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1. 发明申请

US20120294729A1 COLD METAL TRANSFER HARDFACING OF BUCKETS 审中-公开
标题翻译： BUCKETS的金属转移危害
公开(公告)号：US20120294729A1
公开(公告)日：2012-11-22
申请号：US13108939
申请日：2011-05-16
申请人： Attila Szabo , John Drake Vanselow
发明人： Attila Szabo , John Drake Vanselow
IPC分类号： F03B3/12 , B23K9/24
CPC分类号： B23K9/044 , B23K9/09 , B23K2101/001 , F01D5/225 , F05D2230/232 , F05D2230/30 , F05D2300/506 , F05D2300/702
摘要： In one embodiment, the invention provides a method of hardfacing a portion of a bucket subject to mechanical stress, the method comprising: contacting a surface of a bucket with a hardfacing filler metal connected to a welding nozzle to establish an arc between the surface and the filler metal and form a molten weld pool comprising the filler metal and a material of the surface; extending the filler metal into the molten weld pool to short circuit the arc; withdrawing the filler metal from the molten weld pool to re-establish the arc; moving the welding nozzle along the surface; and re-extending the filler metal into the molten weld pool to short circuit the arc, deposit additional filler metal into the molten weld pool, and liquify additional material of the surface into the molten weld pool.
摘要翻译：在一个实施例中，本发明提供了一种使机械应力的铲斗的一部分表面硬化的方法，该方法包括：将铲斗的表面与连接到焊接喷嘴的硬化填充金属接触，以在表面和填充金属并形成包括填充金属和表面材料的熔融熔池; 将填充金属延伸到熔融焊池中以使电弧短路; 从熔融焊池中取出填充金属以重新建立电弧; 沿着表面移动焊接喷嘴; 并将填充金属重新延伸到熔融熔池中以使电弧短路，将另外的填充金属沉积到熔融焊池中，并将表面的附加材料液化成熔融熔池。

2. 发明申请

US20110008614A1 Electrostatic Powder Coatings 审中-公开
标题翻译：静电粉末涂料
公开(公告)号：US20110008614A1
公开(公告)日：2011-01-13
申请号：US12500502
申请日：2009-07-09
申请人： Tamara Jean Muth , Patricia Chapman Irwin , Surinder Singh Pabla , John Drake Vanselow
发明人： Tamara Jean Muth , Patricia Chapman Irwin , Surinder Singh Pabla , John Drake Vanselow
IPC分类号： B32B5/16 , B05D1/04 , B05D1/36 , B32B9/00 , B32B15/04 , B32B18/00 , B32B27/38
CPC分类号： C04B35/6306 , C04B35/6303 , C04B35/6309 , C04B35/6313 , C04B2235/3241 , F01D5/284 , F01D5/288 , F05D2230/90 , F05D2260/95 , Y10T428/256 , Y10T428/31515 , Y10T428/31678
摘要： In one embodiment, a protective coating may be electrostatically applied to a rotary machine component. The powder coating includes an electrically conductive sacrificial base coat and a ceramic oxide erosion resistant top coat.
摘要翻译：在一个实施例中，保护涂层可以静电地施加到旋转机器部件。粉末涂料包括导电牺牲基底涂层和陶瓷耐氧化物侵蚀顶涂层。

