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11.发明申请Systems, Methods, and Apparatus Providing a Secondary Fuel Nozzle Assembly 审中-公开提供二次燃料喷嘴组件的系统，方法和装置公开(公告)号：US20100205970A1
公开(公告)日：2010-08-19
申请号：US12388855
申请日：2009-02-19
IPC分类号： F02C7/22
CPC分类号： F23R3/343
摘要： Provided are systems, methods, and apparatus providing secondary fuel nozzle assemblies. For example, a secondary fuel nozzle assembly can include a central portion having a proximal end and distal end, and defining a central passage therethrough, which can include at least one coiled tube extending through the central passage from the proximal end to the distal end; a flange having at least one main secondary fuel orifice in fluid communication with the central passage at the proximal end and at least one pilot orifice in fluid communication with the at least one coiled tube at the proximal end; and a tip portion having a proximal end and distal end, and defining at least one passage therethrough, which can be in fluid communication with the distal end of the at least one coiled tube and at least one orifice formed in the distal end of the tip portion.
摘要翻译： 提供了提供二次燃料喷嘴组件的系统，方法和装置。 例如，次级燃料喷嘴组件可以包括具有近端和远端的中心部分，并且限定穿过其中的中心通道，该中心通道可包括从近端延伸到远端延伸穿过中心通道的至少一个螺旋管; 具有至少一个主中间燃料孔口的凸缘，所述至少一个主次级燃料孔口在近端处与中心通道流体连通，以及至少一个引导孔口，其在近端与所述至少一个螺旋管道流体连通; 以及尖端部分，其具有近端和远端，并且限定穿过其中的至少一个通道，其可以与所述至少一个盘管的远端流体连通，并且形成在尖端的远端中的至少一个孔口 一部分。
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12.发明申请公开(公告)号：US20090223054A1
公开(公告)日：2009-09-10
申请号：US11828447
申请日：2007-07-26
CPC分类号： F23R3/28 , F02C7/22 , F23R3/34 , Y10T29/49432
摘要： A method of fabricating a fuel nozzle is provided. The method includes providing a unitary portion of material including a first end face, a second end face, and a body extending therebetween. A passageway is fabricated to extend from the first end face to the second end face along a centerline of the portion of material. The method further includes fabricating a plurality of concentrically-aligned channels within the first end face, and fabricating a plurality of inlets that extend through at least one of the second end face and an outer surface of the body to at least one of the passageway and one of the plurality of channels.
摘要翻译： 提供一种制造燃料喷嘴的方法。 该方法包括提供包括第一端面，第二端面和在它们之间延伸的主体的材料的整体部分。 制造通道沿着材料部分的中心线从第一端面延伸到第二端面。 该方法还包括在第一端面内制造多个同心对准的通道，并且制造多个入口，其延伸穿过主体的第二端面和外表面中的至少一个，至少通过通道和 多个通道之一。
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公开(公告)号：US08397512B2
公开(公告)日：2013-03-19
申请号：US12197838
申请日：2008-08-25
IPC分类号： F02C1/00
CPC分类号： F02C7/18 , F01D9/023 , Y10T29/49245
摘要： A method for assembling a gas turbine engine includes coupling a transition piece between a combustor liner and a nozzle assembly. The method also includes extending a first portion of a flow sleeve from the transition piece about at least a portion of the combustor liner. The method further includes coupling a second portion of the flow sleeve to the first portion of the flow sleeve such that the flow sleeve second portion extends from the flow sleeve first portion and at least partially about at least a portion of the transition piece. The flow sleeve second portion includes a scoop that cooperates with the transition piece to at least partially define a unitary cooling air passage that includes a unitary scoop-shaped opening. The scoop is oriented to introduce a substantially uniform cooling air flow to the transition piece.
摘要翻译： 一种用于组装燃气涡轮发动机的方法包括将过渡件联接在燃烧器衬套和喷嘴组件之间。 该方法还包括将过渡件的第一部分从燃烧器衬套的至少一部分延伸出来。 该方法还包括将流动套筒的第二部分联接到流动套筒的第一部分，使得流动套筒第二部分从流动套筒第一部分延伸并且至少部分地围绕过渡件的至少一部分延伸。 流动套筒第二部分包括与过渡件配合以至少部分地限定包括整体式勺状开口的整体冷却空气通道的勺子。 勺子被定向成将大致均匀的冷却空气流引入过渡件。
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公开(公告)号：US08020385B2
公开(公告)日：2011-09-20
申请号：US12180879
申请日：2008-07-28
IPC分类号： F02C1/00
摘要： A turbomachine includes a combustor assembly, a cap assembly attached to the combustor assembly, a centerbody within the cap assembly, a wall of the centerbody having a first end, a second end and an intermediate portion, and an external turbulator member in operable communication with the cap assembly. The external turbulator member is spaced from the wall to form a passage defined by a gap between the wall of the centerbody and the external turbulator. The external turbulator member includes a step positioned at the second end of the centerbody. The step defines a radial distance about the second end of the centerbody. The external turbulator member is formed having a step-to-gap ratio relative to the centerbody in a range of about 0.8 to about 1.2.
