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1. 发明申请

US20050276306A1 ESTIMATING COMBUSTOR FLAME TEMPERATURE BASED ON FREQUENCY OF COMBUSTOR DYNAMICS TRANSVERSE MODE 失效
标题翻译：基于COMBUSTOR动态横向模式频率估算燃烧器火焰温度
公开(公告)号：US20050276306A1
公开(公告)日：2005-12-15
申请号：US10856773
申请日：2004-06-01
申请人： Warren Mick , Eamon Gleeson , Willy Ziminsky , Aparna Basker , Fei Han
发明人： Warren Mick , Eamon Gleeson , Willy Ziminsky , Aparna Basker , Fei Han
IPC分类号： F02C9/00 , F23R3/00 , G01K11/26 , G01K11/22
CPC分类号： G01K11/26
摘要： A method of determining the temperature inside a combustion liner without making a direct measurement of the actual temperature. The technique is based on a measurement of the frequency of one of the transverse acoustic modes occurring inside the combustion chamber. The frequency is determined from the transverse geometric dimensions of the combustion chamber and the speed of sound in the gas inside the combustion chamber. The speed of sound in the gas is known from thermodynamics to be a function of gas temperature and gas properties. Thus, from a measurement of the resonant frequency and knowing the combustor dimensions and gas properties, the temperature can be determined with accuracy.
摘要翻译：确定燃烧衬里内的温度而不直接测量实际温度的方法。该技术基于在燃烧室内发生的横向声学模式之一的频率的测量。频率由燃烧室的横向几何尺寸和燃烧室内气体中的声速确定。气体中的声速从热力学已知是气体温度和气体性质的函数。因此，从谐振频率的测量和知道燃烧器尺寸和气体性质，可以准确地确定温度。

2. 发明申请

US20070062196A1 Method and apparatus to detect onset of combustor hardware damage 有权
标题翻译：检测燃烧器硬件损坏发生的方法和装置
公开(公告)号：US20070062196A1
公开(公告)日：2007-03-22
申请号：US11229168
申请日：2005-09-16
申请人： Eamon Gleeson , Warren Mick , George Williams , Fei Han , Shivakumar Srinivasan , Scott Kopcho , Ilan Leibu
发明人： Eamon Gleeson , Warren Mick , George Williams , Fei Han , Shivakumar Srinivasan , Scott Kopcho , Ilan Leibu
IPC分类号： F02C7/00
CPC分类号： F23N5/242 , F23N5/16 , F23N2031/10 , F23N2041/20
摘要： A method for determining when a combustor is experiencing hardware damage includes sensing acoustic vibrations of a plurality of combustor cans, determining a center frequency for each acoustic tone of the sensed acoustic vibrations within a predetermined frequency range, and indicating an alarm when a center frequency of one or more of the combustor cans changes in a different manner compared to a representative center frequency of the plurality of combustor cans.
摘要翻译：一种用于确定燃烧器何时经历硬件损坏的方法包括：感测多个燃烧器罐的声振动，确定预定频率范围内感测到的声振动的每个声音的中心频率，并且当中心频率为与多个燃烧器罐的代表性中心频率相比，一个或多个燃烧器罐以不同的方式改变。

3. 发明申请

US20060248893A1 METHOD AND SYSTEM FOR DETERMINING LEAN BLOW OUT CONDITION FOR GAS TURBINE COMBUSTION CANS 有权
标题翻译：用于确定燃气涡轮机燃烧罐的亮度冷却条件的方法和系统
公开(公告)号：US20060248893A1
公开(公告)日：2006-11-09
申请号：US10908309
申请日：2005-05-06
申请人： Warren Mick , George Williams , Fei Han , Eamon Gleeson , Shiva Srinivasan , Scott Kopcho , Ilan Leibu
发明人： Warren Mick , George Williams , Fei Han , Eamon Gleeson , Shiva Srinivasan , Scott Kopcho , Ilan Leibu
IPC分类号： F02C7/00
CPC分类号： F02C9/00 , F01D21/003 , F05D2270/092 , F05D2270/14 , F05D2270/301 , F23N5/242 , F23N2025/04 , F23N2031/06
摘要： A method for determining a lean blow out condition for a combustor. In an exemplary embodiment, the method includes determining acoustical frequency data for the combustor, determining a combustor flame temperature based on the acoustical frequency data, determining an existing fuel/air ratio in the combustor based on the combustor flame temperature, and comparing the existing fuel/ratio to a lean blow out fuel/air ratio. A lean blow out condition for the combustor is indicated when the existing fuel/air ratio is about equal to the lean blow out fuel/air ratio.
摘要翻译：一种用于确定燃烧器的稀薄吹出条件的方法。在示例性实施例中，该方法包括确定燃烧器的声频数据，基于声频数据确定燃烧器火焰温度，基于燃烧器火焰温度确定燃烧器中的现有燃料/空气比，以及比较现有燃料 /比与精馏燃料/空气比。当现有燃料/空气比约等于稀吹出燃料/空气比时，指示燃烧器的稀薄吹出条件。

