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1. 发明授权

US09200571B2 Fuel nozzle assembly for a gas turbine engine 有权
标题翻译：用于燃气涡轮发动机的燃油喷嘴组件
公开(公告)号：US09200571B2
公开(公告)日：2015-12-01
申请号：US12498494
申请日：2009-07-07
申请人： Donald Mark Bailey , Scott R. Simmons , Marcus B. Huffman
发明人： Donald Mark Bailey , Scott R. Simmons , Marcus B. Huffman
IPC分类号： F23R3/20 , F02C7/22 , F23R3/14 , F23R3/28 , F23M20/00
CPC分类号： F02C7/22 , F05D2240/128 , F23D2900/00008 , F23M20/005 , F23R3/14 , F23R3/283 , F23R3/286 , F23R2900/00014 , F23R2900/00017 , F23R2900/00018
摘要： A fuel nozzle assembly for a gas turbine engine includes a flange and a pre-mix tube. The flange includes a first end that is configured to couple to an end cover of the combustor, and a second end that is opposite said first end. The pre-mix tube is coupled at a first end to the flange second end. The flange and the pre-mix tube are fabricated to operate at a natural frequency that is different from an operating frequency of the gas turbine engine.
摘要翻译：用于燃气涡轮发动机的燃料喷嘴组件包括凸缘和预混合管。凸缘包括构造成联接到燃烧器的端盖的第一端和与第一端相对的第二端。预混合管在第一端连接到凸缘第二端。法兰和预混合管被制造成以与燃气涡轮发动机的工作频率不同的固有频率工作。

2. 发明授权

US09157635B2 Fuel distribution manifold 有权
标题翻译：燃油分配歧管
公开(公告)号：US09157635B2
公开(公告)日：2015-10-13
申请号：US13342497
申请日：2012-01-03
申请人： Donald Mark Bailey , Gregory Allen Boardman , William Thomas Ross
发明人： Donald Mark Bailey , Gregory Allen Boardman , William Thomas Ross
IPC分类号： B01F5/00 , F23K5/06 , F02C7/22
CPC分类号： F23K5/06 , F02C7/222 , Y10T137/85938
摘要： A fuel distribution manifold comprises an outer shell having an inner surface. The outer shell defines an inlet for receiving fuel from a parent supply line, a base opposite the inlet, a central manifold axis that intersects the inlet, and a plurality of outlets for delivering fuel to offspring fuel lines, each outlet defining a respective outlet axis. In one exemplary embodiment, a fuel distribution manifold also comprises a center-body having an outer surface and being positioned within the outer shell wherein the outer surface of the center-body and the inner surface of the outer shell define a flow-path through which fluid flows from the inlet to the plurality of outlets. In another exemplary embodiment, at least one of the outlets is positioned adjacent to the base and oriented so that its respective outlet axis is rotated relatively to a radial direction that intersects the central manifold axis.
摘要翻译：燃料分配歧管包括具有内表面的外壳。外壳限定用于从母体供应管线接收燃料的入口，与入口相对的底座，与入口相交的中心歧管轴线以及用于将燃料输送到后代燃料管线的多个出口，每个出口限定相应的出口轴线。在一个示例性实施例中，燃料分配歧管还包括具有外表面并且位于外壳内的中心体，其中中心体的外表面和外壳的内表面限定了流动路径，通过该流路流体从入口流到多个出口。在另一个示例性实施例中，至少一个出口定位成与基座相邻并且定向成使得其相应的出口轴线相对于与中心歧管轴线相交的径向方向旋转。