摘要翻译： 涡轮机包括燃烧器组件，附接到燃烧器组件的帽组件，帽组件内的中心体，中心体的壁，其具有第一端，第二端和中间部分，以及外部湍流构件，其可操作地与 盖组件。 外部紊流器构件与壁间隔开以形成由中心体的壁和外部湍流器之间的间隙限定的通道。 外部湍流器构件包括位于中心体的第二端的台阶。 该步骤限定了围绕中心体的第二端的径向距离。 外部紊流器构件形成为具有在约0.8至约1.2的范围内的相对于中心体的台阶间隙比。
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15.发明授权公开(公告)号：US07757491B2
公开(公告)日：2010-07-20
申请号：US12118076
申请日：2008-05-09
申请人： William Kirk Hessler
发明人： William Kirk Hessler
IPC分类号： F02C1/00
CPC分类号： F23R3/286 , F23D2900/14004 , Y10T29/49412
摘要： A method for fabricating a fuel nozzle assembly includes providing a nozzle portion including a fuel passageway defined about a center axis of the fuel nozzle assembly. A longitudinal axis of a first peg is oriented to intersect the fuel nozzle assembly center axis such that a first plane is defined. The first peg defines a first opening having a centerline intersecting the first peg longitudinal axis and obliquely oriented with respect to the first plane. The first peg is coupled in flow communication with the fuel passageway such that the first peg extends radially outward from the nozzle portion and such that the first opening is configured to direct a flow of fuel in an oblique direction with respect to the fuel nozzle assembly center axis to facilitate fuel mixing.
摘要翻译： 一种用于制造燃料喷嘴组件的方法包括提供喷嘴部分，其包括围绕燃料喷嘴组件的中心轴线限定的燃料通路。 第一栓钉的纵向轴线被定向成与燃料喷嘴组件中心轴线相交，使得限定第一平面。 第一栓钉限定第一开口，其具有与第一钉纵向轴线相交并且相对于第一平面倾斜定向的中心线。 第一栓与燃料通道流体连通地联接，使得第一钉从喷嘴部分径向向外延伸，并且使得第一开口构造成沿相对于燃料喷嘴组件中心的倾斜方向引导燃料流 轴以促进燃料混合。
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公开(公告)号：US20100175257A1
公开(公告)日：2010-07-15
申请号：US12656803
申请日：2010-02-17
申请人： William Kirk Hessler
发明人： William Kirk Hessler
IPC分类号： B23P15/00
CPC分类号： F23R3/28 , F23D11/38 , F23R2900/00017 , F23R2900/00018 , Y10T29/49432
摘要： A secondary fuel nozzle is formed by brazing and welding a central core, a cylindrical body, and a unitary secondary fuel nozzle portion. The central core has a central bore for receiving a liquid fuel cartridge, and at least two passages concentric with the central bore. The secondary fuel nozzle portion includes a base flange and a main shaft having a central bore for aligning with the central bore of the core and for receiving the liquid fuel cartridge, and a plurality of peripheral bores disposed at spaced locations about the central bore for flow communication with the concentric passages of the core. The core is brazed to the base flange and the cylindrical body is disposed around the core and welded to the base flange to define a one-piece secondary fuel nozzle assembly.
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17.发明申请公开(公告)号：US20090277177A1
公开(公告)日：2009-11-12
申请号：US12118076
申请日：2008-05-09
申请人： William Kirk Hessler
发明人： William Kirk Hessler
CPC分类号： F23R3/286 , F23D2900/14004 , Y10T29/49412
摘要： A method for fabricating a fuel nozzle assembly includes providing a nozzle portion including a fuel passageway defined about a center axis of the fuel nozzle assembly. A longitudinal axis of a first peg is oriented to intersect the fuel nozzle assembly center axis such that a first plane is defined. The first peg defines a first opening having a centerline intersecting the first peg longitudinal axis and obliquely oriented with respect to the first plane. The first peg is coupled in flow communication with the fuel passageway such that the first peg extends radially outward from the nozzle portion and such that the first opening is configured to direct a flow of fuel in an oblique direction with respect to the fuel nozzle assembly center axis to facilitate fuel mixing.
