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31. 发明申请

US20100126570A1 THIN ABSORBER LAYER OF A PHOTOVOLTAIC DEVICE 有权
标题翻译：一个光伏器件的薄膜层
公开(公告)号：US20100126570A1
公开(公告)日：2010-05-27
申请号：US12605129
申请日：2009-10-23
申请人： Isik C. Kizilyalli , Melissa Archer , Harry Atwater , Thomas J. Gmitter , Gang He , Andreas Hegedus , Gregg Higashi
发明人： Isik C. Kizilyalli , Melissa Archer , Harry Atwater , Thomas J. Gmitter , Gang He , Andreas Hegedus , Gregg Higashi
IPC分类号： H01L31/0304 , H01L31/18
CPC分类号： H01L31/0735 , Y02E10/544
摘要： Methods and apparatus are provided for converting electromagnetic radiation, such as solar energy, into electric energy with increased efficiency when compared to conventional solar cells. In one embodiment of a photovoltaic (PV) device, the PV device generally includes an n-doped layer and a p+-doped layer adjacent to the n-doped layer to form a p-n layer such that electric energy is created when electromagnetic radiation is absorbed by the p-n layer. The n-doped layer and the p+-doped layer may compose an absorber layer having a thickness less than 500 nm. Such a thin absorber layer may allow for greater efficiency and flexibility in PV devices when compared to conventional solar cells.
摘要翻译：提供了与常规太阳能电池相比，用于将诸如太阳能的电磁辐射转换成电能的方法和装置，其效率提高。在光伏（PV）器件的一个实施例中，PV器件通常包括与n掺杂层相邻的n掺杂层和p +掺杂层以形成pn层，使得当电磁辐射被吸收时产生电能由pn层。 n掺杂层和p +掺杂层可以组成厚度小于500nm的吸收层。与常规太阳能电池相比，这种薄的吸收层可以在PV器件中实现更高的效率和灵活性。

32. 发明申请

US20100070176A1 PERSPECTIVE VIEW PRIMARY FLIGHT DISPLAY SYSTEM AND METHOD WITH RANGE LINES 有权
标题翻译：主观视图主要飞行显示系统和方法与范围线
公开(公告)号：US20100070176A1
公开(公告)日：2010-03-18
申请号：US11929027
申请日：2007-10-30
申请人： Thea L. Feyereisen , Gang He , Sandy Wyatt
发明人： Thea L. Feyereisen , Gang He , Sandy Wyatt
IPC分类号： G01C21/00
CPC分类号： G08G5/0086 , G01C23/005 , G08G5/0021
摘要： A display system for a vehicle includes a navigation database storing navigation data; a terrain sensor configured to gather terrain data; a processor adapted to receive the navigation data and the terrain data and operable to supply one or more image rendering display commands based upon the navigation data and the terrain data; and a display device. The display device is coupled to receive the image rendering display commands and operable, in response thereto, to render (i) a perspective view image representative of the terrain data and the navigation data and including terrain and (ii) at least one line on the perspective view image that extends at least partially across the terrain and represents at least one of a ground-referenced range to a fixed location on the terrain and a vehicle-referenced range from the vehicle to a fixed range away from the vehicle.
摘要翻译：一种用于车辆的显示系统包括存储导航数据的导航数据; 地形传感器，用于收集地形数据; 处理器，适于接收导航数据和地形数据，并且可操作以基于导航数据和地形数据提供一个或多个图像呈现显示命令; 和显示装置。显示设备被耦合以接收图像呈现显示命令，并且响应于此可操作地渲染（i）表示地形数据和导航数据并包括地形的透视图，以及（ii）至少一条线透视图图像，其至少部分地跨过地形延伸，并且表示地面上的固定位置的地面参考范围中的至少一个以及从车辆到从车辆到固定范围的车辆参考范围。

