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1. 发明授权

US09267687B2 Combustion system having a venturi for reducing wakes in an airflow 有权
标题翻译：燃烧系统具有文丘里管，用于减少气流中的醒来
公开(公告)号：US09267687B2
公开(公告)日：2016-02-23
申请号：US13289537
申请日：2011-11-04
申请人： Abdul Rafey Khan , David William Cihlar , Ajay Pratap Singh , Bradley Donald Crawley , Jason Thurman Stewart
发明人： Abdul Rafey Khan , David William Cihlar , Ajay Pratap Singh , Bradley Donald Crawley , Jason Thurman Stewart
IPC分类号： F23R3/54 , F23R3/00
CPC分类号： F23R3/002 , F23R3/54 , F23R2900/03044
摘要： A combustion system is provided having a liner, a flow sleeve, a flow-obstructing element, and a venturi. The liner is disposed around a combustion region. The flow sleeve is disposed around the liner. The liner and the flow sleeve cooperate to create an air passage having an airflow located between the liner and the flow sleeve. The flow-obstructing element is disposed within the air passage, and generally obstructs the airflow in the air passage to create wakes in the airflow. The venturi is disposed downstream from the flow-obstructing element, and generally restricts and diffuses the airflow in the air passage to reduce wakes in the airflow.
摘要翻译：提供了具有衬套，流动套筒，阻流元件和文氏管的燃烧系统。衬套围绕燃烧区域设置。流动套管围绕衬套设置。衬套和流动套管配合以产生具有位于衬套和流动套筒之间的气流的空气通道。流动阻塞元件设置在空气通道内，并且通常阻碍空气通道中的气流在气流中产生醒来。文丘里管设置在阻流元件的下游，并且通常限制和扩散空气通道中的气流以减少气流中的醒来。

2. 发明申请

US20130111909A1 Combustion System Having A Venturi For Reducing Wakes In An Airflow 有权
标题翻译：具有文丘里燃烧系统以减少气流中的气味
公开(公告)号：US20130111909A1
公开(公告)日：2013-05-09
申请号：US13289537
申请日：2011-11-04
申请人： Abdul Rafey Khan , David William Cihlar , Ajay Pratap Singh , Bradley Donald Crawley , Jason Thurman Stewart
发明人： Abdul Rafey Khan , David William Cihlar , Ajay Pratap Singh , Bradley Donald Crawley , Jason Thurman Stewart
IPC分类号： F23R3/42
CPC分类号： F23R3/002 , F23R3/54 , F23R2900/03044
摘要： A combustion system is provided having a liner, a flow sleeve, a flow-obstructing element, and a venturi. The liner is disposed around a combustion region. The flow sleeve is disposed around the liner. The liner and the flow sleeve cooperate to create an air passage having an airflow located between the liner and the flow sleeve. The flow-obstructing element is disposed within the air passage, and generally obstructs the airflow in the air passage to create wakes in the airflow. The venturi is disposed downstream from the flow-obstructing element, and generally restricts and diffuses the airflow in the air passage to reduce wakes in the airflow.
摘要翻译：提供了具有衬套，流动套筒，阻流元件和文氏管的燃烧系统。衬套围绕燃烧区域设置。流动套管围绕衬套设置。衬套和流动套管配合以产生具有位于衬套和流动套筒之间的气流的空气通道。流动阻塞元件设置在空气通道内，并且通常阻碍空气通道中的气流在气流中产生醒来。文丘里管设置在阻流元件的下游，并且通常限制和扩散空气通道中的气流以减少气流中的醒来。

3. 发明授权

US08850821B2 System for fuel injection in a fuel nozzle 有权
标题翻译：燃料喷嘴燃料喷射系统
公开(公告)号：US08850821B2
公开(公告)日：2014-10-07
申请号：US13269510
申请日：2011-10-07
申请人： Abdul Rafey Khan , Bradley Donald Crawley , Donald Mark Bailey , Ajay Pratap Singh
发明人： Abdul Rafey Khan , Bradley Donald Crawley , Donald Mark Bailey , Ajay Pratap Singh
IPC分类号： F02C1/00 , F23R3/28 , F23R3/36 , F23R3/14
CPC分类号： F23R3/286 , F23C2900/07001 , F23D2900/14021 , F23R3/14 , F23R3/36 , F23R2900/00013
摘要： A system includes a fuel nozzle. The fuel nozzle includes a hub, a shroud disposed about the hub, an airflow path between the hub and the shroud, multiple first fuel outlets disposed on the hub, and multiple swirl vanes disposed in the airflow path downstream from the multiple first fuel outlets.
摘要翻译：系统包括燃料喷嘴。燃料喷嘴包括轮毂，围绕毂设置的护罩，轮毂和护罩之间的气流路径，设置在轮毂上的多个第一燃料出口以及设置在多个第一燃料出口下游的气流通道中的多个涡流叶片。

