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1. 发明申请

US20130283810A1 COMBUSTION NOZZLE AND A RELATED METHOD THEREOF 审中-公开
标题翻译：燃烧喷嘴及其相关方法
公开(公告)号：US20130283810A1
公开(公告)日：2013-10-31
申请号：US13459930
申请日：2012-04-30
申请人： Uyigue Omoma Idahosa , Keith Robert McManus , Anthony Robert Brand , Hasan Karim , Michael John Hughes
发明人： Uyigue Omoma Idahosa , Keith Robert McManus , Anthony Robert Brand , Hasan Karim , Michael John Hughes
IPC分类号： F02C3/00 , B21K3/00 , F23R3/28
CPC分类号： F23R3/286 , F23D14/58 , Y02E20/16 , Y10T29/49231
摘要： A combustion nozzle includes at least one passage having a mixing section and an exit section. The mixing section includes an air inlet, and a fuel inlet. The mixing section has a first length and a first diameter. The exit section has a second length different from the first length, and a second diameter different from the first diameter.
摘要翻译：燃烧喷嘴包括具有混合部分和出口部分的至少一个通道。混合部分包括空气入口和燃料入口。混合部分具有第一长度和第一直径。出口部分具有不同于第一长度的第二长度和与第一直径不同的第二直径。

2. 发明申请

US20120154813A1 SYSTEM AND METHOD FOR REAL-TIME MEASUREMENT OF EQUIVALENCE RATIO OF GAS FUEL MIXTURE 有权
标题翻译：气体燃料混合物等效比的实时测量系统与方法
公开(公告)号：US20120154813A1
公开(公告)日：2012-06-21
申请号：US12971154
申请日：2010-12-17
申请人： Hejie Li , Shawn David Wehe , Keith Robert McManus
发明人： Hejie Li , Shawn David Wehe , Keith Robert McManus
IPC分类号： G01N21/00 , B24B49/00
CPC分类号： G01J3/433 , F02C9/26 , F02D41/1439 , F02D41/1451 , F05D2260/80 , G01N21/3504 , G01N21/359 , G01N21/39 , G01N2021/399
摘要： A real-time monitoring of an equivalence ratio of a gas-fuel mixture of a gas turbine engine is provided. The system includes multiple optical probes arranged on a plurality of fuel nozzles for transmitting laser beams directly through a gas-fuel mixture or indirectly by reflecting the laser beams from a surface of a centerbody or burner tube of the fuel nozzle. The system also includes one or more detectors to measure the transmitted laser beams from the multiple optical probes. Further, the system includes a data acquisition subsystem for acquiring and processing signals from the one or more detectors to determine the equivalence ratio of the gas-fuel mixture of the nozzle.
摘要翻译：提供了对燃气轮机的气体燃料混合物的当量比的实时监测。该系统包括布置在多个燃料喷嘴上的多个光学探针，用于直接通过气体 - 燃料混合物传输激光束，或间接地通过从燃料喷嘴的中心体或燃烧器管的表面反射激光束。该系统还包括一个或多个检测器，用于测量来自多个光学探针的透射的激光束。此外，该系统包括用于获取和处理来自一个或多个检测器的信号的数据采集子系统，以确定喷嘴的气体 - 燃料混合物的当量比。

3. 发明申请

US20100103424A1 THREE-DIMENSIONAL OPTICAL SENSOR AND SYSTEM FOR COMBUSTION SENSING AND CONTROL 有权
标题翻译：三维光学传感器和用于燃烧感测和控制的系统
公开(公告)号：US20100103424A1
公开(公告)日：2010-04-29
申请号：US12256754
申请日：2008-10-23
申请人： Lewis Berkley Davis, JR. , Keith Robert McManus
发明人： Lewis Berkley Davis, JR. , Keith Robert McManus
IPC分类号： G01J3/50
CPC分类号： G01N21/72 , F23N5/082 , F23N2041/20 , G01J5/0014 , G01J5/0018 , G01J5/08 , G01J5/0806 , G01J5/0862 , G01N21/76 , G01N2021/1785 , G01N2021/8416 , H01L27/146
摘要： A system includes an optical sensor that optically measures and spatially resolves in three dimensions at least one chemical species within a flame produced by a device and a component that correlates the three dimensionally measured at least one chemical species to at least one parameter of the device.
摘要翻译：一种系统包括光学传感器，其光学测量并在空间上分辨由装置产生的火焰内的至少一种化学物质和将三维测量的至少一种化学物质与装置的至少一个参数相关联的部件。