33. 发明申请

US20100026525A1 AIRCRAFT SYNTHETIC VISION SYSTEM FOR APPROACH AND LANDING 有权
标题翻译：用于方法和陆地的飞机综合视觉系统
公开(公告)号：US20100026525A1
公开(公告)日：2010-02-04
申请号：US12183693
申请日：2008-07-31
申请人： Thea L. Feyereisen , Ivan Sandy Wyatt , Gang He
发明人： Thea L. Feyereisen , Ivan Sandy Wyatt , Gang He
IPC分类号： G01C23/00 , G08G5/00 , G06F19/00
CPC分类号： G01C23/005 , G01C5/005 , G08G5/0021 , G08G5/006 , G08G5/025
摘要： An aircraft synthetic vision system (100) is provided for increasing data input to a pilot (109) during approach and landing flight operations, and includes a runway assistance landing system (114) and a plurality of databases (106, 108, 110, 112) which may include, for example, a terrain database (106), an obstacle database (112); and a validated runway database (110). The processor (104) detects the likelihood of an error in determining the altitude from at least one of the runway assistance landing system (114), the plurality of databases (106, 108, 110, 112), and identifies the error. The processor (104) further determines augmented coordinates, and a processor (104) generates symbology commands to a first display (116) for displaying a runway environment in response to data provided to the processor (104) from each of the runway assistance landing system (114), the plurality of databases (106, 108, 110, 112), and the processor (104).
摘要翻译：提供一种飞机合成视觉系统（100），用于在接近和着陆飞行操作期间增加输入到飞行员（109）的数据，并且包括跑道辅助着陆系统（114）和多个数据库（106,108,110,112 ），其可以包括例如地形数据库（106），障碍物数据库（112）; 和经验证的跑道数据库（110）。处理器（104）检测从跑道辅助着陆系统（114），多个数据库（106,108,110,112）中的至少一个确定高度的错误的可能性，并且识别错误。处理器（104）进一步确定增强坐标，并且处理器（104）产生符号体系命令给第一显示器（116），用于响应于从跑道辅助着陆系统中的每一个提供给处理器（104）的数据来显示跑道环境（114），所述多个数据库（106,108,110,112）和所述处理器（104）。

34. 发明申请

US20100001316A1 EPITAXIAL LIFT OFF STACK HAVING A NON-UNIFORM HANDLE AND METHODS THEREOF 有权
标题翻译：具有非均匀手柄的外延提升堆栈及其方法
公开(公告)号：US20100001316A1
公开(公告)日：2010-01-07
申请号：US12475418
申请日：2009-05-29
申请人： Thomas Gmitter , Gang He , Andreas Hegedus
发明人： Thomas Gmitter , Gang He , Andreas Hegedus
IPC分类号： H01L29/20 , H01L21/20
CPC分类号： H01L21/7813 , H01L21/02543 , H01L21/02546 , H01L21/30612 , H01L21/6835 , H01L21/6836 , H01L21/7806 , H01L2221/6835 , H01L2221/68381
摘要： Embodiments of the invention generally relate to epitaxial lift off (ELO) thin films and devices and methods used to form such films and devices. In one embodiment, a method for forming a thin film material during an epitaxial lift off process is provided which includes forming an epitaxial material over a sacrificial layer on a substrate, adhering a non-uniform support handle onto the epitaxial material, and removing the sacrificial layer during an etching process. The etching process further includes peeling the epitaxial material from the substrate while forming an etch crevice therebetween and bending the support handle to form compression in the epitaxial material during the etching process. In one example, the non-uniform support handle contains a wax film having a varying thickness.
摘要翻译：本发明的实施例一般涉及外延剥离（ELO）薄膜，以及用于形成这种膜和装置的装置和方法。在一个实施例中，提供了在外延剥离工艺期间形成薄膜材料的方法，其包括在衬底上的牺牲层上形成外延材料，将不均匀的支撑手柄附着在外延材料上，以及去除牺牲在蚀刻过程中。蚀刻工艺还包括从衬底剥离外延材料，同时在其间形成蚀刻缝隙，并在蚀刻工艺期间弯曲支撑柄以在外延材料中形成压缩。在一个实例中，不均匀的支撑手柄包含具有变化厚度的蜡膜。