4. 发明申请

US20130086910A1 SYSTEM FOR FUEL INJECTION IN A FUEL NOZZLE 有权
标题翻译：燃油喷嘴燃油喷射系统
公开(公告)号：US20130086910A1
公开(公告)日：2013-04-11
申请号：US13269510
申请日：2011-10-07
申请人： Abdul Rafey Khan , Bradley Donald Crawley , Donald Mark Bailey , Ajay Pratap Singh
发明人： Abdul Rafey Khan , Bradley Donald Crawley , Donald Mark Bailey , Ajay Pratap Singh
IPC分类号： F23R3/28
CPC分类号： F23R3/286 , F23C2900/07001 , F23D2900/14021 , F23R3/14 , F23R3/36 , F23R2900/00013
摘要： A system includes a fuel nozzle. The fuel nozzle includes a hub, a shroud disposed about the hub, an airflow path between the hub and the shroud, multiple first fuel outlets disposed on the hub, and multiple swirl vanes disposed in the airflow path downstream from the multiple first fuel outlets.
摘要翻译：系统包括燃料喷嘴。燃料喷嘴包括轮毂，围绕毂设置的护罩，轮毂和护罩之间的气流路径，设置在轮毂上的多个第一燃料出口以及设置在多个第一燃料出口下游的气流通道中的多个涡流叶片。

5. 发明授权

US08850822B2 System for pre-mixing in a fuel nozzle 有权
标题翻译：用于在燃料喷嘴中预混合的系统
公开(公告)号：US08850822B2
公开(公告)日：2014-10-07
申请号：US13012746
申请日：2011-01-24
申请人： Nishant Govindbhai Parsania , Ajay Pratap Singh
发明人： Nishant Govindbhai Parsania , Ajay Pratap Singh
IPC分类号： F02C1/00 , F23R3/36 , F23R3/14 , F23R3/28
CPC分类号： F23R3/36 , F23C2900/07001 , F23R3/14 , F23R3/286
摘要： A system includes a fuel nozzle. The fuel nozzle includes a hub having an axis, a shroud disposed about the hub, an airflow path between the hub and the shroud, multiple vanes extending between the hub and the shroud, and a first fuel path leading to multiple first fuel outlets disposed on the multiple vanes. The fuel nozzle also includes a second fuel path leading to multiple second fuel outlets disposed on at least one of the hub and/or the shroud, wherein the multiple second fuel outlets are disposed at an axial distance upstream from a downstream end of the hub.
摘要翻译：系统包括燃料喷嘴。燃料喷嘴包括具有轴线的轮毂，围绕毂设置的护罩，轮毂和护罩之间的气流路径，在轮毂和护罩之间延伸的多个叶片，以及通向多个第一燃料出口的第一燃料路径，多叶片。燃料喷嘴还包括通向设置在轮毂和/或护罩中的至少一个上的多个第二燃料出口的第二燃料通路，其中多个第二燃料出口设置在距毂的下游端的上游轴向距离处。

6. 发明授权

US09458456B2 Methods and compositions for the diagnosis, classification, and treatment of cancer 有权
标题翻译：用于诊断，分类和治疗癌症的方法和组合物
公开(公告)号：US09458456B2
公开(公告)日：2016-10-04
申请号：US14007938
申请日：2012-03-30
申请人： Ajay Pratap Singh , Sanjeev Srivastava , Seema Singh
发明人： Ajay Pratap Singh , Sanjeev Srivastava , Seema Singh
IPC分类号： C12N15/113 , C12Q1/68 , G01N33/574 , G01N33/50
CPC分类号： C12N15/1135 , A61K31/337 , A61K31/713 , C12N15/113 , C12N2310/11 , C12N2310/111 , C12N2310/14 , C12N2310/141 , C12N2310/531 , C12N2320/31 , C12Q1/6886 , C12Q2600/112 , C12Q2600/158 , G01N33/5011 , G01N33/57434 , G01N33/57438 , G01N33/5748 , G01N2333/47
摘要： Some embodiments of the present technology relate to methods and compositions for the diagnosis and treatment of cancer. Some embodiments include methods and compositions for the diagnosis and treatment of castration-resistant prostate cancer. Some embodiments include methods and compositions for the diagnosis and treatment of pancreatic cancer.
摘要翻译：本技术的一些实施方案涉及用于诊断和治疗癌症的方法和组合物。一些实施方案包括用于诊断和治疗去势抗性前列腺癌的方法和组合物。一些实施方案包括用于诊断和治疗胰腺癌的方法和组合物。

