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    • 93. 发明申请
    • Continuous Feed Chemical Vapor Deposition
    • 连续进料化学气相沉积
    • US20100120233A1
    • 2010-05-13
    • US12577641
    • 2009-10-12
    • Gang He
    • Gang He
    • H01L21/205
    • C23C16/54C23C16/45519C23C16/458C30B25/025C30B29/40C30B29/42H01L21/02463H01L21/02543H01L21/02546H01L21/0262H01L21/67109H01L21/67115H01L21/67173H01L21/6776H01L21/67784
    • Embodiments of the invention generally relate to a method for forming a multi-layered material during a continuous chemical vapor deposition (CVD) process. In one embodiment, a method for forming a multi-layered material during a continuous CVD process is provided which includes continuously advancing a plurality of wafers through a deposition system having at least four deposition zones. Multiple layers of materials are deposited on each wafer, such that one layer is deposited at each deposition zone. The methods provide advancing each wafer through each deposition zone while depositing a first layer from the first deposition zone, a second layer from the second deposition zone, a third layer from the third deposition zone, and a fourth layer from the fourth deposition zone. Embodiments described herein may be utilized to form an assortment of materials on wafers or substrates, especially for forming Group III/V materials on GaAs wafers.
    • 本发明的实施方案一般涉及在连续化学气相沉积(CVD)工艺期间形成多层材料的方法。 在一个实施例中,提供了在连续CVD工艺期间形成多层材料的方法,其包括通过具有至少四个沉积区的沉积系统连续前进多个晶片。 在每个晶片上沉积多层材料,使得在每个沉积区域沉积一层。 该方法提供每个晶片通过每个沉积区域,同时从第一沉积区沉积第一层,从第二沉积区沉积第二层,从第三沉积区沉积第三层,以及从第四沉积区沉积第四层。 本文描述的实施例可以用于在晶片或衬底上形成各种材料,特别是用于在GaAs晶片上形成III / V族材料。
    • 95. 发明授权
    • Dynamic lateral deviation display
    • 动态横向偏差显示
    • US07432828B2
    • 2008-10-07
    • US11353555
    • 2006-02-14
    • Gang HeAaron J. Gannon
    • Gang HeAaron J. Gannon
    • G08B21/00G08B23/00G01C21/00G01C23/00G05D1/00G05D3/00G06F17/00G06G7/76
    • G01C23/005
    • 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.
    • 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。
    • 96. 发明申请
    • Data flow management in generating profile models used in optical metrology
    • 生成光学计量学中使用的轮廓模型的数据流管理
    • US20080091724A1
    • 2008-04-17
    • US11580570
    • 2006-10-12
    • Hong QiuJunwei BaoWei LiuJeffrey A. ChardMiao LiuGang HeHemalatha ErvaVi Vuong
    • Hong QiuJunwei BaoWei LiuJeffrey A. ChardMiao LiuGang HeHemalatha ErvaVi Vuong
    • G06F17/00
    • G01B11/24Y10S707/953
    • To manage data flow in generating profile models for use in optical metrology, a project data object is created. A first profile model data object is created. The first profile model data object corresponds to a first profile model defined using profile parameters. A version number is associated with the first profile model data object. The first profile model data object is linked with the project data object. At least a second profile model data object is created. The second profile model data object corresponds to a second profile model defined using profile parameters. The first and second profile models are different. Another version number is associated with the second profile model data object. The second profile model data object is linked with the project data object. The project data object, the first profile model data object, and the second profile model data object are stored. The version numbers associated with the first profile model data object and the second profile model data object are stored. The link between the first profile model data object and the project data object is stored. The link between the second profile model data object and the project data object is stored.
