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1. 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。

2. 发明申请

US20190158601A1 SOFTWARE DEVELOPMENT KIT FOR AIRCRAFT TABLET DEVICE AND AIRBORNE APPLICATION SERVER 审中-公开
公开(公告)号：US20190158601A1
公开(公告)日：2019-05-23
申请号：US16254198
申请日：2019-01-22
申请人： Honeywell International Inc.
发明人： Matej Dusik , John Beckwith , John Hajdukiewicz , Filip Magula , Frantisek Mikulu , Jiri Vasek
IPC分类号： H04L29/08 , G06F8/70
CPC分类号： H04L67/12 , B64D2045/0075 , G06F8/70 , H04L67/02 , H04W88/02
摘要： A server system for an aircraft is provided. In one embodiment, the server system comprises an aircraft server unit that is operative to receive data from one or more data sources, and a software development kit (SDK) application server in operative communication with the aircraft server unit. The SDK application server comprises one or more processing core modules configured to process the data from the one or more data sources, and one or more application modules including one or more aircraft tablet device logic modules that are configured to respectively execute one or more aircraft tablet device applications. The data processed by the one or more processing core modules is separated from the one or more aircraft tablet device logic modules. The SDK application server is configured to communicate with one or more external portable computing devices.

3. 发明申请

US20180115609A1 SOFTWARE DEVELOPMENT KIT FOR AIRCRAFT TABLET DEVICE AND AIRBORNE APPLICATION SERVER 审中-公开
公开(公告)号：US20180115609A1
公开(公告)日：2018-04-26
申请号：US15334822
申请日：2016-10-26
申请人： Honeywell International Inc.
发明人： Matej Dusik , John Beckwith , John Hajdukiewicz , Filip Magula , Frantisek Mikulu , Jiri Vasek
IPC分类号： H04L29/08
CPC分类号： H04L67/12 , B64D2045/0075 , G06F8/70 , H04L67/02 , H04W88/02
摘要： A server system for an aircraft is provided. In one embodiment, the server system comprises an aircraft server unit that is operative to receive data from one or more data sources, and a software development kit (SDK) application server in operative communication with the aircraft server unit. The SDK application server comprises one or more processing core modules configured to process the data from the one or more data sources, and one or more application modules including one or more aircraft tablet device logic modules that are configured to respectively execute one or more aircraft tablet device applications. The data processed by the one or more processing core modules is separated from the one or more aircraft tablet device logic modules. The SDK application server is configured to communicate with one or more external portable computing devices.

4. 发明申请

US20180013838A1 SYSTEMS AND METHODS FOR COMMUNICATING DATA FROM OFF-VEHICLE DATA SOURCES TO A VEHICLE 审中-公开
公开(公告)号：US20180013838A1
公开(公告)日：2018-01-11
申请号：US15203436
申请日：2016-07-06
申请人： Honeywell International Inc.
发明人： David B. Goldstein , James Alexander Nicholls , Matej Dusik , Simon Innocent , Anup Raje , Bill Nelson
IPC分类号： H04L29/08 , H04L29/06
CPC分类号： H04L67/146 , G08G5/0013 , G08G5/0052 , G08G5/0091 , H04L67/06 , H04L67/10 , H04L67/42
摘要： Systems and methods for communicating data from off-vehicle data sources to a vehicle are provided. In one embodiment, a method for obtaining data for a vehicle comprises: initiating an information request from on-board a vehicle; formatting the information request onboard the vehicle into a data file format to generate a request file; performing a wireless file transfer of the request file from the vehicle to a data center, wherein the request file is transferred to a file system location; polling the file system location for creation of a response file corresponding to the request file; when the response file is detected within the file system location, retrieving the response file from the data center to the vehicle; and displaying at the vehicle information responsive to the information request from the response file. In some embodiments, the file system location is a file system location uniquely associated with the vehicle.

5. 发明申请

US20160114901A1 METHODS AND SYSTEMS FOR MANAGING SITUATION AWARENESS INFORMATION AND ALERTS IN A COCKPIT DISPLAY 审中-公开
标题翻译：用于管理情景显示中的状况意识信息和警报的方法和系统
公开(公告)号：US20160114901A1
公开(公告)日：2016-04-28
申请号：US14860849
申请日：2015-09-22
申请人： HONEYWELL INTERNATIONAL INC.
发明人： Jean-Luc Derouineau , Matej Dusik
IPC分类号： B64D45/00
CPC分类号： B64D45/00 , G08G5/0008 , G08G5/0013 , G08G5/0021 , G08G5/0091
摘要： Methods and system are provided for displaying information on a display device of an aircraft as well as processing crowd sourced information from other aircraft, sensors and information systems in a ground server, and provide it back to aircraft via communication means. In one embodiment, the method includes retrieving information that indicates a current situation and that has been entered by a user, the information being from at least one of a server and another aircraft; determining current situation display data based on the information; and graphically displaying the information on the display based on the current situation display data.
摘要翻译：方法和系统被提供用于在飞机的显示设备上显示信息，以及处理来自地面服务器中的其他飞行器，传感器和信息系统的人群来源的信息，并且经由通信装置将其返回给飞机。在一个实施例中，该方法包括检索指示当前情况并且已由用户输入的信息，该信息来自服务器和另一飞行器中的至少一个; 基于该信息确定当前情况显示数据; 并且基于当前情况显示数据以图形方式显示在显示器上的信息。