4. 发明申请

US20110008737A1 OPTICAL SENSORS FOR COMBUSTION CONTROL 审中-公开
标题翻译：用于燃烧控制的光学传感器
公开(公告)号：US20110008737A1
公开(公告)日：2011-01-13
申请号：US12484447
申请日：2009-06-15
申请人： Keith Robert McManus , Lewis Berkley Davis, JR.
发明人： Keith Robert McManus , Lewis Berkley Davis, JR.
IPC分类号： F23N5/08
CPC分类号： F23N1/022 , F23N5/082 , F23N2029/20 , F23N2041/20 , F23R2900/00013 , G01J3/02 , G01J3/0208 , G01J3/0237 , G01J3/0264 , G01J3/36 , G01N21/72
摘要： Certain embodiments of the invention may include systems and methods for providing optical sensors for combustion control. According to an example embodiment of the invention, a method for controlling combustion parameters associated with a gas turbine combustor is provided. The method can include providing at least one optical path adjacent to a flame region in the combustor, detecting at least a portion of the light emission from the flame region within the at least one optical path, and controlling at least one of the combustion parameters based in part on the detected light emission.
摘要翻译：本发明的某些实施例可以包括用于提供用于燃烧控制的光学传感器的系统和方法。根据本发明的示例性实施例，提供了一种用于控制与燃气轮机燃烧器相关联的燃烧参数的方法。该方法可以包括提供与燃烧器中的火焰区域相邻的至少一个光路，检测来自至少一个光路内的火焰区域的光发射的至少一部分，并基于燃烧参数中的至少一个来控制部分地检测到发光。

5. 发明授权

US07131260B2 Multiple detonation initiator for frequency multiplied pulsed detonation combustion 有权
标题翻译：多重爆震引发器用于频率相加脉冲爆震燃烧
公开(公告)号：US07131260B2
公开(公告)日：2006-11-07
申请号：US10870898
申请日：2004-06-18
申请人： Anthony John Dean , Keith Robert McManus , Venkat Eswarlu Tangirala
发明人： Anthony John Dean , Keith Robert McManus , Venkat Eswarlu Tangirala
IPC分类号： F02C5/00 , F02G1/00 , F02G3/00
CPC分类号： F02C5/00 , F02K7/02 , F23R7/00
摘要： The present invention is a pulse detonation combustion system, having a plurality of detonation initiation devices coupled to a main combustion chamber, where each of the detonation initiation devices is operating out-of-phase with each other. Each of the detonation initiation devices assists in the initiation of a detonation in the main combustion chamber, out-of-phase from each other such that the operational frequency of the pulse detonation combustion system is related to the number of detonation initiation devices multiplied by the operational frequency of a single detonation initiation device.
摘要翻译：本发明是一种脉冲爆震燃烧系统，其具有耦合到主燃烧室的多个爆震启动装置，其中每个爆震启动装置彼此不同相运行。每个爆震启动装置有助于在主燃烧室中引起爆震，彼此不相位，使得脉冲爆震燃烧系统的操作频率与爆震开始装置的数量相乘单个引爆装置的工作频率。

