序号 专利名 申请号 申请日 公开(公告)号 公开(公告)日 发明人
1 增强型近地警告系统的功能及故障的自动测试系统 CN201721190066.7 2017-09-18 CN207232754U 2018-04-13 周卫稳; 杨保田
本实用新型涉及增强型近地警告系统的功能及故障的自动化测试系统,其包括嵌入式控制器、开关资源、多种测试设备以及测试接口适配器。嵌入式控制器运行有自动化测试软件平台与相应的测试脚本程序,控制待测的增强型近地警告系统、测试设备和测试接口适配器按照参数测试的流程完成功能和故障测试。测试设备包括函数信号发生器、数字万用表、可编程电源、示波器和计数器。开关资源将测试设备通过测试接口适配器连接到待测的增强型近地警告系统的测量点。测试接口适配器由自动化测试所需的电子元件及连接线组成,用于待测的增强型近地警告系统与测试设备之间的连接。本实用新型能够实现增强型近地警告系统的全自动化功能以及故障的测试。
2 SYSTEM AND METHOD FOR GROUND PROXIMITY WARNING WITH ENHANCED OBSTACLE DEPICTION PCT/US2006/014453 2006-04-17 WO2006115884A1 2006-11-02 KHATWA, Ratan

Systems and methods for displaying ground obstructions on a visual display are disclosed. In an embodiment, a ground proximity warning system includes at least one aircraft sensor system operable to acquire aircraft data and a ground proximity warning computer coupled to the aircraft sensor system to process the aircraft data that generates ground proximity warning data corresponding to a sensed ground obstruction. An indicating system including a visual display device then presents an image of a visual symbol corresponding to the sensed ground obstruction. At least one of the computer and the visual display device is controllable to selectively display the visual symbol.

3 Systems and methods for reducing nuisance alerts for helicopter enhanced ground proximity warning systems EP07110841.9 2007-06-22 EP1870676A2 2007-12-26 ISHIHARA, Yasuo; BATEMAN, Charles, Donald.

Systems and methods for controlling activation of a look-ahead function of a terrain alert and warning system. The system receives rate of climb and aircraft speed information, compares the rate of climb and aircraft speed information to a predefined threshold, and deactivates a look-ahead function based on the comparison.

4 Systems and methods for reducing nuisance alerts for helicopter enhanced ground proximity warning systems EP07110841.9 2007-06-22 EP1870676B1 2011-07-20 Ishihara, Yasuo; Bateman, Charles, Donald.
5 System for real-time logging of aircraft sensor data received from an Enhanced Ground Proximity Warning System EP11176489.0 2011-08-03 EP2418625A1 2012-02-15 Conner, Kevin J.; Ostrom, Gary A.; Bateman, C. Don

Systems and methods for performing efficient, inexpensive data logging of aircraft sensor data. An example system (20) on board an aircraft (18) includes a plurality of data sources (34) that provide sensor data associated with a plurality of avionic components, a line replaceable processing unit (24) that is in signal communication with the plurality of data sources via one or more databuses (32), a wireless router (26) connected to the line replaceable processing unit via a data cable and a portable data unit (28) in wireless data communication with the wireless router. The wireless router receives at least a portion of the sensor data from the line replaceable processing unit and sends the received sensor data to the portable data unit.

