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1. 发明授权

US06775983B2 Flow control device for a combustor 失效
标题翻译：燃烧器流量控制装置
公开(公告)号：US06775983B2
公开(公告)日：2004-08-17
申请号：US10063864
申请日：2002-05-21
申请人： Simon Ralph Sanderson , Paolo Graziosi
发明人： Simon Ralph Sanderson , Paolo Graziosi
IPC分类号： F23R304
CPC分类号： F23R3/26 , F23R3/14
摘要： A flow control device for a combustor is provided in which the flow control device comprises a shroud having a first end and a second end wherein the second end is coupled to the combustor. The shroud is disposed to receive a primary fluid and disposed to direct the primary fluid into the combustor. In addition, the shroud further comprises a plurality of ports disposed therein wherein the ports are oriented to extract a portion of a flow from a flow path of the primary fluid so as to control a flow rate of the primary fluid through the shroud.
摘要翻译：提供了一种用于燃烧器的流量控制装置，其中流量控制装置包括具有第一端和第二端的护罩，其中第二端联接到燃烧器。护罩被设置成接收初级流体并且设置成将初级流体引导到燃烧器中。此外，护罩还包括设置在其中的多个端口，其中端口被定向成从主要流体的流动路径提取流体的一部分，以便控制主流体通过护罩的流速。

2. 发明授权

US06989209B2 Power generation method 失效
标题翻译：发电方式
公开(公告)号：US06989209B2
公开(公告)日：2006-01-24
申请号：US10330748
申请日：2002-12-27
申请人： Simon Ralph Sanderson
发明人： Simon Ralph Sanderson
IPC分类号： H01M8/04 , H01M2/00
CPC分类号： H01M8/04097 , H01M8/04022 , H01M8/04111 , H01M2008/1095 , H01M2008/1293 , H01M2008/147 , H01M2250/402 , H01M2250/405 , Y02B90/12 , Y02B90/16 , Y02E20/16 , Y02E60/526
摘要： A fuel cell module includes at least one fuel cell stack comprising a number of fuel cell units. An inlet is configured to receive an oxidant flow for supplying the fuel cell stack. An outlet is configured to exhaust an exhaust oxidant flow generated by the fuel cell stack. A recirculation path is configured to convey at least about thirty percent (30%) of the exhaust oxidant flow from the outlet to the inlet as a recirculated exhaust flow, for combination with the new oxidant flow to form the oxidant flow to the fuel cell stack.
摘要翻译：燃料电池模块包括至少一个包括多个燃料电池单元的燃料电池堆。入口构造成接收用于供应燃料电池堆的氧化剂流。出口被配置为排出由燃料电池堆产生的排气氧化剂流。再循环路径被配置为将排气氧化剂流的至少约百分之三十（30％）作为再循环排气流从出口输送到入口，用于与新的氧化剂流组合以形成到燃料电池堆的氧化剂流。

3. 发明授权

US06565255B2 Sensors and methodology for improved turbine exhaust gas temperature measurements 失效
公开(公告)号：US06565255B2
公开(公告)日：2003-05-20
申请号：US09948439
申请日：2001-09-10
申请人： Simon Ralph Sanderson
发明人： Simon Ralph Sanderson
IPC分类号： G01K702
CPC分类号： G01K3/06
摘要： A method for characterizing the parameters of a normally occurring turbine exhaust gas temperature profile is provided. From that characterization the characteristics of a filter function to eliminate or significantly reduce the strength of aliased signals from that normally occurring pattern are established. Sensors to provide filtering functions for that purpose include a distributed gradient thermocouple system and a resistance thermometer system. Examples of such sensor systems are disclosed. The method and related sensors improve the detection limits associated with exhaust gas temperature profiles used to monitor, diagnose, and control gas turbines.

4. 发明授权

US06752018B2 Method and apparatus for characterizing an acoustic impedance 有权
标题翻译：用于表征声阻抗的方法和装置
公开(公告)号：US06752018B2
公开(公告)日：2004-06-22
申请号：US10159267
申请日：2002-06-03
申请人： Jeffrey Scott Goldmeer , Simon Ralph Sanderson
发明人： Jeffrey Scott Goldmeer , Simon Ralph Sanderson
IPC分类号： G01N2916
CPC分类号： G01N29/46 , G01N29/09 , G01N29/2462 , G01N2291/02872 , G01N2291/044 , G01N2291/103
摘要： In one embodiment of the present invention, an apparatus for characterizing an acoustic impedance of an engineering component acoustically coupled to an acoustic waveguide includes: a pressure measurement apparatus adapted to be moved and to be disposed to measure pressure signals, the pressure signals being measured at respective ones of a plurality of predetermined locations along the acoustic waveguide; an exciter adapted to excite the acoustic waveguide with an excitation signal; a data collection module adapted to incorporate the pressure signals from the pressure measurement apparatus into a pressure signal set; a transform module adapted to transform the pressure signal set to a frequency domain set; a wave shape identifier adapted to identify a plurality of wave shape parameters from the frequency domain set; and a statistical computer adapted to compute from the frequency domain set a statistical measure for the wave shape parameters, the statistical measure being selected from the group consisting of residual variance, correlation coefficient, F-statistic, p-statistic, and confidence interval.
摘要翻译：在本发明的一个实施例中，用于表征声学耦合到声波导的工程部件的声阻抗的装置包括：压力测量装置，适于移动并被设置成测量压力信号，压力信号是在沿着声波导的多个预定位置中的相应的一个; 激励器，其适于用激励信号激励声波导; 数据收集模块，适于将来自压力测量装置的压力信号并入压力信号组; 变换模块，其适于将所述压力信号集合变换为频域集合; 波形标识符，用于从所述频域集中识别多个波形参数; 以及适于从频域计算出的波形参数的统计测量的统计计算机，所述统计测量从由残差方差，相关系数，F统计量，p统计量和置信区间组成的组中选择。

