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1. 发明申请

US20170302684A1 SECURITY ARCHITECTURE FOR THE CONNECTED AIRCRAFT 审中-公开
公开(公告)号：US20170302684A1
公开(公告)日：2017-10-19
申请号：US14336230
申请日：2014-07-21
申请人： Honeywell International Inc.
发明人： James C. Kirk , Daniel P. Johnson , Joseph J. Palovick, III , Dewey Mann , Derick Lucas Gerlock
IPC分类号： H04L29/06 , H04L29/08
CPC分类号： H04L63/1416 , G06F2221/2113 , H04L63/101 , H04L63/105 , H04L63/1408 , H04L67/12 , H04W12/0806
摘要： Systems and methods of a security architecture for a connected aircraft are disclosed. In at least one embodiment, an avionics server comprises a plurality of device ports, wherein each of the plurality of device ports is coupled to a respective one of a plurality of device network interface cards and dedicated to a respective one of a plurality of avionics domains which corresponds to the respective device network interface card. Further, at least one processing device is configured to identify one or more signals from a respective user received at one or more of the plurality of device ports and to verify whether the user has access to the respective avionics domains that are dedicated to the one or more device ports over which the one or more signals are received.

2. 发明授权

US10375087B2 Security architecture for the connected aircraft 有权
公开(公告)号：US10375087B2
公开(公告)日：2019-08-06
申请号：US14336230
申请日：2014-07-21
申请人： Honeywell International Inc.
发明人： James C. Kirk , Daniel P. Johnson , Joseph J. Palovick, III , Dewey Mann , Derick Lucas Gerlock
IPC分类号： H04L29/06 , H04L29/08 , H04W12/08
摘要： Systems and methods of a security architecture for a connected aircraft are disclosed. In at least one embodiment, an avionics server comprises a plurality of device ports, wherein each of the plurality of device ports is coupled to a respective one of a plurality of device network interface cards and dedicated to a respective one of a plurality of avionics domains which corresponds to the respective device network interface card. Further, at least one processing device is configured to identify one or more signals from a respective user received at one or more of the plurality of device ports and to verify whether the user has access to the respective avionics domains that are dedicated to the one or more device ports over which the one or more signals are received.

3. 发明授权

US10451725B2 Systems and methods for performing vehicle collision-avoidance warning via sensor pulse 有权
公开(公告)号：US10451725B2
公开(公告)日：2019-10-22
申请号：US16359692
申请日：2019-03-20
申请人： Honeywell International Inc.
发明人： James C. Kirk
IPC分类号： G01S13/66 , G08G5/06 , G08G5/04 , B64D43/00 , B64D45/00 , G01S13/93 , B64C25/42 , G01S13/76 , G01S7/04 , G01C23/00 , B60Q9/00
摘要： Systems and methods for embedding a warning signal in a sensor pulse. When a taxi anticollision system of a host aircraft senses a threat headed for the aircraft, a warning signal is embedded in a sensor pulse to warn the offending vehicle that it is in the field of view of the host aircraft's sensor and is moving on a trajectory that is threatening collision with the host aircraft. Alternately, the radar issues a dedicated pulse for reading and alerting the receiving device.

4. 发明申请

US20140085124A1 SYSTEMS AND METHODS FOR USING RADAR-ADAPTIVE BEAM PATTERN FOR WINGTIP PROTECTION 审中-公开
标题翻译：使用雷达自适应光束模式进行WTITIP保护的系统和方法
公开(公告)号：US20140085124A1
公开(公告)日：2014-03-27
申请号：US13889537
申请日：2013-05-08
申请人： Honeywell International Inc.
发明人： Matej Dusik , Jiri Vasek , James C. Kirk , David C. Vacanti , Filip Magula
IPC分类号： G01S13/93 , G01S13/66
CPC分类号： G01S13/66 , B60Q9/008 , B64C25/42 , B64D43/00 , B64D45/00 , G01C23/00 , G01S7/04 , G01S13/765 , G01S13/93 , G01S13/931 , G01S2013/9335 , G01S2013/9339 , G08G5/04 , G08G5/045 , G08G5/065
摘要： Systems and methods for adaptively steering radar beam patterns for coverage during aircraft turns. The radar sensor system is mechanically or electrically steered to alter the radar sensor's beam pattern in order to adapt the radar sensor's field of view (FOV) to cover the area of anticipated aircraft wingtip trajectory. The anticipated trajectory is derived, for example, from the aircraft groundspeed, acceleration, heading, turn rate, tiller position, attitude, taxi clearance, etc.
摘要翻译：用于自适应地引导雷达波束模式以在飞机转弯期间覆盖的系统和方法。雷达传感器系统被机械或电气控制以改变雷达传感器的波束图案，以便使雷达传感器的视场（FOV）适应于预期飞机翼尖轨迹的面积。例如，从飞机地速，加速度，航向，转弯率，分蘖位置，姿态，出租车清关等导出预期轨迹。