3. 发明授权

US09052113B1 Combustor nozzle and method for modifying the combustor nozzle 有权
标题翻译：燃烧器喷嘴和用于改变燃烧器喷嘴的方法
公开(公告)号：US09052113B1
公开(公告)日：2015-06-09
申请号：US13153499
申请日：2011-06-06
申请人： Scott Robert Simmons , Patrick Benedict Melton , Russell DeForest , Donald Mark Bailey
发明人： Scott Robert Simmons , Patrick Benedict Melton , Russell DeForest , Donald Mark Bailey
IPC分类号： F23R3/28
CPC分类号： F23R3/283 , F23R3/28 , F23R2900/00005
摘要： A combustor nozzle includes a downstream surface having an axial centerline. A plurality of passages through the downstream surface provide fluid communication through the downstream surface, and a downstream section of each passage has at least one of a frusto-conical or frusto-spherical shape. A method for modifying a combustor nozzle includes machining a downstream side of a body to remove a recast surface in a plurality of passages that provide fluid communication through the body. The method may further include machining a downstream section in each passage to form at least one of a frusto-conical or frusto-spherical surface in each passage proximate to the downstream side of the body.
摘要翻译：燃烧器喷嘴包括具有轴向中心线的下游表面。通过下游表面的多个通道提供通过下游表面的流体连通，并且每个通道的下游部分具有截头圆锥形或截头圆球形的至少一个。一种用于改变燃烧器喷嘴的方法包括机械加工主体的下游侧以去除多个通道中的重铸表面，该多个通道提供通过本体的流体连通。该方法可以进一步包括加工每个通道中的下游部分以在靠近主体的下游侧的每个通道中形成截头圆锥形或截头圆球形表面中的至少一个。

4. 发明授权

US08906392B2 Nanocluster compositions and methods 有权
标题翻译：纳米簇组合物和方法
公开(公告)号：US08906392B2
公开(公告)日：2014-12-09
申请号：US12954509
申请日：2010-11-24
申请人： Cory J. Berkland , Lianjun Shi , Nashwa El Gendy , Carl Plumley , Mark Bailey
发明人： Cory J. Berkland , Lianjun Shi , Nashwa El Gendy , Carl Plumley , Mark Bailey
IPC分类号： A61K9/00 , A61K9/16 , B82Y30/00 , A61K9/51 , A61K9/14
CPC分类号： A61K9/14 , A61K9/0075 , A61K9/145 , A61K9/1611 , A61K9/1617 , A61K9/1647 , A61K9/1688 , A61K9/5115 , A61K9/5123 , A61K9/5153 , A61K9/5192 , A61K31/196 , A61K31/337 , A61K31/4422 , A61K31/4545 , A61K31/4709 , A61K31/496 , A61K31/58 , A61K38/28 , A61K38/38 , A61M11/001 , A61M15/0021 , A61M15/0065 , A61M15/009 , A61M15/08 , A61M2202/064 , B82Y30/00
摘要： Compositions, methods of making, and methods of using nanoclusters in which the nanoclusters comprise a plurality of nanoparticles having a core of nanoparticles arranged such that the surfaces of the nanoparticles contact adjacent nanoparticles, the nanoparticles comprise an active ingredient, and the nanocluster has a mass median aerodynamic diameter of from about 0.25 μm to about 20 μm.
摘要翻译：组合物，制备方法和使用纳米团簇的方法，其中纳米团簇包含具有纳米颗粒核心的多个纳米颗粒，其纳米颗粒的表面与纳米颗粒接触，纳米颗粒包含活性成分，纳米团簇具有质量中等空气动力学直径为约0.25μm至约20μm。

5. 发明授权

US08789616B2 Apparatus and method for inhibiting propagation of a flame front 有权
标题翻译：用于抑制火焰前沿传播的装置和方法
公开(公告)号：US08789616B2
公开(公告)日：2014-07-29
申请号：US11989314
申请日：2006-07-17
申请人： Christopher Mark Bailey
发明人： Christopher Mark Bailey
IPC分类号： A62C2/00
CPC分类号： F17D3/00 , A62C4/00 , F16L55/1022 , F16L55/1026 , Y10T137/0318 , Y10T137/1963
摘要： Apparatus and a method are provided for inhibiting the propagation of a flame front that is ignited by a pumping mechanism which draws a waste stream from a process chamber. The apparatus comprises a foreline for conveying the waste stream which is drawn from the process chamber to the pumping mechanism. The foreline comprises an isolation valve for selectively isolating the pumping mechanism from the process chamber and a bypass positioned around the isolation valve. The apparatus further comprises a controller for actuating the isolation valve. The controller is configured to cause the isolation valve to be closed when the waste stream is initially drawn from the process chamber. During which time the waste stream is conveyed to the pumping mechanism via the bypass, the bypass comprises means for inhibiting propagation of a flame front therethrough. The controller is also configured to cause the isolation valve to be opened once a pressure within a region upstream of the isolation valve has been reduced below a value at which propagation of a flame front within the waste stream can be sustained.
摘要翻译：提供了一种装置和方法，用于抑制由泵送机构点燃的火焰前沿的传播，该泵送机构从处理室抽取废物流。该设备包括用于将从处理室抽出的废物流输送到泵送机构的前级管线。前级线包括用于选择性地将泵送机构与处理室隔离的隔离阀和位于隔离阀周围的旁路。该装置还包括用于致动隔离阀的控制器。控制器被配置为当废物流从处理室初始被抽出时，使隔离阀关闭。在此期间，废物流经由旁路输送到泵送机构，旁路包括用于禁止火焰前沿通过其传播的装置。一旦隔离阀上游的区域内的压力降低到能够维持废物流内的火焰前沿的传播的值，控制器也被配置成使隔离阀打开。