5. 发明授权

US06968693B2 Method and apparatus for reducing gas turbine engine emissions 失效
标题翻译：减少燃气轮机发动机排放的方法和装置
公开(公告)号：US06968693B2
公开(公告)日：2005-11-29
申请号：US10667041
申请日：2003-09-22
申请人： Andrei Colibaba-Evulet , Michael John Bowman , Simon Ralph Sanderson , Anthony John Dean
发明人： Andrei Colibaba-Evulet , Michael John Bowman , Simon Ralph Sanderson , Anthony John Dean
IPC分类号： F23R3/14 , F02C1/00 , F02C7/00 , F02C7/232 , F02C9/26 , F23R3/00 , F23R3/02 , F23R3/28 , F23R3/30 , F23R3/32 , F23R3/34 , F23R3/42 , F23R3/54
CPC分类号： F23R3/54 , F23R3/002 , F23R3/14 , F23R3/34 , F23R2900/03044 , Y02T50/675
摘要： A low emission turbine includes a reverse flow can-type combustor that generally includes a primary and secondary fuel delivery system that can be independently controlled to produce low CO, UHC, and NOx emissions at design set point and at conditions other than design set point. The reverse flow can-type combustor generally includes an annularly arranged array of swirler and mixer assemblies within the combustor, wherein each swirler and mixer in the array includes a primary and secondary fuel delivery system that can be independently controlled. Also disclosed herein is a can-type combustor that includes fluid passageways that perpendicularly impinge the outer surface of a heat shield. Processes for operating the can-type combustors are also disclosed.
摘要翻译：低排放涡轮机包括逆流罐式燃烧器，其通常包括主燃料输送系统和辅助燃料输送系统，其可独立控制以在设计设定点和设计设定点以外的条件下产生低CO，UHC和NOx排放。反向流动罐式燃烧器通常包括在燃烧器内的环形排列的旋流器和混合器组件，其中阵列中的每个旋流器和混合器包括可以独立控制的主要和次要燃料输送系统。本文还公开了一种罐型燃烧器，其包括垂直地撞击隔热罩的外表面的流体通道。还公开了用于操作罐式燃烧器的方法。

6. 发明授权

US06517241B1 Sensors and methodology for improved turbine exhaust gas temperature measurements 失效
公开(公告)号：US06517241B1
公开(公告)日：2003-02-11
申请号：US09579231
申请日：2000-05-30
申请人： Simon Ralph Sanderson
发明人： Simon Ralph Sanderson
IPC分类号： G01K702
CPC分类号： G01K3/06
摘要： A method for characterizing the parameters of a normally occurring turbine exhaust gas temperature profile is provided. From that characterization the characteristics of a filter function to eliminate or significantly reduce the strength of aliased signals from that normally occurring pattern are established. Sensors to provide filtering functions for that purpose include a distributed gradient thermocouple system and a resistance thermometer system. Examples of such sensor systems are disclosed. The method and related sensors improve the detection limits associated with exhaust gas temperature profiles used to monitor, diagnose, and control gas turbines.

7. 发明授权

US07260935B2 Method and apparatus for reducing gas turbine engine emissions 失效
标题翻译：减少燃气轮机发动机排放的方法和装置
公开(公告)号：US07260935B2
公开(公告)日：2007-08-28
申请号：US11143266
申请日：2005-06-02
申请人： Andrei Colibaba-Evulet , Michael John Bowman , Simon Ralph Sanderson , Anthony John Dean
发明人： Andrei Colibaba-Evulet , Michael John Bowman , Simon Ralph Sanderson , Anthony John Dean
IPC分类号： F02C1/00
CPC分类号： F23R3/54 , F23R3/002 , F23R3/14 , F23R3/34 , F23R2900/03044 , Y02T50/675
摘要： A low emission turbine includes a reverse flow can-type combustor that generally includes a primary and secondary fuel delivery system that can be independently controlled to produce low CO, UHC, and NOx emissions at design set point and at conditions other than design set point. The reverse flow can-type combustor generally includes an annularly arranged array of swirler and mixer assemblies within the combustor, wherein each swirler and mixer in the array includes a primary and secondary fuel delivery system that can be independently controlled. Also disclosed herein is a can-type combustor that includes fluid passageways that perpendicularly impinge the outer surface of a heat shield. Processes for operating the can-type combustors are also disclosed.
摘要翻译：低排放涡轮机包括逆流罐式燃烧器，其通常包括主燃料输送系统和辅助燃料输送系统，其可独立控制以在设计设定点和设计设定点以外的条件下产生低CO，UHC和NOx排放。反向流动罐式燃烧器通常包括在燃烧器内的环形排列的旋流器和混合器组件，其中阵列中的每个旋流器和混合器包括可以独立控制的主要和次要燃料输送系统。本文还公开了一种罐型燃烧器，其包括垂直地撞击隔热罩的外表面的流体通道。还公开了用于操作罐式燃烧器的方法。

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