6 Pitch alerting angle for enhanced ground proximity warning system (EGPWS) US10114883 2002-04-01 US06940427B2 2005-09-06 Peter J. Bateman
A ground proximity warning system including a pitch angle alerting device, the pitch angle alerting device including warning logic having an input that is structured to receive a signal that is representative of the indicated pitch angle of the aircraft, the warning logic being structured to determine a difference between a pitch angle signal received on the input and a predetermined threshold, the warning logic being structured also to output a signal representative of the difference between the two signals; and an advisory indication generator coupled to accept the output of the warning logic, the advisory indication generator being structured to generate an advisory indication signal as a function of the difference between the two signals.
7 SYSTEM AND METHOD FOR GROUND PROXIMITY WARNING WITH ENHANCED OBSTACLE DEPICTION US10907934 2005-04-21 US20060238402A1 2006-10-26 Ratan Khatwa
Systems and methods for displaying ground obstructions on a visual display are disclosed. In an embodiment, a ground proximity warning system includes at least one aircraft sensor system operable to acquire aircraft data and a ground proximity warning computer coupled to the aircraft sensor system to process the aircraft data that generates ground proximity warning data corresponding to a sensed ground obstruction. An indicating system including a visual display device then presents an image of a visual symbol corresponding to the sensed ground obstruction. At least one of the computer and the visual display device is controllable to selectively display the visual symbol.
8 Pitch alerting angle for enhanced ground proximity warning system (EGPWS) US10114883 2002-04-01 US20030016145A1 2003-01-23 Peter J. Bateman
A ground proximity warning system including a pitch angle alerting device, the pitch angle alerting device including warning logic having an input that is structured to receive a signal that is representative of the indicated pitch angle of the aircraft, the warning logic being structured to determine a difference between a pitch angle signal received on the input and a predetermined threshold, the warning logic being structured also to output a signal representative of the difference between the two signals; and an advisory indication generator coupled to accept the output of the warning logic, the advisory indication generator being structured to generate an advisory indication signal as a function of the difference between the two signals.
9 基于性能的导航飞行程序计算机虚拟环境仿真校验系统 CN201510523982.7 2015-08-25 CN105243173A 2016-01-13 麻士东; 杨国庆
本发明提供了一种基于性能的导航(PBN)飞行程序计算机虚拟环境仿真校验系统,属于民用航空导航领域。该系统包括数据层、模型层、显示层和应用层;数据层用于对飞行程序数据、地形数据和障碍物数据进行处理;模型层为飞行程序的虚拟验证提供飞机的导航系统、动力学系统以及增强型近地警告系统;显示层用于虚拟验证时,为用户提供二维显示以及三维视景系统;应用层为用户提供人机交互以及飞行程序验证的应用。该系统实现了在计算机产生的虚拟环境中对PBN飞行程序进行验证,简单方便、缩短了验证周期,降低了成本,提高了工作效率,其结果能够对飞行程序设计进行评估,对实际飞行验证进行指导,满足PBN飞行程序验证的需求。
10 DIGITAL AUDIO WARNING SYSTEM US13151744 2011-06-02 US20120306667A1 2012-12-06 JONATHAN ERLIN MORITZ; John Alton Moritz
A digital audio warning system (DAWS) that can monitor all relative aircraft systems and provide audio for any warning that requires immediate action. Current aircraft systems only monitor their individual system. The DAWS can monitor all relative aircraft systems. The DAWS may not replace the conventional warning signals, but can be a second level of warning to the flight crew. These warnings are relative to “red flag” type warnings and are not meant to replace warnings such as traffic collision avoidance system (TCAS) or enhanced ground proximity warning system (EGPWS) warnings.
11 Systems and methods for broadcasting an unknown airport advisory EP07115226.8 2007-08-29 EP1926003A2 2008-05-28 Conner, Kevin J.; Ishihara, Yasuo

Systems and methods for advising a flight crew member that an enhanced ground proximity warning system (EGPWS), for example, may continue to provide terrain alerts, cautions, warnings, or the like because an intended landing site for the aircraft is not recognized within a database of airports. An unknown airport advisory is generated and broadcast after the aircraft is in a landing configuration, when the aircraft is greater than a threshold distance from the nearest landing site in the database, but before the terrain alerts are broadcast. The pilot may actuate a "terrain inhibit" selection device after receiving the advisory. The inhibit device may deactivate or mute subsequent alerts generated by the EGPWS during that particular landing sequence.