6. 发明授权

US08484978B2 Fuel nozzle assembly that exhibits a frequency different from a natural operating frequency of a gas turbine engine and method of assembling the same 有权
标题翻译：表现出与燃气涡轮发动机的自然工作频率不同的频率的燃料喷嘴组件及其组装方法
公开(公告)号：US08484978B2
公开(公告)日：2013-07-16
申请号：US12617085
申请日：2009-11-12
申请人： Donald Mark Bailey , Scott Robert Simmons , Marcus Byron Huffman
发明人： Donald Mark Bailey , Scott Robert Simmons , Marcus Byron Huffman
IPC分类号： F02C1/00
CPC分类号： F01D25/28 , F02C7/222 , F05D2230/60 , F05D2240/128 , F23R3/286 , F23R2900/00014 , F23R2900/00018 , Y10T29/49229
摘要： A method of assembling a fuel nozzle assembly for a gas turbine engine having a natural operating frequency includes providing a flange and providing a premix tube. The flange is fabricated from a first alloy such that the flange is configured to exhibit a first frequency that is different than the natural operating frequency of the gas turbine engine. The premix tube is fabricated from a second alloy such that the premix tube is configured to exhibit a second frequency that is different from the natural operating frequency of the gas turbine engine. The premix tube is coupled to the flange.
摘要翻译：组装具有自然工作频率的燃气涡轮发动机的燃料喷嘴组件的方法包括提供凸缘并提供预混管。凸缘由第一合金制成，使得凸缘被配置为呈现与燃气涡轮发动机的自然工作频率不同的第一频率。预混管由第二合金制成，使得预混合管被配置为展现不同于燃气涡轮发动机的自然工作频率的第二频率。预混管连接到凸缘。

7. 发明申请

US20130125549A1 GAS TURBINE COMBUSTOR ENDCOVER WITH ADJUSTABLE FLOW RESTRICTOR AND RELATED METHOD 有权
标题翻译：气体涡轮搅拌机内置可调流量限制器及相关方法
公开(公告)号：US20130125549A1
公开(公告)日：2013-05-23
申请号：US13300396
申请日：2011-11-18
申请人： Donald Mark BAILEY , Abdul Rafey KHAN
发明人： Donald Mark BAILEY , Abdul Rafey KHAN
IPC分类号： F02C7/22 , B23P6/00
CPC分类号： F23R3/28 , F23M20/005 , F23R3/10 , F23R3/286 , F23R2900/00014 , Y10T29/49238
摘要： An endcover for a turbine combustor adapted to support one or more combustor nozzles, includes a plate having one side which in use, faces a combustion chamber and an opposite side which, in use, faces away from the combustion chamber. At least one fuel cavity is formed in the plate; and a fuel restrictor insert is formed with at least one flow orifice located within the fuel cavity for supplying fuel to at least one combustor nozzle. The fuel restrictor insert is adjustable along a length dimension of the fuel cavity.
摘要翻译：适用于支撑一个或多个燃烧器喷嘴的涡轮机燃烧器的端盖包括一个板，该板在使用中面向燃烧室和在使用中相对于燃烧室的相对侧。板中形成至少一个燃料腔; 并且燃料限制器插入件形成有位于燃料腔内的至少一个流动孔，用于将燃料供应到至少一个燃烧器喷嘴。燃料限制器插件可沿燃料腔的长度尺寸调节。