4. 发明授权

US06979118B1 Estimating combustor flame temperature based on frequency of combustor dynamics transverse mode 失效
标题翻译：基于燃烧器动态横向模式的频率估算燃烧器火焰温度
公开(公告)号：US06979118B1
公开(公告)日：2005-12-27
申请号：US10856773
申请日：2004-06-01
申请人： Warren James Mick , Eamon P. Gleeson , Willy Steve Ziminsky , Aparna Basker , Fei Han
发明人： Warren James Mick , Eamon P. Gleeson , Willy Steve Ziminsky , Aparna Basker , Fei Han
IPC分类号： F02C9/00 , F23R3/00 , G01K11/26 , G01K11/026
CPC分类号： G01K11/26
摘要： A method of determining the temperature inside a combustion liner without making a direct measurement of the actual temperature. The technique is based on a measurement of the frequency of one of the transverse acoustic modes occurring inside the combustion chamber. The frequency is determined from the transverse geometric dimensions of the combustion chamber and the speed of sound in the gas inside the combustion chamber. The speed of sound in the gas is known from thermodynamics to be a function of gas temperature and gas properties. Thus, from a measurement of the resonant frequency and knowing the combustor dimensions and gas properties, the temperature can be determined with accuracy.
摘要翻译：确定燃烧衬里内的温度而不直接测量实际温度的方法。该技术基于在燃烧室内发生的横向声学模式之一的频率的测量。频率由燃烧室的横向几何尺寸和燃烧室内气体中的声速确定。气体中的声速从热力学已知是气体温度和气体性质的函数。因此，从谐振频率的测量和知道燃烧器尺寸和气体性质，可以准确地确定温度。

5. 发明授权

US06813925B2 Calibration method and system for a dynamic combustor sensor 有权
标题翻译：动态燃烧器传感器的校准方法和系统
公开(公告)号：US06813925B2
公开(公告)日：2004-11-09
申请号：US10161702
申请日：2002-06-05
申请人： Robert Naumiec , Walter Smith , Fei Han , Eamon Gleeson , Robert A. Hedeen
发明人： Robert Naumiec , Walter Smith , Fei Han , Eamon Gleeson , Robert A. Hedeen
IPC分类号： G01L2700
CPC分类号： G01L27/005
摘要： In one embodiment, the invention is a pressure sensor calibration system comprising a pressure chamber in fluid communication with a pressure sensor to be calibrated, the chamber is pressurized to a static pressure level. An oscillating surface on a wall of the chamber imparts a rapid pressure fluctuation in the static pressure level of the chamber. These rapid pressure fluctuations in a high-static pressure level chamber are used to calibrate the pressure sensor.
摘要翻译：在一个实施例中，本发明是一种压力传感器校准系统，其包括与待校准的压力传感器流体连通的压力室，该室被加压至静态压力水平。在室的壁上的摆动表面给出了室的静压水平的快速压力波动。高静态压力水平室中的这些快速压力波动用于校准压力传感器。