12 METHODS AND SYSTEMS FOR MONITORING AIRCRAFT APPROACH BETWEEN APPROACH GATES US11470188 2006-09-05 US20070120708A1 2007-05-31 Yasuo Ishihara; Steve Johnson; Kevin Conner
Using signals available into an Enhanced Ground Proximity Warning System (EGPWS), approach monitor systems and methods compare approach speed, approach angle and amount of tailwind/crosswind to the pre-selected envelopes. When the aircraft approach speed, approach angle, or tailwind/crosswind is greater than the pre-defined envelope, the approach monitor system generates an aural/visual advisory indicating the violation. The envelope is set as a function of “height above runway elevation”.
13 Systems and methods for automatic detection of QFE operations US11625714 2007-01-22 US07389164B1 2008-06-17 Kevin J Conner; Steve C. Johnson; Yasuo Ishihara
Systems and methods for determining if an aircraft is approaching a atmospheric pressure at field elevation (QFE) airport and for alerting if any errors that might affect the production of an accurate altitude value. In an example method a global positioning system (GPS) altitude value is compared to a corrected barometric altitude, if an airport that the aircraft is proximate to (approaching) is a QFE airport. The field elevation of the proximate airport is added to the corrected barometric altitude to generate an adjusted barometric altitude, if the comparison between the GPS altitude and the corrected barometric altitude is greater than a predefined threshold. The adjusted barometric altitude is sent to relevant aircraft systems, such as an Enhanced Ground Proximity Warning System.
14 Vehicle positioning and data integrating method and system thereof US09374480 1999-08-13 US06205400B1 2001-03-20 Ching-Fang Lin
A vehicle positioning and data integrating process and system can substantially solve the problems encountered in avionics system integration, which employs integrated global positioning system/inertial measurement unit enhanced with altitude measurements to derive vehicle position, velocity, attitude, and body acceleration and rotation information. A vehicle positioning and data integrating system comprises navigation sensors and an IMU interface and preprocessing board, an altitude interface and processing board, a navigation processing board, a shared memory card, a bus arbiter, a control board, and a bus interface. The control board distributes navigation data to flight management system, flight control system, automatic dependent aurveillance, cockpit display, enhanced ground proximity warning system, weather radar, and satellite communication system.
15 SURGICAL LOCATION MONITORING SYSTEM AND METHOD US13822358 2012-10-21 US20140228675A1 2014-08-14 Ehud (Udi) Daon
A surgical hardware and software monitoring system and method allows for surgical planning while the patient is available for surgery, for example while the patient is being prepared for surgery so that the system may model the surgical site. Tracker obtains image information, with controller configured to spatially relate image information with previously obtained scan data. Fiducial reference is configured for removably attaching to a location proximate a surgical site. The fiducial reference is observable by the tracker so that software of the controller determines three-dimensional location and orientation based on scan data and image data of the surgical site, spatially relating the image information to the scan data to determine the three-dimensional location and the orientation of the fiducial reference. In one embodiment, the model may be used to track contemplated surgical procedures and warn the physician regarding possible boundary violations that would indicate an inappropriate location in a surgical procedure. In another embodiment, the monitoring system may track the movement of instruments during the procedure and in reference to the model to enhance observation of the procedure. In a further embodiment the monitoring system can be used to model and track the changes in the surgical site itself.
16 基于增强现实和云端智能决策的车联网事故黑点警告系统及方法 CN201710022303.7 2017-01-12 CN106846863A 2017-06-13 叶昊
本发明公开了一种基于增强现实和云端智能决策的车联网事故黑点警告系统及方法,其车载客户端系统层实现行车数据的采集,并通过蜂窝通信网络层将采集到的行车数据发送到云端控制中心层;并接收从云端控制中心层发回的数据决策包,以增强现实的方式结合实景路况显示给驾驶员;云端控制中心层依据实时接收的行车数据和黑点数据库中数据,针对车辆行车状态和当时的交通和天气情况做出决策分析,并将相应警告信息以数据包格式发布到车载客户端系统层。本发明通过融合各类动态交通数据源,结合云端智能决策和增强现实,可以大大提高司机在道路黑点对各类事故风险的觉察力,增强驾驶员在不可见的道路黑点的安全意识,从而降低事故率,改善道路黑点安全。
17 基于增强现实和云端智能决策的事故黑点警告系统及方法 CN201710022303.7 2017-01-12 CN106846863B 2020-05-05 叶昊
本发明公开了一种基于增强现实和云端智能决策的车联网事故黑点警告系统及方法,其车载客户端系统层实现行车数据的采集,并通过蜂窝通信网络层将采集到的行车数据发送到云端控制中心层;并接收从云端控制中心层发回的数据决策包,以增强现实的方式结合实景路况显示给驾驶员;云端控制中心层依据实时接收的行车数据和黑点数据库中数据,针对车辆行车状态和当时的交通和天气情况做出决策分析,并将相应警告信息以数据包格式发布到车载客户端系统层。本发明通过融合各类动态交通数据源,结合云端智能决策和增强现实,可以大大提高司机在道路黑点对各类事故风险的觉察力,增强驾驶员在不可见的道路黑点的安全意识,从而降低事故率,改善道路黑点安全。
18 控制检查点进入车辆的安全程序和安全塔楼 CN201780070838.X 2017-12-27 CN110235170A 2019-09-13 佩德罗·卡萨泰贾达; 赫雷拉
本发明涉及对检查点进入车辆进行实时检查的安全程序,包括在检查点附近执行的采集阶段(1,2,3),分析阶段(4,5,6,7),包括评估预先确定的风险状况类别与汇集已采集的车辆信息,个人信息和手机信息的进入车辆的总体状况之间的相似度或不同度的步骤(7),包括触发代表触发所述警告的至少一个警告触发动机的警告的结果阶段(8),以及根据所述已触发的警告,发送所述已触发的警告给负责检查点安全的人员,由其决定是否阻止检查点所述进入车辆的决定阶段(9)。
19 用于增强型近地系统的实时数据记录的系统和方法 CN201110274979.8 2011-08-10 CN102376106B 2016-09-21 K·J·康纳; G·A·奥斯特伦; C·D·贝特曼
本发明涉及用于增强型近地系统的实时数据记录的系统和方法。用于执行有效的,价廉的航空器传感器数据的数据记录的系统和方法。在航空器(18)上的示例系统(20)包括提供与多个航空电子部件相关的传感器数据的多个数据源(34),经由一个或多个数据总线(32)与多个数据源信号通信的线路能更换处理单元(24),经由数据电缆连接到线路能更换处理单元的无线路由器(26)和与无线路由器无线数据通信的便携式数据单元(28)。无线路由器从线路能更换处理单元接收至少一部分传感器数据并且将接收到的传感器数据发送到便携式数据单元。
20 用于增强型近地系统的实时数据记录的系统和方法 CN201110274979.8 2011-08-10 CN102376106A 2012-03-14 K·J·康纳; G·A·奥斯特伦; C·D·贝特曼
本发明涉及用于增强型近地系统的实时数据记录的系统和方法。用于执行有效的,价廉的航空器传感器数据的数据记录的系统和方法。在航空器(18)上的示例系统(20)包括提供与多个航空电子部件相关的传感器数据的多个数据源(34),经由一个或多个数据总线(32)与多个数据源信号通信的线路能更换处理单元(24),经由数据电缆连接到线路能更换处理单元的无线路由器(26)和与无线路由器无线数据通信的便携式数据单元(28)。无线路由器从线路能更换处理单元接收至少一部分传感器数据并且将接收到的传感器数据发送到便携式数据单元。
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