5. 发明授权

US09959774B2 Systems and methods for displaying obstacle-avoidance information during surface operations 有权
公开(公告)号：US09959774B2
公开(公告)日：2018-05-01
申请号：US13764701
申请日：2013-02-11
申请人： Honeywell International Inc.
发明人： Jiri Vasek , Ratan Khatwa , James C. Kirk , Olukayode Olofinboba , Pavel Kolcarek , Tomas Svoboda , Matej Dusik
IPC分类号： G08G5/04 , G01S13/93 , G08G5/00 , G08G5/06
CPC分类号： G08G5/04 , G01S13/93 , G01S13/931 , G01S2013/9335 , G08G5/0021 , G08G5/0078 , G08G5/045 , G08G5/065
摘要： Systems and methods for aiding in pilot awareness of obstacles relative to aircraft features. An exemplary processor receives sensor information from one or more sensors mounted in an aircraft feature (e.g. light modules), determines if at least one obstacle is located within a predefined field of view based on the received sensor or database information and generates an image. The image includes an ownship icon having at least one feature representing wingtips of the aircraft and at least one indicator associated with the determined at least one obstacle. A display device presents the generated image. The display device presents a tip of a first sense coverage area adjacent to one wingtip feature associated with the port wing and a tip of the second sense coverage area adjacent to one wingtip feature associated with the starboard wing. The indicator is presented within at least one of the coverage areas.

6. 发明申请

US20130321177A1 SYSTEMS AND METHODS FOR PERFORMING VEHICLE COLLISION-AVOIDANCE WARNING VIA SENSOR PULSE 审中-公开
标题翻译：通过传感器脉冲执行车辆碰撞避免警报的系统和方法
公开(公告)号：US20130321177A1
公开(公告)日：2013-12-05
申请号：US13888216
申请日：2013-05-06
申请人： HONEYWELL INTERNATIONAL INC.
发明人： James C. Kirk
IPC分类号： B60Q9/00
CPC分类号： G01S13/66 , B60Q9/008 , B64C25/42 , B64D43/00 , B64D45/00 , G01C23/00 , G01S7/04 , G01S13/765 , G01S13/93 , G01S13/931 , G01S2013/9335 , G01S2013/9339 , G08G5/04 , G08G5/045 , G08G5/065
摘要： Systems and methods for embedding a warning signal in a sensor pulse. When a taxi anticollision system of a host aircraft senses a threat headed for the aircraft, a warning signal is embedded in a sensor pulse to warn the offending vehicle that it is in the field of view of the host aircraft's sensor and is moving on a trajectory that is threatening collision with the host aircraft. Alternately, the radar issues a dedicated pulse for reading and alerting the receiving device.
摘要翻译：在传感器脉冲中嵌入警告信号的系统和方法。当主机飞机的出租车防冲突系统感测到飞机的威胁时，将一个警告信号嵌入到传感器脉冲中，以警告违规车辆它在主机飞行器的传感器的视场内并且正在轨迹上移动这与威胁与主机的碰撞。或者，雷达发出用于读取和警告接收设备的专用脉冲。

7. 发明申请

US20190219684A1 SYSTEMS AND METHODS FOR PERFORMING VEHICLE COLLISION-AVOIDANCE WARNING VIA SENSOR PULSE 审中-公开
公开(公告)号：US20190219684A1
公开(公告)日：2019-07-18
申请号：US16359692
申请日：2019-03-20
申请人： Honeywell International Inc.
发明人： James C. Kirk
IPC分类号： G01S13/66 , B60Q9/00 , G01C23/00 , G08G5/06 , G08G5/04 , B64D43/00 , B64D45/00 , G01S13/93 , B64C25/42 , G01S13/76 , G01S7/04
CPC分类号： G01S13/66 , B60Q9/008 , B64C25/42 , B64D43/00 , B64D45/00 , G01C23/00 , G01S7/04 , G01S13/765 , G01S13/93 , G01S13/931 , G01S2013/9335 , G01S2013/9339 , G08G5/04 , G08G5/045 , G08G5/065
摘要： Systems and methods for embedding a warning signal in a sensor pulse. When a taxi anticollision system of a host aircraft senses a threat headed for the aircraft, a warning signal is embedded in a sensor pulse to warn the offending vehicle that it is in the field of view of the host aircraft's sensor and is moving on a trajectory that is threatening collision with the host aircraft. Alternately, the radar issues a dedicated pulse for reading and alerting the receiving device.

