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1. 发明申请

WO2012084545A1 TUNABLE REFLECTOR AND LIGHTING DEVICE COMPRISING THE SAME 审中-公开
标题翻译：可逆反射器和包括其的照明装置
公开(公告)号：WO2012084545A1
公开(公告)日：2012-06-28
申请号：PCT/EP2011/072267
申请日：2011-12-09
申请人： OSRAM AG , DAI, Chenglong , HUANG, Hao , LUO, Yabin , WANG, Xuefeng
发明人： DAI, Chenglong , HUANG, Hao , LUO, Yabin , WANG, Xuefeng
IPC分类号： F21V7/16
CPC分类号： F21V7/16 , G02B5/09 , G02B5/10
摘要： The present invention relates to a tunable reflector comprising a mounting seat (1) and multiple independent flake reflecting bodies, and such flake reflecting bodies (2) are connected to the mounting seat (1) at one end, wherein the respective flake reflecting bodies (2) are joined with one another and can swing with respect to the mounting seat (1). This type of tunable reflector can freely adjust the incident angle of the light of a light source with respect to the reflecting bodies, thereby obtaining a tunable light distribution range and changeable light strength. In addition, the present invention also relates to a lighting device comprising this type of tunable reflector.
摘要翻译：本发明涉及一种包括安装座（1）和多个独立的薄片反射体的可调谐反射器，并且这样的薄片反射体（2）在一端连接到安装座（1），其中各个薄片反射体 2）彼此连接并且可相对于安装座（1）摆动。这种类型的可调谐反射器可以相对于反射体自由调节光源的入射角，从而获得可调光分布范围和可变光强度。此外，本发明还涉及包括这种类型的可调谐反射器的照明装置。

2. 发明申请

WO2012079922A2 MOUNTING MECHANISM AND LIGHTING APPARATUS HAVING THE MOUNTING MECHANISM 审中-公开
标题翻译：具有安装机构的安装机构和照明设备
公开(公告)号：WO2012079922A2
公开(公告)日：2012-06-21
申请号：PCT/EP2011/070656
申请日：2011-11-22
申请人： OSRAM AG , DAI, Chenglong , HUANG, Hao , QIN, Tengzhi , WANG, Xuefeng
发明人： DAI, Chenglong , HUANG, Hao , QIN, Tengzhi , WANG, Xuefeng
CPC分类号： F21S8/026 , F21S8/02 , F21V21/04
摘要： The present invention relates to a mounting mechanism used for a lighting apparatus, having a base (1) to be fixed on a mounting surface, wherein the base (1) is provided with at least two notches (2), each of the notches (2) is provided with a slide bar (3) connected between two opposite side surfaces of the notch (2), each slide bar (3) is sleeved with a locking member (4) capable of sliding thereon, and wherein the base (1) is provided with a first locating member (5a) and a second locating member (5b), and wherein the first locating member (5a) is used to limit the locking member (4) in a locked mounting state, and the second locating member (5b) is used to limit the locking member (4) in an inserted state. With the mounting mechanism of this type, the lighting apparatus can be simply installed into the mounting surface, and the mounting edge of the mounting surface will not be damaged when the lighting apparatus is mounted and demounted. The present invention further relates to a lighting apparatus having the mounting mechanism of the above type.
摘要翻译：本发明涉及一种用于照明设备的安装机构，该安装机构具有待固定在安装表面上的基座（1），其中基座（1）设置有至少两个凹口（（如图2所示），每个切口（2）上设置有连接在切口（2）的两个相对侧面之间的滑杆（3），每个滑杆（3）套设有可滑动的锁定件并且其中所述基座（1）设置有第一定位构件（5a）和第二定位构件（5b），并且其中所述第一定位构件（5a）用于将所述锁定构件（4）限制在锁定位置并且第二定位构件（5b）用于将锁定构件（4）限制在插入状态中。利用这种安装机构，照明装置可以简单地安装到安装表面中，并且当照明装置被安装和拆卸时安装表面的安装边缘不会被损坏。本发明还涉及具有上述类型的安装机构的照明设备。