6. 发明申请

US20050016255A1 Calibration method and system for a dynamic combustor sensor 审中-公开
标题翻译：动态燃烧器传感器的校准方法和系统
公开(公告)号：US20050016255A1
公开(公告)日：2005-01-27
申请号：US10926010
申请日：2004-08-26
申请人： Robert Naumiec , Walter Smith , Fei Han , Eamon Gleeson , Robert Hedeen
发明人： Robert Naumiec , Walter Smith , Fei Han , Eamon Gleeson , Robert Hedeen
IPC分类号： G01L27/00
CPC分类号： G01L27/005
摘要： In one embodiment, the invention is a pressure sensor calibration system comprising a pressure chamber in fluid communication with a pressure sensor to be calibrated, the chamber is pressurized to a static pressure level. An oscillating surface on a wall of the chamber imparts a rapid pressure fluctuation in the static pressure level of the chamber. These rapid pressure fluctuations in a high-static pressure level chamber are used to calibrate the pressure sensor.
摘要翻译：在一个实施例中，本发明是一种压力传感器校准系统，其包括与待校准的压力传感器流体连通的压力室，该室被加压至静态压力水平。在室的壁上的摆动表面给出了室的静压水平的快速压力波动。高静态压力水平室中的这些快速压力波动用于校准压力传感器。

7. 发明申请

US20140158444A1 MOUNTING STRUCTURE FOR IN-VEHICLE POWER BATTER AND VEHICLE COMPRISING THE SAME 有权
标题翻译：用于车载电源的安装结构和包含它的车辆
公开(公告)号：US20140158444A1
公开(公告)日：2014-06-12
申请号：US14234581
申请日：2012-07-27
申请人： Fei Han , Bengang Yi , Hengshan Zhang
发明人： Fei Han , Bengang Yi , Hengshan Zhang
IPC分类号： B60K1/04
CPC分类号： B60K1/04 , B60K2001/0438 , B60K2001/0472 , H01M2/1083 , H01M2220/20
摘要： A mounting structure for an in-vehicle power battery may be provided. The mounting structure may comprise an upper cover (3), a suspension tray (1) and a bracket (2) for supporting at least a peripheral bottom portion of the suspension tray (1). The suspension tray (1) may be hermetically connected with the upper cover, forming a sealed space for receiving the power battery. The bracket (2) may be detachably fixed to a bottom surface of a body floor in a vehicle. Further, a vehicle (100) comprising the mounting structure described above is also provided.
摘要翻译：可以提供用于车载动力电池的安装结构。安装结构可以包括上盖（3），悬挂托盘（1）和用于支撑悬架托盘（1）的至少周边底部的托架（2）。悬挂托盘（1）可以与上盖气密连接，形成用于接收动力电池的密封空间。支架（2）可以可拆卸地固定在车辆的车身底板的底面上。此外，还提供了包括上述安装结构的车辆（100）。

8. 发明授权

US08469141B2 Acoustic damping device for use in gas turbine engine 有权
标题翻译：用于燃气轮机的声阻尼装置
公开(公告)号：US08469141B2
公开(公告)日：2013-06-25
申请号：US13207074
申请日：2011-08-10
申请人： Shanwu Wang , Fei Han , Mark Anthony Mueller
发明人： Shanwu Wang , Fei Han , Mark Anthony Mueller
IPC分类号： F02K1/00
CPC分类号： F23R3/002 , F02C7/24 , F05D2260/963 , F23M20/005 , F23R2900/00014
摘要： An acoustic dampener comprises a first wall, orifice plate, and second wall. The first wall separates a first fluid source from a second fluid source. The first wall has a hole for allowing fluid communication between the first fluid source and a first cavity of the acoustic dampener. The office plate separates the first cavity of the acoustic dampener from a second cavity of the acoustic dampener. The second wall has a hole for allowing fluid communication between the first cavity of the acoustic dampener in the second cavity of the acoustic dampener. The second wall separates the second cavity of the acoustic dampener from the second fluid source. The second wall has a hole for allowing fluid communication between the second cavity of the acoustic dampener and the second fluid source. In one embodiment, the acoustic dampener is formed in a combustion chamber liner of a gas turbine engine.
摘要翻译：声阻尼器包括第一壁，孔板和第二壁。第一壁将第一流体源与第二流体源分开。第一壁具有用于允许第一流体源和声学缓冲器的第一腔之间的流体连通的孔。办公室板将隔音器的第一腔与声学缓冲器的第二腔分开。第二壁具有用于允许声学缓冲器的第二腔中的声学缓冲器的第一腔之间的流体连通的孔。第二壁将声阻尼器的第二腔与第二流体源分开。第二壁具有用于允许声阻尼器的第二腔和第二流体源之间的流体连通的孔。在一个实施例中，声阻尼器形成在燃气涡轮发动机的燃烧室衬套中。