3. 发明申请

US20100089020A1 METERING OF DILUENT FLOW IN COMBUSTOR 审中-公开
标题翻译：二氧化碳计量流量
公开(公告)号：US20100089020A1
公开(公告)日：2010-04-15
申请号：US12250933
申请日：2008-10-14
申请人： Jesse Ellis Barton , Jonathan Dwight Berry , Mark Allan Hadley , John Drake Vanselow
发明人： Jesse Ellis Barton , Jonathan Dwight Berry , Mark Allan Hadley , John Drake Vanselow
IPC分类号： F02C3/20 , F02C3/30
CPC分类号： F23R3/04 , F23R3/002 , F23R3/10 , F23R3/283 , F23R3/286
摘要： Disclosed is a combustor including a baffle plate having at least one through baffle hole and at least one fuel nozzle extending through the at least one baffle hole. A circumferentially adjustable collar is located at the at least one baffle hole between the baffle plate and the at least one fuel nozzle. A plurality of openings at the collar are configured to meter a flow of diluent between the baffle hole and the at least one fuel nozzle. Further disclosed is a method for providing diluent to a combustor including providing a plurality of openings disposed at a circumferentially adjustable collar between a baffle plate and at least one fuel nozzle extending through a through hole in the baffle plate. The diluent is flowed through the plurality of openings toward at least one airflow hole in the at least one fuel nozzle.
摘要翻译：公开了一种燃烧器，其包括具有至少一个通过挡板孔的挡板和至少一个延伸穿过至少一个挡板孔的燃料喷嘴。一个可周向调节的套环位于挡板和至少一个燃料喷嘴之间的至少一个挡板孔处。在轴环处的多个开口被配置成测量在挡板孔和至少一个燃料喷嘴之间的稀释剂流。还公开了一种用于向燃烧器提供稀释剂的方法，包括提供设置在挡板和至少一个延伸穿过挡板中的通孔的燃料喷嘴之间的周向可调环圈处的多个开口。稀释剂通过多个开口朝向至少一个燃料喷嘴中的至少一个气流孔流动。

4. 发明授权

US09249679B2 Impingement sleeve and methods for designing and forming impingement sleeve 有权
标题翻译：冲击套筒和冲击套管的设计和成型方法
公开(公告)号：US09249679B2
公开(公告)日：2016-02-02
申请号：US13589375
申请日：2012-08-20
申请人： Matthew Paul Berkebile , Jerome David Brown , Ronald James Chila , Patrick Benedict Melton , Russell DeForest , David William Cihlar , Wei Chen , John Drake Vanselow
发明人： Matthew Paul Berkebile , Jerome David Brown , Ronald James Chila , Patrick Benedict Melton , Russell DeForest , David William Cihlar , Wei Chen , John Drake Vanselow
IPC分类号： F23R3/06 , F01D9/02
CPC分类号： F01D9/023 , F05D2260/201 , F23R3/06 , F23R2900/03044
摘要： An impingement sleeve and methods for designing and forming an impingement sleeve are disclosed. In one embodiment, the impingement sleeve includes a body configured to at least partially surround a transition piece of the combustor. The impingement sleeve further includes a plurality of cooling holes defined in the body, the plurality of cooling holes having a cooling hole pattern configured to provide a desired operational value for the transition piece. At least one of the plurality of cooling holes has a chamfer extending at least partially between an inlet and an outlet of the at least one of the plurality of cooling holes. At least a portion of the plurality of cooling holes are generally longitudinally asymmetric.
摘要翻译：公开了一种冲击套筒和用于设计和形成冲击套筒的方法。在一个实施例中，冲击套筒包括构造成至少部分地围绕燃烧器的过渡件的主体。所述冲击套筒还包括限定在所述主体中的多个冷却孔，所述多个冷却孔具有冷却孔图案，所述冷却孔图案被配置为为所述过渡件提供期望的操作值。多个冷却孔中的至少一个具有至少部分地在所述多个冷却孔中的至少一个冷却孔的入口和出口之间延伸的倒角。多个冷却孔的至少一部分大体上是纵向不对称的。

5. 发明授权

US08938978B2 Gas turbine engine combustor with lobed, three dimensional contouring 有权
标题翻译：燃气涡轮发动机燃烧器具有叶片，三维轮廓
公开(公告)号：US08938978B2
公开(公告)日：2015-01-27
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： F23R3/28 , F23R3/46 , F23R3/54
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。