3. 发明申请

WO2018022647A1 METHOD AND SYSTEM FOR GENERATING A SUBSURFACE MODEL 审中-公开
标题翻译：生成一个子模型的方法和系统
公开(公告)号：WO2018022647A1
公开(公告)日：2018-02-01
申请号：PCT/US2017/043775
申请日：2017-07-25
申请人： EXXONMOBIL UPSTREAM RESEARCH COMPANY , HUANG, Hao , CHANG, Dar-Lon , WU, Xiao-Hui , IMHOF, Matthias , STRIPLING, Hayes, F.
发明人： HUANG, Hao , CHANG, Dar-Lon , WU, Xiao-Hui , IMHOF, Matthias , STRIPLING, Hayes, F.
IPC分类号： G01V99/00
CPC分类号： G01V1/48 , G01V99/005 , G01V2210/66 , G06T17/05 , G06T17/20 , G06T17/205
摘要： A method and system are described for creating a subsurface model. In this method, a framework is obtained that includes various objects associated with a subsurface region. A background mesh is generated to enclose the framework and then cell splitting is performed to modify the background mesh into a watertight model. The watertight model may be assigned properties and utilized in simulations to assist in performing hydrocarbon operations.
摘要翻译：描述了用于创建地下模型的方法和系统。在该方法中，获得了包括与地下区域相关联的各种物体的框架。生成背景网格以包围框架，然后执行单元分割以将背景网格修改为水密模型。水密模型可以被分配属性并用于模拟以帮助执行碳氢化合物操作。

4. 发明申请

WO2011043862A1 DISCRETIZED PHYSICS-BASED MODELS AND SIMULATIONS OF SUBTERRANEAN REGIONS, AND METHODS FOR CREATING AND USING THE SAME 审中-公开
标题翻译：基于物理学的分层模型和模拟亚区域及其创建和使用方法
公开(公告)号：WO2011043862A1
公开(公告)日：2011-04-14
申请号：PCT/US2010/045031
申请日：2010-08-10
申请人： EXXONMOBIL UPSTREAM RESEARCH COMPANY , WALLACE, Jon, M. , HUANG, Hao , WAN, Jing
发明人： WALLACE, Jon, M. , HUANG, Hao , WAN, Jing
IPC分类号： G06G7/48
CPC分类号： E21B49/00 , E21B43/00 , G01V99/00
摘要： Methods for creating and using discretized physics-based models of subsurface regions, which may contain a hydrocarbon reservoir or other subsurface feature(s). The methods may include selecting a pre-solved model, applying a mesh to the pre-solved model, defining the shape of the subsurface region to be modeled, and transforming the pre-solved model, to which the mesh has been applied, to the shape of the subsurface region. In some methods, the pre-solved model is an idealized model. In some methods, the mesh is applied to a solution of potential field lines associated with the pre-solved model, and in some methods, the solution of potential field lines is a composite solution of a plurality of solutions of potential field lines. In some methods, one or more supershapes are used to define the shape of the subsurface region. In some methods, a hyperelastic strain deformation calculation is utilized for the transforming.
摘要翻译：用于创建和使用可能包含烃储层或其他地下特征的地下区域的基于离散物理的模型的方法。所述方法可以包括选择预先解决的模型，将网格应用于预先确定的模型，定义待建模的地下区域的形状，以及将已应用网格的预先解决的模型转换为地下区域的形状。在一些方法中，预先解决的模型是一个理想化的模型。在一些方法中，将网格应用于与预定模型相关联的潜在场线的解，并且在一些方法中，势场线的解是多个势场解的解的复合解。在一些方法中，使用一个或多个超级形状来限定地下区域的形状。在一些方法中，使用超弹性应变变形计算进行变换。