6. 发明授权

US08625098B2 System and method for real-time measurement of equivalence ratio of gas fuel mixture 有权
标题翻译：实时测量气体燃料混合物当量比的系统和方法
公开(公告)号：US08625098B2
公开(公告)日：2014-01-07
申请号：US12971154
申请日：2010-12-17
申请人： Hejie Li , Shawn David Wehe , Keith Robert McManus
发明人： Hejie Li , Shawn David Wehe , Keith Robert McManus
IPC分类号： G01N21/00 , G01J3/433 , G01N21/39
CPC分类号： G01J3/433 , F02C9/26 , F02D41/1439 , F02D41/1451 , F05D2260/80 , G01N21/3504 , G01N21/359 , G01N21/39 , G01N2021/399
摘要： A real-time monitoring of an equivalence ratio of a gas-fuel mixture of a gas turbine engine is provided. The system includes multiple optical probes arranged on a plurality of fuel nozzles for transmitting laser beams directly through a gas-fuel mixture or indirectly by reflecting the laser beams from a surface of a centerbody or burner tube of the fuel nozzle. The system also includes one or more detectors to measure the transmitted laser beams from the multiple optical probes. Further, the system includes a data acquisition subsystem for acquiring and processing signals from the one or more detectors to determine the equivalence ratio of the gas-fuel mixture of the nozzle.
摘要翻译：提供了对燃气轮机的气体燃料混合物的当量比的实时监测。该系统包括布置在多个燃料喷嘴上的多个光学探针，用于直接通过气体 - 燃料混合物传输激光束，或间接地通过从燃料喷嘴的中心体或燃烧器管的表面反射激光束。该系统还包括一个或多个检测器，用于测量来自多个光学探针的透射的激光束。此外，该系统包括用于获取和处理来自一个或多个检测器的信号的数据采集子系统，以确定喷嘴的气体 - 燃料混合物的当量比。

7. 发明授权

US08456634B2 Optical interrogation sensors for combustion control 有权
标题翻译：用于燃烧控制的光学询问传感器
公开(公告)号：US08456634B2
公开(公告)日：2013-06-04
申请号：US12484466
申请日：2009-06-15
申请人： Keith Robert McManus , Lewis Berkley Davis, Jr.
发明人： Keith Robert McManus , Lewis Berkley Davis, Jr.
IPC分类号： G01N21/00
CPC分类号： G01N21/72 , F02C9/00 , F02D41/1451 , F23N5/082 , F23N2029/00 , F23N2041/20
摘要： Certain embodiments of the invention may include systems and methods for providing optical interrogation sensors for combustion control. According to an example embodiment of the invention, a method for controlling combustion parameters associated with a gas turbine combustor is provided. The method can include providing an optical path through the gas turbine combustor, propagating light along the optical path, measuring absorption of the light within the gas turbine combustor, and controlling at least one of the combustion parameters based at least in part on the measured absorption.
摘要翻译：本发明的某些实施例可以包括用于提供用于燃烧控制的光学询问传感器的系统和方法。根据本发明的示例性实施例，提供了一种用于控制与燃气轮机燃烧器相关联的燃烧参数的方法。该方法可以包括提供通过燃气轮机燃烧器的光路，沿着光路传播光，测量燃气轮机燃烧器内的光的吸收，以及至少部分地基于所测量的吸收来控制至少一个燃烧参数。

8. 发明申请

US20120131926A1 ADVANCED LASER IGNITION SYSTEMS FOR GAS TURBINES INCLUDING AIRCRAFT ENGINES 有权
标题翻译：用于包括飞机发动机的气体涡轮机的先进激光点火系统
公开(公告)号：US20120131926A1
公开(公告)日：2012-05-31
申请号：US12956191
申请日：2010-11-30
申请人： Herbert Kopecek , Sara Rocci Denis , Keith Robert McManus , Michael Breit
发明人： Herbert Kopecek , Sara Rocci Denis , Keith Robert McManus , Michael Breit
IPC分类号： F02C7/264 , F02P23/04
CPC分类号： F02C7/264 , F02P23/04 , F23R2900/00006
摘要： A laser ignition system for an internal combustion engine, and more specifically a gas turbine engine, is provided. The system comprises at least one laser light source configured to generate a laser beam and an optical beam guidance component. The optical beam guidance component is configured to transmit the laser beam to irradiate on an oxygenated fuel mixture supplied into the combustion chamber at a region of highest ignitability to generate a combustor flame in a flame region. The system further includes an integrated control diagnostic component configured to detect at least a portion of a light emission and operable to control one or more combustion parameters based in part on the detected light emission. The system further includes additional enhanced ignition control configurations. A method for igniting a fuel mixture in an internal combustion engine is also presented.
摘要翻译：提供了一种用于内燃机，特别是燃气涡轮发动机的激光点火系统。该系统包括被配置为产生激光束和光束引导部件的至少一个激光光源。光束引导部件被配置为透射激光束以在最高可燃性的区域供应到燃烧室中的氧化燃料混合物照射以在火焰区域中产生燃烧器火焰。该系统还包括集成控制诊断部件，其被配置为检测至少一部分发光并可操作以部分地基于检测到的光发射来控制一个或多个燃烧参数。该系统还包括额外增强的点火控制配置。还提出了一种用于点燃内燃机中的燃料混合物的方法。