8. 发明申请

US20130005366A1 ASYNCHRONOUS MESSAGING TAGS 有权
标题翻译：不寻常的消息标签
公开(公告)号：US20130005366A1
公开(公告)日：2013-01-03
申请号：US13608078
申请日：2012-09-10
申请人： Mark Bailey , James E. Christensen , Jason B. Ellis , Robert G. Farrell
发明人： Mark Bailey , James E. Christensen , Jason B. Ellis , Robert G. Farrell
IPC分类号： H04W4/14
CPC分类号： G06Q30/0207
摘要： A method includes receiving a message from a user device, determining whether the message includes a tag, identifying at least one interaction the user device performed with an application responsive to determining that the message includes the tag, calculating a difference between a time the message was received and a time associated with the at least one identified interaction, determining whether the difference between the time the message was received and the time associated with the at least one identified interaction is within a threshold value, and associating the tag with the application associated with the at least one interaction responsive to determining that the difference between the time the message was received and the time associated with the at least one identified interaction is within the threshold value.
摘要翻译：一种方法包括从用户设备接收消息，确定所述消息是否包括标签，响应于确定所述消息包含所述标签，识别响应于所述消息包括所述标签的所述用户设备执行的至少一次交互，计算所述消息是接收到的时间和与所述至少一个所识别的交互相关联的时间，确定所述消息被接收的时间与所述至少一个所识别的交互相关联的时间之间的差异是否在阈值内，以及将所述标签与与所述至少一个交互响应于确定所述消息被接收的时间与与所述至少一个所识别的交互相关联的时间之间的差异在所述阈值内。

9. 发明申请

US20120279224A1 GAS TURBINE ENGINE COMBUSTOR 有权
标题翻译：燃气轮机发动机
公开(公告)号：US20120279224A1
公开(公告)日：2012-11-08
申请号：US13099938
申请日：2011-05-03
申请人： Donald Mark Bailey , Jonathan Dwight Berry , Luis Manuel Flamand , Kwanwoo Kim , Patrick Benedict Melton , Robert Joseph Rohrssen , John Drake Vanselow
发明人： Donald Mark Bailey , Jonathan Dwight Berry , Luis Manuel Flamand , Kwanwoo Kim , Patrick Benedict Melton , Robert Joseph Rohrssen , John Drake Vanselow
IPC分类号： F23C3/00
CPC分类号： F23R3/283 , F23D2900/00003 , F23R3/286 , F23R3/46 , F23R3/54 , F23R2900/00017 , F23R2900/00018
摘要： A gas turbine engine combustor is provided and includes an array of fuel nozzles, a combustion casing assembly disposed about the array of fuel nozzles and an end cap assembly disposed within the combustion casing assembly to define with the combustion casing assembly an axis-symmetric annulus through which fluid travels into each of the fuel nozzles, at least one of the combustion casing assembly and the end cap assembly being formed with lobed, three-dimensional contouring.
摘要翻译：提供了一种燃气涡轮发动机燃烧器，其包括燃料喷嘴阵列，围绕燃料喷嘴阵列设置的燃烧壳体组件和设置在燃烧壳体组件内的端盖组件，以便与燃烧壳体组件形成轴对称的环通过所述流体行进到每个燃料喷嘴中，燃烧壳体组件和端盖组件中的至少一个形成有叶状的三维轮廓。

10. 发明申请

US20120181354A1 COMBUSTOR NOZZLE AND METHOD FOR FABRICATING THE COMBUSTOR NOZZLE 有权
标题翻译： COMBUSTOR喷嘴及其制造方法
公开(公告)号：US20120181354A1
公开(公告)日：2012-07-19
申请号：US13009108
申请日：2011-01-19
申请人： Donald Mark Bailey , William Lawrence Byrne , Patrick Benedict Melton
发明人： Donald Mark Bailey , William Lawrence Byrne , Patrick Benedict Melton
IPC分类号： B05B7/10 , B22D25/00
CPC分类号： B22D25/00 , F23C2900/07001 , F23D2900/00008 , F23R3/14 , F23R3/286 , F23R2900/00018 , Y02T50/675
摘要： A combustor nozzle includes a single-piece swirler. The single-piece swirler includes a center body extending axially along the single-piece swirler, a first fuel passage inside the center body, and a plurality of vanes extending radially from the center body. A method for fabricating a combustor nozzle includes casting a single-piece swirler having a center body and a plurality of vanes extending radially from the center body.
摘要翻译：燃烧器喷嘴包括单件旋流器。单件旋流器包括沿着单件旋流器轴向延伸的中心体，中心体内的第一燃料通道和从中心体径向延伸的多个叶片。一种用于制造燃烧器喷嘴的方法包括浇铸具有中心体的单件旋流器和从中心体径向延伸的多个叶片。

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