部燃料通道内。 每个叶片大体上被构造成具有压力侧和相对的吸力侧的翼型的形状，每个叶片的吸力侧与相邻叶片的并置压力侧隔开，以限定相应的叶片 在它们之间的多个对准的空气流动通道。 燃料被引导通过燃料流动通道以从喷嘴发出，作为具有基本均匀速度分布的大致螺旋流。
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3.发明授权Fuel atomization method for turbine combustion engines having aerodynamic turning vanes 有权具有空气动力学转向叶片的涡轮内燃机的燃料雾化方法公开(公告)号：US06460344B1
公开(公告)日：2002-10-08
申请号：US09532534
申请日：2000-03-22
IPC分类号： F23R328
CPC分类号： F23R3/14 , F23D11/107 , F23D2900/11101 , F23R3/30
摘要： A fuel nozzle for dispensing an atomized fluid spray into the combustion chamber of a gas turbine engine. The nozzle includes a body assembly with an inner fuel passage and an annular outer atomizing air passage. The inner fuel passage extends axially along a longitudinal axis to a first terminal end defining a first discharge orifice of the nozzle. The outer air passage extends coaxially with the inner fuel passage along the longitudinal axis to a second terminal end disposed concentrically with the first terminal end and defining a second discharge orifice oriented such that the discharge therefrom impinges on the fuel discharge from the first discharge orifice. An array of turning vanes is disposed within the outer air passage in a circular locus about the longitudinal axis. Each of the vanes is configured generally in the shape of an airfoil and has a pressure side and an opposing suction side. The vanes extend axially from a leading edge surface to a tapering trailing edge surface along a corresponding array of chordal axes, each of axes is disposed at a given turning angle to the longitudinal axis. The suction side of each vane is spaced-apart from a juxtaposing pressure side of an adjacent vane to define a corresponding one of a plurality of aligned air flow channels therebetween. Atomizing air is directed through the air flow channels to be issued from the second discharge orifice as a generally helical flow having a substantial uniform velocity profile.
摘要翻译： 一种用于将雾化的流体喷雾分配到燃气涡轮发动机的燃烧室中的燃料喷嘴。 喷嘴包括具有内部燃料通道和环形外部雾化空气通道的主体组件。 内部燃料通道沿着纵向轴线延伸到限定喷嘴的第一排出孔的第一终端。 外部空气通道沿着纵向轴线与内部燃料通道同轴地延伸到与第一终端同心设置的第二终端并且限定第二排放孔，其定向成使得其排出物从第一排放孔撞击燃料排放。 旋转叶片阵列围绕纵向轴线设置在外部空气通道内的圆形轨迹中。 每个叶片大体上构成翼型的形状，并且具有压力侧和相对的吸力侧。 叶片从前缘表面沿着相应的弦弦阵列轴向延伸到渐缩的后缘表面，每个轴线以相对于纵向轴线的给定转角设置。 每个叶片的吸入侧与相邻叶片的并置压力侧间隔开，以限定其间的多个对准的空气流动通道中的相应一个。 雾化空气被引导通过空气流动通道，以从第二排放孔排出，作为具有基本均匀速度分布的大致螺旋流。
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公开(公告)号：US20090255257A1
公开(公告)日：2009-10-15
申请号：US12182500
申请日：2008-07-30
IPC分类号： F02C1/00
CPC分类号： B23P6/007 , B22F2007/068 , B23P6/005 , B23P2700/13 , B33Y80/00 , F23D2213/00 , F23D2900/00018 , F23D2900/14701 , F23R3/14 , F23R3/28 , F23R3/283 , F23R3/286 , F23R3/343 , F23R2900/00018 , Y02T50/675 , Y10T29/49318 , Y10T29/4932 , Y10T29/49746 , Y10T137/265
摘要： A unitary distributor is disclosed, comprising at least one main flow passage located within a distributor ring body, the main flow passage having an arcuate portion oriented in a circumferential direction around a distributor axis. Exemplary embodiments of a unitary distributor having an annular ring located at the axially forward end of the distributor ring body are disclosed. A fuel distributor is disclosed, comprising a fuel conduit and a distributor wherein the fuel distributor has a unitary construction.