6. 发明授权

US07722916B2 Methods for controlling plasma spray coating porosity on an article and articles manufactured therefrom 有权
标题翻译：用于控制由其制造的制品和制品上的等离子体喷涂孔隙率的方法
公开(公告)号：US07722916B2
公开(公告)日：2010-05-25
申请号：US11420867
申请日：2006-05-30
申请人： Hsin-Pang Wang , Michael Charles Ostrowski , Eric Moran , Stephen Gerard Pope , John Drake Vanselow , Edward Richard Haupt
发明人： Hsin-Pang Wang , Michael Charles Ostrowski , Eric Moran , Stephen Gerard Pope , John Drake Vanselow , Edward Richard Haupt
IPC分类号： C23C16/52
CPC分类号： B05B12/00 , C23C4/12
摘要： Disclosed herein is a spray coating process for a robotic spray gun assembly comprising importing a discretized model of an object geometry to be coated; importing a numerically characterized spray pattern file; importing a robot motion file comprising a plurality of motion positions, dwell times and orientations defining a spray direction of the robotic spray gun; reading each motion position within the motion file; determining which portions of the object geometry are visible at each motion position; computing a void volume fraction at each visible portion of the object geometry based on the core compression, the incident angle of the robotic spray gun and the ricocheting of the spray for each motion position; and calculating total coating thickness on portions of the object geometry for the complete motion step.
摘要翻译：本文公开了一种用于机器人喷枪组件的喷涂方法，包括导入待涂覆的物体几何体的离散模型; 导入数字表征的喷雾图案文件; 导入包括限定所述机器人喷枪的喷射方向的多个运动位置，停留时间和方向的机器人运动文件; 读取运动文件内的每个运动位置; 确定对象几何的哪些部分在每个运动位置可见; 基于核心压缩，机器人喷枪的入射角度和每个运动位置的喷射喷射计算物体几何体的每个可见部分处的空隙体积分数; 以及在整个运动步骤的对象几何部分上计算总涂层厚度。

7. 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。

8. 发明申请

US20100092896A1 METHOD AND APPARATUS FOR INTRODUCING DILUENT FLOW INTO A COMBUSTOR 有权
标题翻译：用于将液体流引入燃烧器的方法和装置
公开(公告)号：US20100092896A1
公开(公告)日：2010-04-15
申请号：US12250875
申请日：2008-10-14
申请人： Jesse Ellis Barton , Jonathan Dwight Berry , Mark Allan Hadley , Glenn David Nelson , Robert Joseph Rohrssen , John Drake Vanselow
发明人： Jesse Ellis Barton , Jonathan Dwight Berry , Mark Allan Hadley , Glenn David Nelson , Robert Joseph Rohrssen , John Drake Vanselow
IPC分类号： F23L7/00 , F23D11/38 , F23N1/08
CPC分类号： F23R3/04 , F23L7/005 , F23L2900/07002 , F23L2900/07003 , F23L2900/07009 , F23R3/283 , F23R3/44 , F23R3/60 , F23R2900/00017 , Y02E20/342
摘要： Disclosed is a combustor including a baffle plate having at least one through baffle hole and at least one fuel nozzle extending through the at least one baffle hole. At least one shroud is secured to the baffle plate and includes at least one piston ring disposed at the shroud. The at least one piston ring is configured to meter a flow of diluent between the at least one shroud and the at least one fuel nozzle. Further disclosed is a method for providing diluent to a combustor including providing a piston ring gap defined by at least one piston ring disposed at a baffle plate and a fuel nozzle extending through a through hole in the baffle plate. The diluent is flowed through the piston ring gap toward at least one airflow hole in the fuel nozzle.
摘要翻译：公开了一种燃烧器，其包括具有至少一个通过挡板孔的挡板和至少一个延伸穿过至少一个挡板孔的燃料喷嘴。至少一个护罩固定在挡板上并且包括设置在护罩上的至少一个活塞环。所述至少一个活塞环构造成测量所述至少一个护罩和所述至少一个燃料喷嘴之间的稀释剂流。还公开了一种向燃烧器提供稀释剂的方法，包括提供由设置在挡板上的至少一个活塞环限定的活塞环间隙和延伸穿过挡板中的通孔的燃料喷嘴。稀释剂通过活塞环间隙朝向燃料喷嘴中的至少一个气流孔流动。

