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1. 发明授权

US07679528B1 Modulation of aircraft guidance lights 有权
标题翻译：飞机导向灯调制
公开(公告)号：US07679528B1
公开(公告)日：2010-03-16
申请号：US11494939
申请日：2006-07-28
申请人： Timothy J. Etherington , Arlen E. Breiholz
发明人： Timothy J. Etherington , Arlen E. Breiholz
IPC分类号： G08B21/00
CPC分类号： G08G5/0021 , B64F1/20 , G01S1/70 , G08G5/025
摘要： An aircraft landing and/or taxiing system has a plurality of landing zone, runway, and/or taxiway lights capable of receiving information signals and transmitting optically signals representative of the information signals. A processing system for providing the information signals to the plurality of lights is also used. The system also comprises a sensor tuned to receive light of a specific range of wavelengths, the light being emitted from the lights. Also, a processing system coupled to the sensor and configured with software to interpret signals received by the sensor is used. Program code runs on the processing system. The program code is configured to determine the location of an aircraft on the taxiway based on the light signal received from one or more of the taxiway lights. Also, the aircraft landing and/or taxiing system utilizes modulated lights to provide information pertinent to aircraft landing and/or taxiing operations.
摘要翻译：飞机着陆和/或滑行系统具有能够接收信息信号并发送表示信息信号的光信号的多个着陆区，跑道和/或滑行道灯。还使用用于向多个灯提供信息信号的处理系统。该系统还包括被调谐以接收特定波长范围的光的传感器，光从灯发射。此外，使用耦合到传感器并配置有用于解释由传感器接收的信号的软件的处理系统。程序代码在处理系统上运行。程序代码被配置为基于从一个或多个滑行道灯接收到的光信号来确定飞行器在滑行道上的位置。此外，飞机着陆和/或滑行系统利用调制光提供与飞机着陆和/或滑行操作有关的信息。

2. 外观设计

USD746747S1 Flight control panel 有权
标题翻译：飞行控制面板
公开(公告)号：USD746747S1
公开(公告)日：2016-01-05
申请号：US29468159
申请日：2013-09-26
申请人： Geoffrey A. Shapiro , Timothy J. Etherington , Laura Maxine Smith-Velazquez
设计人： Geoffrey A. Shapiro , Timothy J. Etherington , Laura Maxine Smith-Velazquez
CPC分类号： G08G5/0039 , G06F3/013 , G06F3/017 , G06F3/04883 , G08G5/0021 , G08G5/006 , G08G5/0086 , G08G5/0091
摘要： A method. The method includes receiving user input data from a user interface system. The user input data includes user gesture data, wherein the user gesture data is associated with one or more detected user gestures. The method also includes manipulating one or more graphical flight path elements based at least upon received user gesture data. The method further includes performing at least one flight path modification operation based at least upon one or more factors and the received user gesture data. The method additionally includes outputting updated graphical data to the user interface system, wherein the updated graphical data includes updated graphical flight path element data and updated graphical flight path data.

3. 发明授权

US09132913B1 Simplified auto-flight system coupled with a touchscreen flight control panel 有权
标题翻译：简化的自动飞行系统以及触摸屏飞行控制面板
公开(公告)号：US09132913B1
公开(公告)日：2015-09-15
申请号：US14038439
申请日：2013-09-26
申请人： Geoffrey A. Shapiro , Timothy J. Etherington , Laura Maxine Smith-Velazquez
发明人： Geoffrey A. Shapiro , Timothy J. Etherington , Laura Maxine Smith-Velazquez
IPC分类号： G05D1/00 , G09G5/00 , B64C19/00
CPC分类号： B64C13/18 , B64C19/00 , B64D43/02 , G01C23/005 , G05D1/101 , G06F3/0412 , G06F3/0416 , G06F3/04883 , G06F2203/04808 , G08G5/0021 , G08G5/0034 , G08G5/0052 , G08G5/006 , G08G5/0086
摘要： A system includes an auto-flight system and a touchscreen flight mode control panel. The auto-flight system is configured to control a plurality of primary flight modes. The touchscreen flight mode control panel is communicatively coupled to the auto-flight system. The touchscreen flight mode control panel is configured to receive primary flight mode data from the auto-flight system. The touchscreen flight mode control panel is also configured to graphically present each primary flight mode of the plurality of primary flight modes to a user. The touchscreen flight mode control panel is further configured to detect touch gestures and direct executions of the user. The touchscreen flight mode control panel is additionally configured to output touch gesture data and direct execution data to the auto-flight system.
摘要翻译：系统包括自动飞行系统和触摸屏飞行模式控制面板。自动飞行系统被配置为控制多个主飞行模式。触摸屏飞行模式控制面板通信耦合到自动飞行系统。触摸屏飞行模式控制面板配置为从自动飞行系统接收主飞行模式数据。触摸屏飞行模式控制面板还被配置为向用户图形地呈现多个主飞行模式的每个主飞行模式。触摸屏飞行模式控制面板还被配置为检测用户的触摸手势和直接执行。触摸屏飞行模式控制面板另外被配置为输出触摸手势数据并将自动飞行系统的执行数据直接输出。