摘要翻译： 一种用于制造燃料喷嘴组件的方法包括提供喷嘴部分，其包括围绕燃料喷嘴组件的中心轴线限定的燃料通路。 第一栓钉的纵向轴线被定向成与燃料喷嘴组件中心轴线相交，使得限定第一平面。 第一栓钉限定第一开口，其具有与第一钉纵向轴线相交并且相对于第一平面倾斜定向的中心线。 第一栓与燃料通道流体连通地联接，使得第一钉从喷嘴部分径向向外延伸，并且使得第一开口构造成沿相对于燃料喷嘴组件中心的倾斜方向引导燃料流 轴以促进燃料混合。
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公开(公告)号：US07941923B2
公开(公告)日：2011-05-17
申请号：US12656803
申请日：2010-02-17
申请人： William Kirk Hessler
发明人： William Kirk Hessler
CPC分类号： F23R3/28 , F23D11/38 , F23R2900/00017 , F23R2900/00018 , Y10T29/49432
摘要： A secondary fuel nozzle is formed by brazing and welding a central core, a cylindrical body, and a unitary secondary fuel nozzle portion. The central core has a central bore for receiving a liquid fuel cartridge, and at least two passages concentric with the central bore. The secondary fuel nozzle portion includes a base flange and a main shaft having a central bore for aligning with the central bore of the core and for receiving the liquid fuel cartridge, and a plurality of peripheral bores disposed at spaced locations about the central bore for flow communication with the concentric passages of the core. The core is brazed to the base flange and the cylindrical body is disposed around the core and welded to the base flange to define a one-piece secondary fuel nozzle assembly.
摘要翻译： 二次燃料喷嘴通过钎焊和焊接中心芯，圆柱体和单一二次燃料喷嘴部分而形成。 中心芯具有用于接收液体燃料盒的中心孔，以及与中心孔同心的至少两个通道。 次级燃料喷嘴部分包括基部凸缘和主轴，该主轴具有用于与芯的中心孔对准的中心孔并用于容纳液体燃料盒，以及多个周边孔，围绕中心孔设置在间隔开的位置，用于流动 与核心的同心通道的通信。 芯部钎焊到基部凸缘上，并且圆柱形主体设置在芯部周围并焊接到基部凸缘以限定一体式二次燃料喷嘴组件。
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19.发明授权公开(公告)号：US07908863B2
公开(公告)日：2011-03-22
申请号：US12069870
申请日：2008-02-12
申请人： William Kirk Hessler
发明人： William Kirk Hessler
CPC分类号： F23D11/24 , F23D11/38 , F23D2900/11001 , F23D2900/14004 , F23R3/18 , F23R3/28 , F23R3/343 , Y10T29/49432
摘要： A method for fabricating a secondary fuel nozzle assembly includes providing a nozzle portion defining a passageway configured to supply fuel. At least one peg is operatively coupled in fuel flow communication with the passageway. The at least one peg extends radially outward from the nozzle portion and defines at least one opening configured to direct a flow of fuel in a substantially upstream direction. A disc is positioned about the nozzle portion upstream of the at least one peg. The disc is positioned in communication with the at least one opening and configured to interfere with the flow of fuel to facilitate fuel atomization.
摘要翻译： 一种用于制造二次燃料喷嘴组件的方法包括提供限定被配置为供应燃料的通道的喷嘴部分。 至少一个销可操作地联接在与通道的燃料流连通中。 至少一个钉从喷嘴部分径向向外延伸并且限定至少一个开口，该开口被构造成引导基本上游方向上的燃料流。 圆盘围绕至少一个钉的上游的喷嘴部分定位。 盘被定位成与至少一个开口连通并且被配置成干扰燃料的流动以促进燃料雾化。
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公开(公告)号：US20100043441A1
公开(公告)日：2010-02-25
申请号：US12197838
申请日：2008-08-25
CPC分类号： F02C7/18 , F01D9/023 , Y10T29/49245
摘要： A method for assembling a gas turbine engine includes coupling a transition piece between a combustor liner and a nozzle assembly. The method also includes extending a first portion of a flow sleeve from the transition piece about at least a portion of the combustor liner. The method further includes coupling a second portion of the flow sleeve to the first portion of the flow sleeve such that the flow sleeve second portion extends from the flow sleeve first portion and at least partially about at least a portion of the transition piece. The flow sleeve second portion includes a scoop that cooperates with the transition piece to at least partially define a unitary cooling air passage that includes a unitary scoop-shaped opening. The scoop is oriented to introduce a substantially uniform cooling air flow to the transition piece.
摘要翻译： 一种用于组装燃气涡轮发动机的方法包括将过渡件联接在燃烧器衬套和喷嘴组件之间。 该方法还包括将过渡件的第一部分从燃烧器衬套的至少一部分延伸出来。 该方法还包括将流动套筒的第二部分联接到流动套筒的第一部分，使得流动套筒第二部分从流动套筒第一部分延伸并且至少部分地围绕过渡件的至少一部分延伸。 流动套筒第二部分包括与过渡件配合以至少部分地限定包括整体式勺状开口的整体冷却空气通道的勺子。 勺子被定向成将大致均匀的冷却空气流引入过渡件。
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