7. 发明申请

US20120324896A1 PREMIXER FUEL NOZZLE FOR GAS TURBINE ENGINE 有权
标题翻译：优质燃油喷嘴用于气体涡轮发动机
公开(公告)号：US20120324896A1
公开(公告)日：2012-12-27
申请号：US13170133
申请日：2011-06-27
申请人： Kwanwoo Kim , Nishant Govindbhai Parsania , Ajay Pratap Singh
发明人： Kwanwoo Kim , Nishant Govindbhai Parsania , Ajay Pratap Singh
IPC分类号： F02C7/22
CPC分类号： F23C7/004 , F23C2900/07001 , F23R3/286
摘要： In an embodiment, a system includes a turbine fuel nozzle having a hub with an axis, a shroud surrounding the hub along the axis, an air flow path between the hub and the shroud, and a fuel flow path. The turbine fuel nozzle also includes a swirl vane extending between the hub and the shroud in a radial direction relative to the axis. The swirl vane includes a fuel inlet coupled to the fuel flow path, a fuel chamber extending from the fuel inlet, and a plurality of fuel outlets extending from the fuel chamber to the air flow path. The plurality of fuel outlets is positioned at an axial distance of at least approximately ⅔ of an axial length of the fuel chamber downstream from an upstream point along an upstream edge of the fuel chamber.
摘要翻译：在一个实施例中，系统包括涡轮燃料喷嘴，其具有带有轴的轮毂，围绕轴线的轮毂的护罩，轮毂和护罩之间的空气流动路径以及燃料流动路径。涡轮燃料喷嘴还包括在毂和护罩之间沿相对于轴线的径向方向延伸的旋流叶片。涡旋叶片包括联接到燃料流动路径的燃料入口，从燃料入口延伸的燃料室和从燃料室延伸到空气流动路径的多个燃料出口。多个燃料出口被定位在燃料室的沿着燃料室的上游边缘的上游点下游的燃料室的轴向长度的至少近似⅔的轴向距离处。

8. 发明申请

US20120111013A1 SYSTEM FOR DIRECTING AIR FLOW IN A FUEL NOZZLE ASSEMBLY 审中-公开
标题翻译：用于指导燃油喷嘴组件中的空气流的系统
公开(公告)号：US20120111013A1
公开(公告)日：2012-05-10
申请号：US12941808
申请日：2010-11-08
申请人： Nishant Govindbhai Parsania , Ajay Pratap Singh
发明人： Nishant Govindbhai Parsania , Ajay Pratap Singh
IPC分类号： F02C7/22 , B05B1/28
CPC分类号： F23R3/54 , F23C7/004 , F23D2900/00003 , F23D2900/14004 , F23R3/14 , F23R3/16 , F23R3/286
摘要： According to various embodiments, a system includes a fuel nozzle assembly. The fuel nozzle assembly includes a hub, a shroud disposed about the hub, a flow sleeve disposed about the shroud, and an air flow path extending between the flow sleeve and the shroud in an upstream direction toward an opening region between the shroud and the hub, wherein the air flow path extends between the hub and the shroud in a downstream direction from the opening region toward an outlet region of the fuel nozzle assembly. The fuel nozzle assembly also includes a fuel flow path extending to at least one fuel port along the air flow path, and a flow guide disposed along the air flow path in the opening region, wherein the flow guide includes a first guide portion configured to guide an air flow radially outward from the hub toward the shroud.
摘要翻译：根据各种实施例，系统包括燃料喷嘴组件。燃料喷嘴组件包括轮毂，围绕轮毂设置的护罩，围绕护罩设置的流动套筒，以及沿着上游方向在流动套管和护罩之间延伸的空气流动通道，该空气流动路径朝向护罩和轮毂之间的开口区域其中所述空气流动路径在所述轮毂和所述护罩之间沿着从所述开口区域朝向所述燃料喷嘴组件的出口区域的下游方向延伸。燃料喷嘴组件还包括沿着空气流动路径延伸到至少一个燃料端口的燃料流动路径和沿开口区域中的空气流动路径布置的流动引导件，其中流动引导件包括构造成引导的第一引导部分从轮毂向护罩径向向外的空气流。