4. 发明授权

US08615337B1 System supporting flight operations under instrument meteorological conditions using precision course guidance 有权
标题翻译：系统使用精准课程指导，在仪表气象条件下支持飞行运行
公开(公告)号：US08615337B1
公开(公告)日：2013-12-24
申请号：US12284787
申请日：2008-09-25
申请人： Patrick D. McCusker , Sarah Barber , Felix B. Turcios , Douglas A. Bell , Richard D. Jinkins , Timothy J. Etherington , Michael J. Krenz , Charles B. Dirks
发明人： Patrick D. McCusker , Sarah Barber , Felix B. Turcios , Douglas A. Bell , Richard D. Jinkins , Timothy J. Etherington , Michael J. Krenz , Charles B. Dirks
IPC分类号： G06F7/70 , G06F19/00 , G06G7/00 , G06G7/76
CPC分类号： G01C21/20
摘要： The present examples provide circuits, systems, processes, and the like for providing precision course guidance, typically for improved positive course guidance below published minimum descent altitude or decision altitude, including just in time calculations of obstacle free flight paths. The calculated flight path may be presented in the context of a synthetic scene of the environment surrounding the aircraft. To provide precision course guidance, exemplary avionics systems, processes and the like, as described below may be utilized.
摘要翻译：本示例提供电路，系统，过程等，用于提供精确的课程指导，通常用于在公开的最低下降高度或决策高度以下的改进的积极课程指导，包括刚刚在无障碍飞行路径的时间计算中。计算的飞行路线可以在飞机周围的环境的合成场景的背景下呈现。为了提供精确的课程指导，可以使用如下所述的示例性航空电子系统，过程等。

5. 发明授权

US07098913B1 Method and system for providing depth cues by attenuating distant displayed terrain 有权
标题翻译：通过衰减遥远的显示地形来提供深度线索的方法和系统
公开(公告)号：US07098913B1
公开(公告)日：2006-08-29
申请号：US10208567
申请日：2002-07-30
申请人： Timothy J. Etherington , Alex Postnikov , Thomas L. Vogl
发明人： Timothy J. Etherington , Alex Postnikov , Thomas L. Vogl
IPC分类号： G06T15/50 , G09G5/00 , G09G5/02
CPC分类号： G06T15/10 , G06T15/50 , G08G5/045
摘要： A method of increasing situational awareness of terrain is disclosed. A representation of a terrain feature is generated from a source of stored data. A distance from a reference point to the terrain feature is determined. The representation of the terrain feature is attenuated if the distance from the reference point to the terrain feature is within a predetermined range. The representation of the terrain feature is displayed.
摘要翻译：披露了增加地形情境意识的方法。从存储数据源生成地形特征的表示。确定从参考点到地形特征的距离。如果从参考点到地形特征的距离在预定范围内，则地形特征的表示将被衰减。显示地形特征的表示。

6. 发明授权

US07026956B1 Method of integrating speed deviation cues in a vehicle navigation display 有权
标题翻译：在车辆导航显示器中集成速度偏差提示的方法
公开(公告)号：US07026956B1
公开(公告)日：2006-04-11
申请号：US10692260
申请日：2003-10-23
申请人： Jason C. Wenger , Alexei Postnikov , Eric N. Anderson , Timothy J. Etherington
发明人： Jason C. Wenger , Alexei Postnikov , Eric N. Anderson , Timothy J. Etherington
IPC分类号： G01C23/00
CPC分类号： G01C23/00
摘要： A display system for a vehicle is provided. The display system includes a display configured to render a representation of an intended vehicle path. At least one relative speed indicator is rendered upon the display. The at least one relative speed indicator is configured to move along the representation of the intended vehicle path, in an area of the display that is peripheral to a focus area of the display, in response to a difference between an actual value of a speed-based parameter and a preferred value of a speed-based parameter of the vehicle.
摘要翻译：提供了一种用于车辆的显示系统。显示系统包括被配置为呈现预期车辆路径的表示的显示器。在显示器上呈现至少一个相对速度指示器。所述至少一个相对速度指示器被配置为响应于速度 - 速度指示器的实际值之间的差异，沿着所述显示器的对应于所述显示器的对焦区域周边的区域中的所述目标车辆路径的表示，并且车辆的基于速度的参数的优选值。

7. 发明授权

US06686851B1 Altitude tape and integral vertical speed indicator 失效
标题翻译：高度磁带和积分垂直速度指示器
公开(公告)号：US06686851B1
公开(公告)日：2004-02-03
申请号：US09648829
申请日：2000-08-25
申请人： Thomas M. Gordon , Timothy J. Etherington
发明人： Thomas M. Gordon , Timothy J. Etherington
IPC分类号： G08B2300
CPC分类号： G01C23/005
摘要： A device for enhancing altitude awareness in an avionics display is disclosed. The device includes an altitude indicator that displays a current altitude on the avionics display. A scrolling display of altitude levels is displayed with the altitude indicator on the avionics display. The scrolling display includes a plurality of scaled numbers that represent predetermined intervals of altitude levels surrounding the current altitude. The scrolling display also includes a non-numeric graphic construct that is displayed adjacent the plurality of scaled numbers. The graphic construct has first and second substantially mirror-image portions that are positioned on first and second opposing sides of the plurality of scaled numbers. A controller causes the altitude indicator to display the current altitude on the avionics display. The controller also causes the scrolling display to display the predetermined intervals of altitude levels surrounding the current altitude and to vary the graphic construct consistent with the predetermined altitude levels that are displayed. A vertical speed indicator may be superimposed upon the scrolling display.
摘要翻译：公开了一种用于在航空电子显示器中提高高度感知的装置。该设备包括一个高度指示器，显示航空电子显示屏上的当前高度。显示海拔高度的滚动显示，航空电子显示屏上显示高度指示。滚动显示器包括多个缩放的数字，其表示围绕当前高度的高度级的预定间隔。滚动显示器还包括与多个缩放数字相邻地显示的非数字图形构造。图形构造具有位于多个缩放数字的第一和第二相对侧上的第一和第二基本上镜像部分。控制器使高度指示器显示航空电子显示屏上的当前高度。控制器还使得滚动显示器显示围绕当前高度的高度水平的预定间隔并且改变与所显示的预定高度水平一致的图形构造。垂直速度指示器可以叠加在滚动显示器上。

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