    • 为了管理生成用于光学测量的轮廓模型中的数据流,创建了一个项目数据对象。 创建第一个配置文件模型数据对象。 第一个轮廓模型数据对象对应于使用轮廓参数定义的第一轮廓模型。 版本号与第一个轮廓模型数据对象相关联。 第一个配置文件模型数据对象与项目数据对象链接。 至少创建一个第二个轮廓模型数据对象。 第二轮廓模型数据对象对应于使用轮廓参数定义的第二轮廓模型。 第一个和第二个轮廓模型是不同的。 另一个版本号与第二个配置文件模型数据对象相关联。 第二个配置文件模型数据对象与项目数据对象链接。 存储项目数据对象,第一个轮廓模型数据对象和第二个轮廓模型数据对象。 存储与第一轮廓模型数据对象和第二轮廓模型数据对象相关联的版本号。 存储第一轮廓模型数据对象与项目数据对象之间的链接。 存储第二轮廓模型数据对象与项目数据对象之间的链接。
    • 98. 发明申请
    • Hybrid centered head-down aircraft attitude display and method for calculating displayed drift angle limit
    • 混合中心向下飞机姿态显示和计算显示漂移角限制的方法
    • US20070080828A1
    • 2007-04-12
    • US11249237
    • 2005-10-12
    • Gang He
    • Gang He
    • G01C21/00
    • G01C23/005
    • Methods and apparatus are provided for displaying terrain and attitude data symbology for an aircraft. The apparatus is a hybrid centered head-down display for an aircraft having a monitor configured to generate a display and a processor coupled to the display. The display has a centerline. The processor is configured to calculate a displayed drift angle limit, a displayed drift angle, align the centerline of the display with reference to the displayed drift angle, and generate on the display a first symbol corresponding to a terrain and a second symbol corresponding to an attitude of the aircraft. The processor is further configured to center the first symbol and the second symbol with reference to the centerline.
    • 提供了用于显示飞机的地形和姿态数据符号的方法和装置。 该装置是用于具有被配置为产生显示器的监视器和与显示器耦合的处理器的用于飞机的混合居中的下降显示器。 显示屏有一个中心线。 处理器被配置为计算显示的漂移角限制,显示的漂移角度,参考所显示的漂移角度对齐显示器的中心线,并且在显示器上生成对应于地形的第一符号和对应于 飞机的态度 处理器还被配置为参照中心线使第一符号和第二符号居中。
    • 100. 发明申请
    • System and method for facilitating target aiming and aircraft control using aircraft displays
    • 使用飞机显示屏进行目标瞄准和飞机控制的系统和方法
    • US20060227012A1
    • 2006-10-12
    • US11103878
    • 2005-04-12
    • Gang He
    • Gang He
    • G08B21/00
    • G01C23/005G02B2027/0141
    • An improved system and method are disclosed for facilitating target aiming and aircraft control by flight crews using electronic displays. For example, an aircraft display system is disclosed that includes a database for storing target location and boundary data, a processing unit, a position and direction determination unit for use in determining the position of an aiming symbol on a display, a graphics display generator, and a visual display. The processing unit determines whether or not a selected target to be displayed is obscured or covered by the aiming symbol to be displayed. If any portion of the target is obscured or covered by the aiming symbol, then the processing unit directs the graphics display generator to generate graphic control signals for the visual display, which increase the transparency of the portions of the aiming symbol that obscure or cover the target. Notably, the transparency of any symbol (or portion of a symbol) can be increased if that symbol obscures or covers a target being displayed or viewed. Thus, the visibility of targets viewed using onboard visual displays is significantly enhanced, whereby the targets are obscured by the symbols used to aim and control the aircraft. Advantageously, target aiming and aircraft control are facilitated, which reduces pilot workload and navigation errors, and thus results in increased aircraft safety.
    • 公开了一种改进的系统和方法,用于促进使用电子显示器的飞行机组的目标瞄准和飞行器控制。 例如,公开了包括用于存储目标位置和边界数据的数据库的飞行器显示系统,用于确定显示器上的瞄准符号的位置的处理单元,位置和方向确定单元,图形显示生成器, 和视觉显示。 处理单元确定要显示的所选择的目标是否被要显示的瞄准符号遮蔽或覆盖。 如果目标的任何部分被瞄准符号遮蔽或覆盖,则处理单元引导图形显示发生器产生用于视觉显示的图形控制信号,这增加了遮蔽或覆盖目标的瞄准符号的部分的透明度 目标。 值得注意的是,如果符号掩盖或覆盖正在显示或查看的目标,则可以增加任何符号(或符号的部分)的透明度。 因此,使用车载视觉显示器观看的目标的可见性显着增强,由此目标被用于瞄准和控制飞行器的符号遮蔽。 有利的是,目标瞄准和飞机控制得到了便利,这减少了飞行员的工作量和导航误差,从而导致了飞机安全性的提高。