摘要翻译： 公开了一种单一分配器，其包括位于分配器环体内的至少一个主流动通道，主流动通道具有围绕分配器轴线在圆周方向上定向的弓形部分。 公开了具有位于分配器环体的轴向前端的环形环的整体分配器的示例性实施例。 公开了一种燃料分配器，其包括燃料管道和分配器，其中燃料分配器具有整体结构。
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公开(公告)号：US06763663B2
公开(公告)日：2004-07-20
申请号：US10120288
申请日：2002-04-10
IPC分类号： F02C100
CPC分类号： F23R3/286 , F23D2900/14004 , F23R3/283
摘要： An injector includes a plurality of flat, circular plates which provide fuel delivery and cooling of the injector. Fuel delivery passages in the plates have swirl chambers and spray orifices which are formed by chemical etching. A pair of fuel delivery plates define a fuel cavity therebetween, and include a plurality of radially-outwardly extending spokes, with the spokes from one fuel plate in adjacent, surface-to-surface relation with opposing spokes from the adjacent fuel plate. A fuel passage is defined between each of the opposing spokes, leading from the fuel cavity to a fuel outlet opening at the distal end of each spoke. A fuel tube delivers fuel to the fuel cavity between the plates, from where the fuel is then directed through the outlet openings. Downstream plates shape the fuel into appropriate sprays for ignition. An upstream cooling plate assembly directs air against the upstream fuel plate, and radially outwardly along the spokes of the upstream plate. The air is delivered through an air tube, concentric with the fuel delivery tube.
摘要翻译： 喷射器包括多个平坦的圆形板，其提供喷射器的燃料输送和冷却。 板中的燃料输送通道具有通过化学蚀刻形成的旋流室和喷射孔。 一对燃料输送板在它们之间限定一个燃料腔，并且包括多个径向向外延伸的辐条，其中一个燃料板的轮辐与相邻燃料板的相对的辐条相邻，表面到表面的关系。 燃料通道被限定在每个相对的辐条之间，从燃料腔引导到每个辐条的远端处的燃料出口。 燃料管将燃料输送到板之间的燃料腔，从那里燃料被引导通过出口。 下游板将燃料转化为合适的喷射剂。 上游冷却板组件将空气引导到上游燃料板，并沿着上游板的辐条径向向外。 空气通过与燃料输送管同心的空气管输送。
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公开(公告)号：US08171734B2
公开(公告)日：2012-05-08
申请号：US12200956
申请日：2008-08-29
IPC分类号： F02C1/00
CPC分类号： B23P6/007 , B22F2007/068 , B23P6/005 , B23P2700/13 , B33Y80/00 , F23D2213/00 , F23D2900/00018 , F23D2900/14701 , F23R3/14 , F23R3/28 , F23R3/283 , F23R3/286 , F23R3/343 , F23R2900/00018 , Y02T50/675 , Y10T29/49318 , Y10T29/4932 , Y10T29/49746 , Y10T137/265
摘要： A unitary swirler is disclosed, comprising a body having a swirler axis, and a plurality of vanes arranged in a circumferential direction around the swirler axis, wherein the swirler has a unitary construction. In one embodiment, the unitary swirler has a rim located coaxially with the swirler axis, and a wall extending between a portion of the rim and a portion of the hub. In another embodiment, the unitary swirler has an adaptor having a passage that is configured to direct a flow of air towards at least some of the plurality of vanes.
摘要翻译： 公开了一种单一旋流器，包括具有旋流器轴线的主体和围绕旋流器轴线沿圆周方向布置的多个叶片，其中旋流器具有整体结构。 在一个实施例中，整体旋流器具有与旋流器轴线同轴的边缘，以及在轮缘的一部分和轮毂的一部分之间延伸的壁。 在另一个实施例中，单一旋流器具有适配器，该适配器具有通道，该通道被配置为将空气流引向多个叶片中的至少一些。
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公开(公告)号：US20100065142A1
公开(公告)日：2010-03-18
申请号：US12182485
申请日：2008-07-30
CPC分类号： B23P6/007 , B22F2007/068 , B23P6/005 , B23P2700/13 , B33Y80/00 , F23D2213/00 , F23D2900/00018 , F23D2900/14701 , F23R3/14 , F23R3/28 , F23R3/283 , F23R3/286 , F23R3/343 , F23R2900/00018 , Y02T50/675 , Y10T29/49318 , Y10T29/4932 , Y10T29/49746 , Y10T137/265
摘要： A method for fabricating a unitary conduit is disclosed the method comprising the steps of determining three-dimensional information of the unitary conduit having at least one flow passage, converting the three-dimensional information into a plurality of slices that each define a cross-sectional layer of the unitary conduit, and successively forming each layer of the unitary conduit by fusing a metallic powder using laser energy. A unitary conduit is disclosed, comprising a body and a flow passage, wherein the flow passage and the body have a unitary construction, and made by using a rapid manufacturing process.