5. 发明申请

WO2007111970A2 AIRCRAFT ENGINE STARTER/GENERATOR AND CONTROLLER 审中-公开
标题翻译：飞机发动机起动器/发电机和控制器
公开(公告)号：WO2007111970A2
公开(公告)日：2007-10-04
申请号：PCT/US2007/007192
申请日：2007-03-23
申请人： SMITHS AEROSPACE LLC , HUANG, Hao , KARIPIDES, David , ABBAS, Mohamed , TSUI, David
发明人： HUANG, Hao , KARIPIDES, David , ABBAS, Mohamed , TSUI, David
IPC分类号： F02N11/04 , H02P9/00
CPC分类号： F02N11/04 , H02P9/302 , H02P2101/30
摘要： An aircraft starting and generating system includes a starter/generator that includes a main machine, an exciter, and a permanent magnet generator. The system also includes an inverter/converter/controller that is connected to the starter/generator and that generates AC power to drive the starter/generator in a start mode for starting a prime mover of the aircraft, and that converts AC power, obtained from the starter/generator after the prime mover have been started, to DC power in a generate mode of the starter/generator. The exciter includes a stator and a rotor, and wherein the exciter rotor includes a three-phase AC winding.
摘要翻译：飞机启动和发电系统包括起动器/发电机，其包括主机，励磁机和永磁发电机。该系统还包括连接到起动器/发电机的逆变器/转换器/控制器，并且产生AC电力以起动模式启动起动器/发电机，以启动飞机的原动机，并且将AC电力起动器/发电机起动器/发电机的发电模式启动后，起动器/发电机起动，直流电。励磁机包括定子和转子，其中励磁机转子包括一个三相交流绕组。

6. 发明申请

WO2010077766A2 METHOD AND SYSTEMS FOR AN ENGINE STARTER/GENERATOR 审中-公开
标题翻译：发动机起动器/发电机的方法和系统
公开(公告)号：WO2010077766A2
公开(公告)日：2010-07-08
申请号：PCT/US2009/067497
申请日：2009-12-10
申请人： GENERAL ELECTRIC COMPANY , XU, Longya , KARIPIDES, David, Kimitri , ABBAS, Mohamed , HUANG, Hao
发明人： XU, Longya , KARIPIDES, David, Kimitri , ABBAS, Mohamed , HUANG, Hao
IPC分类号： F02N15/08 , F02N11/08 , F02N15/04 , F02N15/00 , F02C7/26 , H02P21/00 , H02P21/14
CPC分类号： F02N15/00 , F01D15/10 , F02C7/268 , F02N11/04 , F02N11/0859 , F02N2011/0888 , F02N2011/0896 , F02N2250/08 , H02P21/24 , Y02T50/671
摘要： A method and system for an engine starter/generator is provided The starter/generator system includes a three phase squirrel cage induction machine, a three phase inverter/converter electrically coupled Io the three phase squirrel cage induction machine The starter/generator system also includes a bidirectional DC-DC converter electrically coupled to the three phase inverter/converter, and a digital control board configured to sensorlessly determine a rotor angle from a plurality of phase currents to the induction machine during a start mode. During the start mode, logic in the digital control board configures the starter: generator system into a combination of an induction motor, a three phase DC-AC inverter, and a DC -DC boost converter, and during a generate mode, the logic in the digital control board configures the starter generator system into a combination of an induction generator, a three phase AC-DC converter, and a DC-DC buck converter.
摘要翻译：提供一种用于发动机起动器/发电机的方法和系统。起动器/发电机系统包括三相鼠笼式感应电动机，三相逆变器/转换器，电耦合到三相鼠笼式感应电机。起动器/发电机系统还包括一个电耦合到三相逆变器/转换器的双向DC-DC转换器和被配置为在启动模式期间无级地确定从多个相电流到感应电机的转子角度的数字控制板。在启动模式下，数字控制板中的逻辑将起动器：发电机系统配置为感应电动机，三相DC-AC逆变器和DC-DC升压转换器的组合，在生成模式期间，逻辑数字控制板将起动发电机系统配置为感应发电机，三相AC-DC转换器和DC-DC降压转换器的组合。