9. 发明授权

US08408004B2 Resonator assembly for mitigating dynamics in gas turbines 有权
标题翻译：用于减轻燃气轮机动力学的谐振器组件
公开(公告)号：US08408004B2
公开(公告)日：2013-04-02
申请号：US12485505
申请日：2009-06-16
申请人： Lewis Berkley Davis, Jr. , Fei Han , Shiva Srinivasan , Kapil Kumar Singh , Kwanwoo Kim , Venkateswarlu Narra
发明人： Lewis Berkley Davis, Jr. , Fei Han , Shiva Srinivasan , Kapil Kumar Singh , Kwanwoo Kim , Venkateswarlu Narra
IPC分类号： F02C3/00 , F23R3/46
CPC分类号： F23R3/002 , F23M20/005 , F23R2900/00013 , F23R2900/00014
摘要： A combustor for a gas turbine engine and related method is provided in which a plurality of combustor cans are selectively adapted with corresponding resonators. The resonators may, for example, be attached to every can in the consecutive arrangement of combustor cans, every other can, every third can or the like, and may be tuned to the same or first, second, third, etc. frequencies of operation. Such selective tuning is configured to suppress one or more of out-of-phase and in-phase dynamic interaction of streams discharged from adjacent combustor cans by changing the frequencies of pressure oscillation instabilities across the arrangement of consecutive cans.
摘要翻译：提供了一种用于燃气涡轮发动机的燃烧器和相关方法，其中多个燃烧器罐选择性地适应于相应的谐振器。例如，谐振器可以在燃烧器罐的连续布置中，每隔一个可以，每隔三分之一或者类似地连接到每个罐，并且可以调谐到相同或第一，第二，第三等操作频率。这种选择性调谐被配置为通过改变跨连续罐排列的压力振荡不稳定性的频率来抑制从相邻燃烧器罐排出的流的异相和同相动态相互作用中的一个或多个。

10. 发明授权

US08381530B2 System and method for controlling combustion dynamics 有权
标题翻译：控制燃烧动力学的系统和方法
公开(公告)号：US08381530B2
公开(公告)日：2013-02-26
申请号：US12431095
申请日：2009-04-28
申请人： Kapil Kumar Singh , Fei Han , Shiva Srinivasan , Kwanwoo Kim
发明人： Kapil Kumar Singh , Fei Han , Shiva Srinivasan , Kwanwoo Kim
IPC分类号： F02C7/22
CPC分类号： F23D14/48 , F02C7/222 , F02C9/28 , F05D2260/964 , F23D2900/14482 , F23N5/24 , F23R2900/00013
摘要： A tunable fluid flow control system for controlling combustion dynamics in a combustor is disclosed. The control system includes a fuel supply path having an inlet portion, a first diverted portion, a second diverted portion, and an exit portion. A first diverted portion has a first length and a first diameter. A second diverted portion has a second length and a second diameter and spaced apart from the first diverted portion. The first and second diverted portions converge at a merging location. The exit portion is coupled to the merging location of the first and second diverted portions. At least one flow regulation device is coupled to the inlet portion and configured to divert fuel flow to the first and second diverted portions alternately to generate fuel flow perturbations at the merging location.
摘要翻译：公开了一种用于控制燃烧器中的燃烧动力学的可调流体流量控制系统。控制系统包括具有入口部分，第一转向部分，第二转向部分和出口部分的燃料供给路径。第一转向部分具有第一长度和第一直径。第二转向部分具有第二长度和第二直径并且与第一转向部分间隔开。第一和第二转向部分在合并位置收敛。出口部分耦合到第一和第二转向部分的合并位置。至少一个流量调节装置联接到入口部分并被配置成交替地将燃料流转移到第一和第二转向部分以在合并位置产生燃料流动扰动。

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