9. 发明申请

US20140007584A1 SYSTEM AND METHOD FOR REDUCING PRESSURE OSCILLATIONS WITHIN A GAS TURBINE ENGINE 有权
标题翻译：用于降低气体涡轮发动机内压力振荡的系统和方法
公开(公告)号：US20140007584A1
公开(公告)日：2014-01-09
申请号：US13538836
申请日：2012-06-29
申请人： Zekai Hong , Joel Meier Haynes , Keith Robert McManus , John Thomas Herbon
发明人： Zekai Hong , Joel Meier Haynes , Keith Robert McManus , John Thomas Herbon
IPC分类号： F02C7/232
CPC分类号： F02C7/232 , F02C9/26 , F05D2270/14 , F23R2900/00013
摘要： In one embodiment, a system for reducing pressure oscillations within a gas turbine engine includes at least one fuel injector configured to inject fuel into a combustor. The system also includes a valve fluidly coupled to the at least one fuel injector. The system further includes a controller communicatively coupled to the valve. The controller is configured to cycle the valve between an open position and a closed position at a first frequency and a first duty cycle while a magnitude of pressure oscillations within the combustor is less than a threshold value, to cycle the valve between the open position and the closed position at a second frequency and a second duty cycle while the magnitude of the pressure oscillations within the combustor is greater than or equal to the threshold value, and to adjust the second frequency based on a measured frequency of the pressure oscillations.
摘要翻译：在一个实施例中，用于减少燃气涡轮发动机内的压力振荡的系统包括构造成将燃料喷射到燃烧器中的至少一个燃料喷射器。该系统还包括流体地联接到至少一个燃料喷射器的阀。该系统还包括通信地联接到阀的控制器。控制器被配置为在第一频率和第一占空比的情况下将阀在打开位置和关闭位置之间循环，同时燃烧器内的压力振荡的幅度小于阈值，以使阀在打开位置和在第二频率和第二占空比下的关闭位置，同时燃烧器内的压力振荡的大小大于或等于阈值，并且基于测量的压力振荡频率来调节第二频率。

10. 发明申请

US20100313572A1 OPTICAL INTERROGATION SENSORS FOR COMBUSTION CONTROL 有权
标题翻译：用于燃烧控制的光学传感器
公开(公告)号：US20100313572A1
公开(公告)日：2010-12-16
申请号：US12484466
申请日：2009-06-15
申请人： Keith Robert McManus , Lewis Berkley Davis, JR.
发明人： Keith Robert McManus , Lewis Berkley Davis, JR.
IPC分类号： F02C9/00
CPC分类号： G01N21/72 , F02C9/00 , F02D41/1451 , F23N5/082 , F23N2029/00 , F23N2041/20
摘要： Certain embodiments of the invention may include systems and methods for providing optical interrogation sensors for combustion control. According to an example embodiment of the invention, a method for controlling combustion parameters associated with a gas turbine combustor is provided. The method can include providing an optical path through the gas turbine combustor, propagating light along the optical path, measuring absorption of the light within the gas turbine combustor, and controlling at least one of the combustion parameters based at least in part on the measured absorption.
摘要翻译：本发明的某些实施例可以包括用于提供用于燃烧控制的光学询问传感器的系统和方法。根据本发明的示例性实施例，提供了一种用于控制与燃气轮机燃烧器相关联的燃烧参数的方法。该方法可以包括提供通过燃气轮机燃烧器的光路，沿着光路传播光，测量燃气轮机燃烧器内的光的吸收，以及至少部分地基于所测量的吸收来控制至少一个燃烧参数。

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