7. 发明申请

WO2010068426A1 ELECTRIC ENERGY STORAGE INTEGRATED WITHIN OR PROXIMATE TO ELECTRICALLY DRIVEN FLIGHT CONTROL ACTUATORS 审中-公开
标题翻译：集成在或靠近电动驾驶飞行控制执行器的电力存储
公开(公告)号：WO2010068426A1
公开(公告)日：2010-06-17
申请号：PCT/US2009/065679
申请日：2009-11-24
申请人： GE AVIATION SYSTEMS LLC , HUANG, Hao , KARIPIDES, David, Dimitri , RADUN, Arthur, Vorwerk
发明人： HUANG, Hao , KARIPIDES, David, Dimitri , RADUN, Arthur, Vorwerk
IPC分类号： H02P27/08 , B64C13/50 , H02M3/158
CPC分类号： H02P27/08 , H02M3/1582 , Y10T29/49002
摘要： An apparatus for use with a flight control actuator and method for assembling the same is provided. The apparatus includes a motor drive system (100) and a control unit. The motor drive system (100) includes a capacitor-based energy storage (120) configured to store and provide energy within or proximate to the actuator. The control unit is coupled to the motor drive system and is configured to facilitate managing power within or proximate to the actuator.
摘要翻译：提供了一种用于飞行控制致动器的装置及其组装方法。该装置包括电机驱动系统（100）和控制单元。马达驱动系统（100）包括基于电容器的能量存储器（120），其被配置为在致动器内或附近存储和提供能量。控制单元耦合到马达驱动系统并且被配置为便于在致动器内部或附近管理动力。

8. 发明申请

WO2012114208A1 WEARABLE ARTICLES WITH WETNESS SENSING 审中-公开
标题翻译：耐磨感的文具
公开(公告)号：WO2012114208A1
公开(公告)日：2012-08-30
申请号：PCT/IB2012/050271
申请日：2012-01-20
申请人： CKICOM TECHNOLOGY LIMITED , WONG, Sun Hoi , XU, Fei , HUANG, Hao
发明人： WONG, Sun Hoi , XU, Fei , HUANG, Hao
IPC分类号： A61F5/48 , A61F13/15 , G01N27/22 , G01N27/02
CPC分类号： G01N27/223 , A61F13/42 , A61F2013/424
摘要： A wearable article for wearing by a user and comprising wetness sensing electrodes, wherein the wetness sensing electrodes are to be in contact with a wetting electrolytic liquid during normal use when the wearable article is wetted by the electrolytic liquid, and to operate as a capacitor upon application of a direct current at contact terminals of the wetness sensing electrodes when so wetted to facilitate capacitance measurement through the wetness sensing electrodes whereby wetness information of the wearable article is provided.
摘要翻译：一种穿戴用品，用于使用者佩戴并且包括湿度感测电极，其中当穿用物品被电解液润湿时，湿度感测电极在正常使用期间与润湿电解液接触，并且作为电容器操作当湿润感应电极的接触端子处施加直流电以便通过湿度感测电极进行电容测量，从而提供可穿戴制品的湿度信息。