9. 发明授权

US09260948B2 Multi-level reservoir history matching 有权
标题翻译：多级油藏历史匹配
公开(公告)号：US09260948B2
公开(公告)日：2016-02-16
申请号：US13563270
申请日：2012-07-31
申请人： Marko Maucec , Gustavo Carvajal , Seyed M. Mirzadeh , Ajay Pratap Singh , Hasnain A. Khan , Luigi A. Saputelli
发明人： Marko Maucec , Gustavo Carvajal , Seyed M. Mirzadeh , Ajay Pratap Singh , Hasnain A. Khan , Luigi A. Saputelli
IPC分类号： G06G7/48 , G06F7/60 , E21B43/00 , G01V99/00
CPC分类号： E21B43/00 , G01V99/00
摘要： The present disclosure describes systems and methods for performing multi-level reservoir history matching. At least some illustrative embodiments include a method that includes generating a first history-matched model using at least one updated model parameter derived from one or more existing model parameters, generating a set of second history-matched models by applying a probabilistic inversion to the first history-matched model, and deriving a set of third history-matched models from the set of second history-matched models. The method further includes generating dynamic simulation realization sets using each of the set of third history-matched models, ranking each of the set of third history-matched models based at least in part on the dynamic simulation realization sets, and presenting a production forecast to a user based on the highest ranked third history-matched models.
摘要翻译：本公开描述了用于执行多级油藏历史匹配的系统和方法。至少一些说明性实施例包括一种方法，其包括使用从一个或多个现有模型参数导出的至少一个更新模型参数生成第一历史匹配模型，通过将概率反演应用于第一历史匹配模型历史匹配模型，并从一组第二历史匹配模型中推导出一组第三历史匹配模型。所述方法还包括使用所述一组第三历史匹配模型中的每一者生成动态模拟实现集合，至少部分地基于所述动态模拟实现集合对所述第三历史匹配模型集合中的每一者进行排序，并将生产预测呈现给基于最高排名第三的历史匹配模型的用户。

10. 发明授权

US09046262B2 Premixer fuel nozzle for gas turbine engine 有权
标题翻译：燃气涡轮发动机预混合燃料喷嘴
公开(公告)号：US09046262B2
公开(公告)日：2015-06-02
申请号：US13170133
申请日：2011-06-27
申请人： Kwanwoo Kim , Nishant Govindbhai Parsania , Ajay Pratap Singh
发明人： Kwanwoo Kim , Nishant Govindbhai Parsania , Ajay Pratap Singh
IPC分类号： F02C7/22 , F23R3/14 , F23C7/00 , F23R3/28
CPC分类号： F23C7/004 , F23C2900/07001 , F23R3/286
摘要： In an embodiment, a system includes a turbine fuel nozzle having a hub with an axis, a shroud surrounding the hub along the axis, an air flow path between the hub and the shroud, and a fuel flow path. The turbine fuel nozzle also includes a swirl vane extending between the hub and the shroud in a radial direction relative to the axis. The swirl vane includes a fuel inlet coupled to the fuel flow path, a fuel chamber extending from the fuel inlet, and a plurality of fuel outlets extending from the fuel chamber to the air flow path. The plurality of fuel outlets is positioned at an axial distance of at least approximately ⅔ of an axial length of the fuel chamber downstream from an upstream point along an upstream edge of the fuel chamber.
摘要翻译：在一个实施例中，系统包括涡轮燃料喷嘴，其具有带有轴的轮毂，围绕轴线的轮毂的护罩，轮毂和护罩之间的空气流动路径以及燃料流动路径。涡轮燃料喷嘴还包括在毂和护罩之间沿相对于轴线的径向方向延伸的旋流叶片。涡旋叶片包括联接到燃料流动路径的燃料入口，从燃料入口延伸的燃料室和从燃料室延伸到空气流动路径的多个燃料出口。多个燃料出口被定位在燃料室的沿着燃料室的上游边缘的上游点下游的燃料室的轴向长度的至少近似⅔的轴向距离处。

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