8. 发明授权

US10274595B2 Systems and methods for performing vehicle collision-avoidance warning via sensor pulse 有权
公开(公告)号：US10274595B2
公开(公告)日：2019-04-30
申请号：US13888216
申请日：2013-05-06
申请人： Honeywell International Inc.
发明人： James C. Kirk
IPC分类号： B60Q9/00 , G01S7/04 , G08G5/04 , G08G5/06 , B64C25/42 , B64D43/00 , B64D45/00 , G01C23/00 , G01S13/66 , G01S13/76 , G01S13/93
摘要： Systems and methods for embedding a warning signal in a sensor pulse. When a taxi anticollision system of a host aircraft senses a threat headed for the aircraft, a warning signal is embedded in a sensor pulse to warn the offending vehicle that it is in the field of view of the host aircraft's sensor and is moving on a trajectory that is threatening collision with the host aircraft. Alternately, the radar issues a dedicated pulse for reading and alerting the receiving device.

9. 发明申请

US20150329217A1 AIRCRAFT STRIKE ZONE DISPLAY 审中-公开
标题翻译：飞机区域显示
公开(公告)号：US20150329217A1
公开(公告)日：2015-11-19
申请号：US14281627
申请日：2014-05-19
申请人： HONEYWELL INTERNATIONAL INC.
发明人： James C. Kirk , Matej Dusik , Ondrej Pokorny , Andrew F. Lamkin
IPC分类号： B64D45/00 , B64D47/08 , G06K9/00 , B64D43/00
CPC分类号： B64D45/00 , B64D43/00 , B64D47/08 , G06K9/0063 , G06K9/00744 , G06K9/00805 , G08G5/0021 , G08G5/0078 , G08G5/045 , G08G5/065
摘要： A system is configured to generate and display information regarding a strike zone of an aircraft. In some examples, a system is configured to generate and display an image of an environment around an aircraft together with a graphical indication of a strike zone of the aircraft, where the indication is scaled to reflect the strike zone at a distance range of one or more detected objects.
摘要翻译：一个系统被配置为产生和显示有关飞行器的撞击区域的信息。在一些示例中，系统被配置为生成并显示飞行器周围的环境的图像以及飞行器的撞击区域的图形指示，其中指示被缩放以在距离范围1或更多检测到的物体。

10. 发明申请

US20130321176A1 SYSTEMS AND METHODS FOR DISPLAYING OBSTACLE-AVOIDANCE INFORMATION DURING SURFACE OPERATIONS 有权
标题翻译：用于在表面操作期间显示异常避风信息的系统和方法
公开(公告)号：US20130321176A1
公开(公告)日：2013-12-05
申请号：US13764701
申请日：2013-02-11
申请人： HONEYWELL INTERNATIONAL INC.
发明人： Jiri Vasek , Ratan Khatwa , James C. Kirk , Olukayode Olofinboba , Pavel Kolcarek , Tomas Svoboda , Matej Dusik
IPC分类号： G08G5/04
CPC分类号： G08G5/04 , G01S13/93 , G01S13/931 , G01S2013/9335 , G08G5/0021 , G08G5/0078 , G08G5/045 , G08G5/065
摘要： Systems and methods for aiding in pilot awareness of obstacles relative to aircraft features. An exemplary processor receives sensor information from one or more sensors mounted in an aircraft feature (e.g. light modules), determines if at least one obstacle is located within a predefined field of view based on the received sensor or database information and generates an image. The image includes an ownship icon having at least one feature representing wingtips of the aircraft and at least one indicator associated with the determined at least one obstacle. A display device presents the generated image. The display device presents a tip of a first sense coverage area adjacent to one wingtip feature associated with the port wing and a tip of the second sense coverage area adjacent to one wingtip feature associated with the starboard wing. The indicator is presented within at least one of the coverage areas.
摘要翻译：帮助驾驶员了解相对于飞机特征的障碍的系统和方法。示例性处理器从安装在飞行器特征（例如，光模块）中的一个或多个传感器接收传感器信息，基于接收到的传感器或数据库信息确定至少一个障碍物是否位于预定视场内，并产生图像。图像包括具有至少一个表示飞机的翼尖的特征的自身图标以及与所确定的至少一个障碍物相关联的至少一个指示符。显示装置呈现生成的图像。所述显示装置呈现与所述端口翼相关联的一个翼尖特征附近的第一感测覆盖区域的尖端和与所述右舷翼相关联的一个翼尖特征相邻的所述第二感测覆盖区域的尖端。该指示符被呈现在至少一个覆盖区域内。

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