35. 发明申请

US20080169941A1 Aircraft glide slope display system and method 有权
标题翻译：飞机滑坡显示系统及方法
公开(公告)号：US20080169941A1
公开(公告)日：2008-07-17
申请号：US11652185
申请日：2007-01-11
申请人： Gang He
发明人： Gang He
IPC分类号： G01C21/00
CPC分类号： G01C23/00
摘要： A system and method for displaying aircraft glide slope includes determining a glide slope deviation that is representative of a difference between a desired aircraft glide slope and an actual aircraft glide slope. A glide slope icon that is representative of the desired aircraft glide slope and a glide slope deviation icon that is representative of the determined glide slope deviation are simultaneously rendered on a display.
摘要翻译：用于显示飞行器滑翔坡的系统和方法包括确定代表期望的飞行器滑翔坡与实际的飞机滑翔坡之间的差的滑翔坡偏差。代表所希望的飞行器滑翔坡的滑翔坡图标和表示确定的滑翔坡偏差的滑翔坡偏差图标同时呈现在显示器上。

36. 发明申请

US20070188350A1 Dynamic lateral deviation display 有权
标题翻译：动态横向偏差显示
公开(公告)号：US20070188350A1
公开(公告)日：2007-08-16
申请号：US11353555
申请日：2006-02-14
申请人： Gang He , Aaron Gannon
发明人： Gang He , Aaron Gannon
IPC分类号： G01C21/00 , G06F15/00 , G06F17/00
CPC分类号： G01C23/005
摘要： A method of dynamically displaying lateral deviation in formats on a display is provided. The method comprises assigning one or more positional boundaries for displaying the lateral deviation information, wherein the one or more positional boundaries define areas on a display. The method also comprises calculating display positions of a lateral deviation symbology and determining if each calculated display position is allowed based on where the lateral deviation display would be located, if displayed at each calculated position, in relation to the one or more positional boundaries. The method further comprises, displaying the lateral deviation symbology at the calculated positions when the calculated positions are allowed, and displaying a lateral deviation indicator when the calculated positions are not allowed.
摘要翻译：提供了一种在显示器上动态显示格式的横向偏差的方法。该方法包括分配用于显示横向偏差信息的一个或多个位置边界，其中所述一个或多个位置边界限定显示器上的区域。该方法还包括计算横向偏差符号系统的显示位置，并且相对于一个或多个位置边界，如果在每个计算位置显示，则基于横向偏差显示将位于哪里来确定是否允许每个计算的显示位置。该方法还包括：当允许计算的位置时，在所计算的位置处显示横向偏差符号，并且当不允许计算的位置时显示横向偏差指示符。

37. 发明申请

US20070174358A1 SYSTEMS AND METHODS FOR VERSIONING BASED TRIGGERS 有权
标题翻译：用于基于变换的触发器的系统和方法
公开(公告)号：US20070174358A1
公开(公告)日：2007-07-26
申请号：US11696166
申请日：2007-04-03
申请人： Gang He , Michael Zwilling
发明人： Gang He , Michael Zwilling
IPC分类号： G06F17/30
CPC分类号： G06F17/3051 , G06F17/30309 , Y10S707/99953 , Y10S707/99954 , Y10S707/99955
摘要： A system and/or methodology to track and organize database application data in response to a delete, insert or update procedure. More specifically, a system and/or methodology that employs a version-based retention and linkage approach with respect to triggering implementations is provided.
摘要翻译：响应于删除，插入或更新过程来跟踪和组织数据库应用程序数据的系统和/或方法。更具体地，提供了一种采用基于版本的保持和链接方法相对于触发实现的系统和/或方法。

38. 发明申请

US20050216520A1 Systems and methods for versioning based triggers 有权
标题翻译：基于版本控制的触发器的系统和方法
公开(公告)号：US20050216520A1
公开(公告)日：2005-09-29
申请号：US10889415
申请日：2004-07-12
申请人： Gang He , Michael Zwilling
发明人： Gang He , Michael Zwilling
IPC分类号： G01N33/48 , G01N33/50 , G01N33/53 , G01N33/543 , G06F17/30 , G06F19/00
CPC分类号： G06F17/3051 , G06F17/30309 , Y10S707/99953 , Y10S707/99954 , Y10S707/99955
摘要： A system and/or methodology to track and organize database application data in response to a delete, insert or update procedure. More specifically, a system and/or methodology that employs a version-based retention and linkage approach with respect to triggering implementations is provided.
摘要翻译：响应于删除，插入或更新过程来跟踪和组织数据库应用程序数据的系统和/或方法。更具体地，提供了一种采用基于版本的保持和链接方法相对于触发实现的系统和/或方法。