6. 发明申请

US20160093302A1 SYSTEMS AND METHODS FOR CONVERTING TAXIWAY VOICE COMMANDS INTO TAXIWAY TEXTUAL COMMANDS 有权
标题翻译：将税收政策转换为税收文本指令的系统和方法
公开(公告)号：US20160093302A1
公开(公告)日：2016-03-31
申请号：US14497897
申请日：2014-09-26
申请人： HONEYWELL INTERNATIONAL INC.
发明人： Jan Bilek , Vaclav Pfeifer , Matej Dusik , Tomas Kralicek
IPC分类号： G10L15/26 , G10L15/22 , G08G5/06 , G10L21/10 , G10L25/48
CPC分类号： G10L15/26 , G08G5/0013 , G08G5/065 , G10L15/22 , G10L21/10 , G10L25/48 , G10L2015/223
摘要： Systems and methods are provided for converting taxiway voice commands into taxiway textual commands. In various embodiments, the systems can comprise a radio receiver that is configured to receive the taxiway voice commands from an air traffic control center, a voice recognition processor coupled to the radio receiver that is configured to receive and convert the taxiway voice commands into the taxiway textual commands, and/or a taxiway clearance display coupled to the voice recognition processor that is configured to receive and display the taxiway textual commands.
摘要翻译：系统和方法用于将滑行道语音命令转换为滑行道文本命令。在各种实施例中，系统可以包括无线电接收机，其被配置为从空中交通控制中心接收滑行道语音命令，耦合到无线电接收机的语音识别处理器，其被配置为接收并将滑行道语音命令转换成滑行道文本命令和/或与被配置为接收和显示滑行道文本命令的语音识别处理器耦合的滑行道清除显示。

7. 发明申请

US20140081567A1 AIRPORT SURFACE COLLISION-AVOIDANCE SYSTEM (ASCAS) 有权
标题翻译：机场表面碰撞避免系统（ASCAS）
公开(公告)号：US20140081567A1
公开(公告)日：2014-03-20
申请号：US13742688
申请日：2013-01-16
申请人： HONEYWELL INTERNATIONAL INC.
发明人： James Christopher Kirk , Matej Dusik , Joseph Duval , Jiri Vasek , Andrew Fannon Lamkin
IPC分类号： G08G5/04 , G08G5/06
CPC分类号： G08G5/06 , B64D47/08 , G01S13/93 , G08G5/0021 , G08G5/04 , G08G5/065
摘要： Systems and methods for performing airport surface collision-avoidance. A wingtip-mounted camera allows the pilot to positively ascertain that the wingtip will clear objects located in the video. An exemplary system implemented on an aircraft includes a wingtip module having a camera that generates a video stream and a communication device that transmits the generated video stream. A processor receives the video stream and generates a reticule for the video stream. A display device simultaneously presents the video stream and the reticule. The reticule includes a horizon line and is based on a focal length of a lens of the camera and height of the camera above ground. The reticule includes curved and/or straight distance lines and curved or straight travel lines. The travel line(s) correspond to at least one aircraft component or a zone of importance and are based on location of the camera and trajectory of the aircraft.
摘要翻译：执行机场防碰撞的系统和方法。机翼安装的相机允许飞行员肯定地确定翼尖将清除位于视频中的物体。在飞行器上实现的示例性系统包括具有生成视频流的摄像机的翼尖模块和发送生成的视频流的通信设备。处理器接收视频流并生成视频流的网状。显示装置同时呈现视频流和网状物。网格包括水平线，并且基于相机的镜头的焦距和相机在地面上方的高度。网状物包括弯曲和/或直线距离线和弯曲或直线行进线。行驶线对应于至少一个飞行器部件或重要的区域，并且基于相机的位置和飞行器的轨迹。

8. 发明授权

US10666734B2 Software development kit for aircraft tablet device and airborne application server 有权
公开(公告)号：US10666734B2
公开(公告)日：2020-05-26
申请号：US16254198
申请日：2019-01-22
申请人： Honeywell International Inc.
发明人： Matej Dusik , John Beckwith , John Hajdukiewicz , Filip Magula , Frantisek Mikulu , Jiri Vasek
IPC分类号： H04L29/08 , G06F8/70 , H04W88/02 , B64D45/00
摘要： A server system for an aircraft is provided. In one embodiment, the server system comprises an aircraft server unit that is operative to receive data from one or more data sources, and a software development kit (SDK) application server in operative communication with the aircraft server unit. The SDK application server comprises one or more processing core modules configured to process the data from the one or more data sources, and one or more application modules including one or more aircraft tablet device logic modules that are configured to respectively execute one or more aircraft tablet device applications. The data processed by the one or more processing core modules is separated from the one or more aircraft tablet device logic modules. The SDK application server is configured to communicate with one or more external portable computing devices.

9. 发明授权

US10225349B2 Software development kit for aircraft tablet device and airborne application server 有权
公开(公告)号：US10225349B2
公开(公告)日：2019-03-05
申请号：US15334822
申请日：2016-10-26
申请人： Honeywell International Inc.
发明人： Matej Dusik , John Beckwith , John Hajdukiewicz , Filip Magula , Frantisek Mikulu , Jiri Vasek
IPC分类号： H04W80/04 , H04L29/08 , G06F8/70 , H04W88/02 , B64D45/00
摘要： A server system for an aircraft is provided. In one embodiment, the server system comprises an aircraft server unit that is operative to receive data from one or more data sources, and a software development kit (SDK) application server in operative communication with the aircraft server unit. The SDK application server comprises one or more processing core modules configured to process the data from the one or more data sources, and one or more application modules including one or more aircraft tablet device logic modules that are configured to respectively execute one or more aircraft tablet device applications. The data processed by the one or more processing core modules is separated from the one or more aircraft tablet device logic modules. The SDK application server is configured to communicate with one or more external portable computing devices.

10. 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.

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