9. 发明申请

US20070281074A1 METHODS FOR CONTROLLING PLASMA SPRAY COATING POROSITY ON AN ARTICLE AND ARTICLES MANUFACTURED THEREFROM 有权
标题翻译：用于控制其制造的物品和制品上的等离子喷涂涂层的方法
公开(公告)号：US20070281074A1
公开(公告)日：2007-12-06
申请号：US11420867
申请日：2006-05-30
申请人： Hsin-Pang Wang , Michael Charles Ostrowski , Eric Moran , Stephen Gerard Pope , John Drake Vanselow , Edward Richard Haupt
发明人： Hsin-Pang Wang , Michael Charles Ostrowski , Eric Moran , Stephen Gerard Pope , John Drake Vanselow , Edward Richard Haupt
IPC分类号： C23C16/52 , B05D5/00
CPC分类号： B05B12/00 , C23C4/12
摘要： Disclosed herein is a spray coating process for a robotic spray gun assembly comprising importing a discretized model of an object geometry to be coated; importing a numerically characterized spray pattern file; importing a robot motion file comprising a plurality of motion positions, dwell times and orientations defining a spray direction of the robotic spray gun; reading each motion position within the motion file; determining which portions of the object geometry are visible at each motion position; computing a void volume fraction at each visible portion of the object geometry based on the core compression, the incident angle of the robotic spray gun and the ricocheting of the spray for each motion position; and calculating total coating thickness on portions of the object geometry for the complete motion step.
摘要翻译：本文公开了一种用于机器人喷枪组件的喷涂方法，包括导入待涂覆的物体几何体的离散模型; 导入数字表征的喷雾图案文件; 导入包括限定所述机器人喷枪的喷射方向的多个运动位置，停留时间和方向的机器人运动文件; 读取运动文件内的每个运动位置; 确定对象几何的哪些部分在每个运动位置可见; 基于核心压缩，机器人喷枪的入射角度和每个运动位置的喷射喷射计算物体几何体的每个可见部分处的空隙体积分数; 以及在整个运动步骤的对象几何部分上计算总涂层厚度。

10. 发明申请

US20130318975A1 TURBOMACHINE COMBUSTOR NOZZLE INCLUDING A MONOLITHIC NOZZLE COMPONENT AND METHOD OF FORMING THE SAME 有权
标题翻译：涡轮喷雾器喷嘴，包括单声道喷嘴组件及其形成方法
公开(公告)号：US20130318975A1
公开(公告)日：2013-12-05
申请号：US13482540
申请日：2012-05-29
申请人： Lucas John Stoia , Patrick Benedict Melton , Thomas Edward Johnson , Christian Xavier Stevenson , John Drake Vanselow , James Harold Westmoreland
发明人： Lucas John Stoia , Patrick Benedict Melton , Thomas Edward Johnson , Christian Xavier Stevenson , John Drake Vanselow , James Harold Westmoreland
IPC分类号： F23R3/28 , B23P11/00 , F23R3/10
CPC分类号： F23R3/283 , F23R3/286 , F23R2900/00017 , F23R2900/00018 , Y10T29/49323
摘要： A turbomachine combustor nozzle includes a monolithic nozzle component having a plate element and a plurality of nozzle elements. Each of the plurality of nozzle elements includes a first end extending from the plate element to a second end. The plate element and plurality of nozzle elements are formed as a unitary component. A plate member is joined with the nozzle component. The plate member includes an outer edge that defines first and second surfaces and a plurality of openings extending between the first and second surfaces. The plurality of openings are configured and disposed to register with and receive the second end of corresponding ones of the plurality of nozzle elements.
摘要翻译：涡轮机燃烧器喷嘴包括具有板元件和多个喷嘴元件的单片喷嘴部件。多个喷嘴元件中的每一个包括从板元件延伸到第二端的第一端。板元件和多个喷嘴元件形成为整体部件。板构件与喷嘴部件接合。板构件包括限定第一和第二表面的外边缘和在第一和第二表面之间延伸的多个开口。多个开口被配置和设置成与多个喷嘴元件中对应的喷嘴元件的对应的第二端对准并接收。

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