39. 发明申请

US20050137758A1 Graphic airways displays for flight management systems 有权
标题翻译：图形航空显示飞行管理系统
公开(公告)号：US20050137758A1
公开(公告)日：2005-06-23
申请号：US10741111
申请日：2003-12-19
申请人： Gang He , Blake Wilson , John Suddreth , Carlos Gameros , Peter Daniel
发明人： Gang He , Blake Wilson , John Suddreth , Carlos Gameros , Peter Daniel
IPC分类号： B64D43/00 , G01C23/00 , G06F3/023 , G01C21/00
CPC分类号： G01C23/005
摘要： Methods and apparatus are provided for interactively building flight paths for entry into an aircraft flight management system (FMS). The apparatus comprises a database containing map information, a display for presenting the map information, a user controlled cursor and selection buttons, all under the control of a graphics processor. The processor presents the map information with included navigation features on the display, correlated with the aircraft position and cursor location. When the cursor overlies a navigational feature (airways, waypoints, etc.), the processor highlights the feature. Feature ID information may also pop up when the feature is highlighted. Using a mouse button or equivalent, the user selects the highlighted feature or ID, whereupon the processor sends the information associated therewith to the FMS. By successively highlighting and selecting features or IDs an entire flight path can be identified and entered automatically into the FMS without the need for individual text entry.
摘要翻译：提供了用于交互地建立进入飞行器飞行管理系统（FMS）的飞行路径的方法和装置。该装置包括在图形处理器的控制下，包含地图信息的数据库，用于呈现地图信息的显示器，用户控制的光标和选择按钮。处理器在显示器上显示包含导航功能的地图信息，与飞机位置和光标位置相关。当光标覆盖导航功能（航空公司，航点等）时，处理器突出显示该功能。当功能突出显示时，功能ID信息也可能会弹出。使用鼠标按钮或等效物，用户选择突出显示的特征或ID，于是处理器将与其相关联的信息发送到FMS。通过连续突出显示和选择功能或ID，可以将整个飞行路径识别并自动进入FMS，而不需要单独的文本输入。

40. 发明授权

US6107631A Self-calibration approach for tunable laser spectral absorption sensors 失效
标题翻译：可调激光光谱吸收传感器的自校准方法
公开(公告)号：US6107631A
公开(公告)日：2000-08-22
申请号：US041896
申请日：1998-03-13
申请人： Gang He
发明人： Gang He
IPC分类号： G01N21/27 , G01N21/39 , G01N21/35
CPC分类号： G01N21/274
摘要： An on-line self-calibrating system where prior calibration information is updated by combining prior stored calibration information with current sensor reading information to simulate the introduction of a known calibrating sample and to generate new calibration information. A preferred embodiment of the present invention is in a laser spectral absorption system for determining the concentration of a particular gas in a gaseous sample by sensing a characteristic narrow spectral pulse in the absorption characteristics of the sample, the area or spectral integration of the pulse being proportional to the concentration of the particular gas. The disclosed technique effects on-line recalibration of the system based on current operating parameters of the system to compensate for time or usage induced degradation in system accuracy without introducing a sample of a known concentration of the gas into the system.
摘要翻译：在线自校准系统，其中通过将先前存储的校准信息与当前传感器读取信息组合来更新先前的校准信息，以模拟已知校准样品的引入并产生新的校准信息。本发明的一个优选实施例在激光光谱吸收系统中，用于通过感测样品的吸收特性中的特征窄光谱脉冲来确定气体样品中特定气体的浓度，脉冲的面积或光谱积分为与特定气体的浓度成比例。所公开的技术基于系统的当前操作参数来实现系统的在线重新校准，以补偿时间或使用引起的系统精度的降低，而不将已知浓度的气体的样本引入系统。

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