9. 发明申请

WO2009139949A1 MODELING OF HYDROCARBON RESERVOIRS USING DESIGN OF EXPERIMENTS METHODS 审中-公开
标题翻译：使用实验设计方法建立油气储层
公开(公告)号：WO2009139949A1
公开(公告)日：2009-11-19
申请号：PCT/US2009/035855
申请日：2009-03-03
申请人： EXXONMOBIL UPSTREAM RESEARCH COMPANY , HUANG, Hao , HSU, Sheng-Yuan , BURDETTE, Jason, A. , ASMANN, Marcus
发明人： HUANG, Hao , HSU, Sheng-Yuan , BURDETTE, Jason, A. , ASMANN, Marcus
IPC分类号： G06F7/60
CPC分类号： E21B43/00
摘要： Methods for generating a surrogate model for subsurface analysis may include identifying input parameters for the subsurface analysis, and selecting a range of values for the identified parameters. The methods also include selecting a design of experiments method for filling sampling points within the ranges of values for the identified input parameters. The design of experiments method may be a classical method or a space-filling technique. The methods also include filling sampling points within the ranges of values for the identified input parameters. The sampling points are filled based on the design of experiments method selected. The methods further include acquiring output values for each of the selected sampling points, and constructing a surrogate model based upon the output values for at least some of the selected sampling points. The surrogate model is a mathematical equation that represents a simplified model for predicting solutions to complex reservoir engineering problems.
摘要翻译：用于生成用于地下分析的替代模型的方法可以包括识别用于地下分析的输入参数，以及为所识别的参数选择值的范围。所述方法还包括选择用于在所识别的输入参数的值的范围内填充采样点的实验方法的设计。实验方法的设计可以是经典的方法或空间填充技术。这些方法还包括在所识别的输入参数的值的范围内填充采样点。基于所选实验方法的设计填充采样点。所述方法还包括获取每个所选择的采样点的输出值，以及基于所选择的采样点中的至少一些的输出值构建代理模型。代理模型是一个数学方程，代表了一个简化的模型，用于预测复杂油藏工程问题的解决方案。

10. 发明申请

WO2007146246A2 DUAL-STRUCTURED AIRCRAFT ENGINE STARTER/GENERATOR 审中-公开
标题翻译：双结构飞机发动机起动器/发电机
公开(公告)号：WO2007146246A2
公开(公告)日：2007-12-21
申请号：PCT/US2007/013718
申请日：2007-06-12
申请人： SMITHS AEROSPACE LLC , PADGETT, Gary, A. , ZYWOT, Jan , WIRSCH, Paul , ABBAS, Mohamed , TANEJA, Dinesh, N. , HUANG, Hao
发明人： PADGETT, Gary, A. , ZYWOT, Jan , WIRSCH, Paul , ABBAS, Mohamed , TANEJA, Dinesh, N. , HUANG, Hao
CPC分类号： F02N11/04 , F01D15/10 , F02C7/268 , F05D2260/85 , H02K1/02 , H02K1/24 , H02K1/32 , H02K1/325 , H02K3/527 , H02K9/02 , H02K9/19 , H02K19/38 , Y02T50/671
摘要： An aircraft starting and generating system includes a first starter/main machine assembly that includes a first exciter and a first main machine, and second starter/main machine assembly that includes a second exciter and a second main machine. The system also includes a permanent magnet generator (PMG) that is connected to the first and second starter/main machine assemblies. The system further includes a first inverter/converter/controller (ICC) that is connected to the first starter/main machine assembly and to the PMG, and a second ICC that is connected to the second starter/main machine assembly and to the PMG. The first and second ICCs generate AC power to respective drive the first and second starter/main machine assemblies in a start mode of the starting and generating system for starting a prime mover of the aircraft, and the first and second ICCs convert AC power, respectively obtained from the PMG after the prime mover has been started, to DC power in a generate mode of the starting and generating system.
摘要翻译：飞机起动和发电系统包括包括第一激励器和第一主机的第一启动器/主机组件，以及包括第二激励器和第二主机的第二起动器/主机组件。该系统还包括连接到第一和第二起动器/主机组件的永磁发电机（PMG）。该系统还包括连接到第一启动器/主机组件和PMG的第一逆变器/转换器/控制器（ICC），以及连接到第二起动器/主机组件和PMG的第二ICC。第一和第二ICC产生AC电力以分别驱动第一和第二启动器/主机组件，起动和发电系统的启动模式用于启动飞行器的原动机，并且第一和第二ICC分别转换AC电力原动机启动后从PMG获得的直流电源以起动和发电系统的生成模式。

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