摘要翻译： 公开了一种用于制造单一管道的方法，该方法包括以下步骤：确定具有至少一个流动通道的单一管道的三维信息，将三维信息转换成多个切片，每个切片限定横截面层 的单一导管，并且通过使用激光能量融合金属粉末来连续地形成单层管道的每一层。 公开了一种单体导管，其包括主体和流动通道，其中流动通道和主体具有整体结构，并且通过使用快速制造工艺制成。
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公开(公告)号：US20090255102A1
公开(公告)日：2009-10-15
申请号：US12418901
申请日：2009-04-06
IPC分类号： B23P6/00
CPC分类号： B23P6/007 , B22F2007/068 , B23P6/005 , B23P2700/13 , B33Y80/00 , F23D2213/00 , F23D2900/00018 , F23D2900/14701 , F23R3/14 , F23R3/28 , F23R3/283 , F23R3/286 , F23R3/343 , F23R2900/00018 , Y02T50/675 , Y10T29/49318 , Y10T29/4932 , Y10T29/49746 , Y10T137/265
摘要： A method of repairing a fuel nozzle is disclosed comprising the steps of preparing a damaged component for repair; directing thermal energy towards a substrate; directing a stream of powder material; and depositing the powder material onto the substrate.
摘要翻译： 公开了一种修理燃料喷嘴的方法，包括以下步骤：制备损坏的部件进行修理; 将热能引向衬底; 引导粉末物料流; 并将粉末材料沉积到基底上。
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公开(公告)号：US06622488B2
公开(公告)日：2003-09-23
申请号：US10010216
申请日：2001-12-07
IPC分类号： F02C100
CPC分类号： F23D11/107 , F23D2900/11101 , F23R3/28
摘要： A fuel injector for a gas turbine engine of an aircraft has an inlet fitting, a fuel nozzle, and a housing stem with an internal conduit fluidly interconnecting the nozzle and fitting. The fuel nozzle includes a fuel swirler, which includes a plenum for receiving fuel from the conduit. A plurality of fuel passages direct fuel from the plenum to discharge orifices. The downstream ends of the passages are angled such that a swirl component is imparted to fuel exiting the discharge orifices. The swirling fuel is then applied to a prefilmer, which outwardly surrounds the fuel swirler. The passages in the fuel swirler are arranged such that the discharge orifices surround the entire nozzle for the even distribution of fuel. The plenum and passages are dimensioned and configured to receive and distribute the fuel for uniform spray patternization and low pressure drop, which provides improved combustion and flame stability.
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公开(公告)号：US06311473B1
公开(公告)日：2001-11-06
申请号：US09517823
申请日：2000-03-02
IPC分类号： F02C100
CPC分类号： F23D11/402 , F23C7/002 , F23D14/64 , F23D2900/11002 , F23D2900/14642
摘要： A combustion system includes a combustion chamber and a fuel injection apparatus, where a radial inflow swirler stage in the injector housing includes a plurality of radial inflow swirlers spaced longitudinally from each other to direct air radially inward in a swirling motion to cause fuel streams to swirl and thoroughly mix with air before passing into the combustion chamber. A plurality of liquid fuel nozzles are supported in the housing in an annular arrangement to dispense liquid fuel in a plurality of sprays in the downstream direction. A plurality of gaseous fuel nozzles are also provided in the housing supported in an annular arrangement intermediate the liquid fuel nozzles. The plurality of gaseous fuel nozzles include a series of nozzles arranged in radial spokes between each of the liquid fuel nozzles, with the size of the openings in the gaseous fuel nozzles increasing in the radially outer direction from the longitudinal axis of the housing. An outer annular flow passage is provided around the nozzles to create a cylindrical sheet of air around all the fuel streams, while an annular flow passage is provided around each of the liquid fuel nozzles to provide an annular flow of air around each of the liquid fuel sprays. A central air passage provides air centrally of the arrangement of nozzles. The air vaporizes the liquid fuel as the fuel passes downstream through the housing.
摘要翻译： 燃烧系统包括燃烧室和燃料喷射装置，其中喷射器壳体中的径向流入旋流器台包括彼此纵向间隔开的多个径向流入旋流器，以在旋转运动中径向向内引导空气，以使燃料流旋转 并在进入燃烧室之前与空气充分混合。 多个液体燃料喷嘴以环形装置支撑在壳体中，以在下游方向上分配多个喷雾中的液体燃料。 多个气体燃料喷嘴还设置在壳体中，以液体燃料喷嘴中间的环形装置支撑。 多个气体燃料喷嘴包括在每个液体燃料喷嘴之间以径向辐条布置的一系列喷嘴，气态燃料喷嘴中的开口的尺寸在从壳体的纵向轴线的径向外侧方向上增加。 在喷嘴周围设置外部环形流动通道，以围绕所有燃料流形成圆柱形空气，同时在每个液体燃料喷嘴周围设置环形流动通道，以提供围绕每个液体燃料的环形空气流 喷雾 中央空气通道在喷嘴布置的中央提供空气。 当燃料通过壳体的下游时，空气使液体燃料蒸发。
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