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公开(公告)号：US20160281808A1
公开(公告)日：2016-09-29
申请号：US14668392
申请日：2015-03-25
Applicant: Honeywell International Inc.
Inventor： Andrew Fannon Lamkin , Christopher Montano , PerriLynne Silva
CPC classification number: F16D66/024 , B60T17/22 , F16D55/38 , F16D55/40 , F16D65/52 , F16D66/021 , F16D66/025 , G01N27/72
Abstract: In some examples, a brake wear measurement system includes an emitter configured to emit a signal and a passive powered sensor system including a controller and a sensor configured to sense the signal emitted by the emitter. The emitter and the sensor of the sensor system are mounted on the brake assembly such as the emitter and the sensor may be configured to move relative to each other as the brake disc stack wears. Thus, a characteristic of the signal emitted by the emitter and sensed by the sensor may change as a function of the brake disc stack wear. The brake wear measurement may further include a processor configured to receive the output generated by the sensor and determine, based on the output, an amount of wear of the brake disc stack assembly.
Abstract translation: 在一些示例中，制动磨损测量系统包括被配置为发射信号的发射器和包括控制器和被配置为感测由发射器发射的信号的传感器的无源动力传感器系统。 传感器系统的发射器和传感器安装在诸如发射器的制动组件上，并且传感器可以被配置为当制动盘堆叠磨损时相对于彼此移动。 因此，由发射器发射并由传感器感测的信号的特性可以根据制动盘堆叠磨损而变化。 制动磨损测量还可以包括被配置为接收由传感器产生的输出并且基于输出确定制动盘堆叠组件的磨损量的处理器。
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公开(公告)号：US09037392B2
公开(公告)日：2015-05-19
申请号：US13742688
申请日：2013-01-16
Applicant: Honeywell International Inc.
Inventor： James Christopher Kirk , Matej Dusik , Joseph Duval , Jiri Vasek , Andrew Fannon Lamkin
Abstract: 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.
Abstract translation: 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。
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公开(公告)号：US20140081567A1
公开(公告)日：2014-03-20
申请号：US13742688
申请日：2013-01-16
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： James Christopher Kirk , Matej Dusik , Joseph Duval , Jiri Vasek , Andrew Fannon Lamkin
Abstract: 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.
Abstract translation: 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。
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公开(公告)号：US20140062756A1
公开(公告)日：2014-03-06
申请号：US13835122
申请日：2013-03-15
Applicant: Honeywell International Inc.
Inventor： Andrew Fannon Lamkin , Jeffrey W. Starr , Duke Buster
IPC: G01S13/93
CPC classification number: G01S13/9303 , G01S7/04 , G01S7/22 , G01S13/931 , G01S2013/9335 , G08G5/0021 , G08G5/065
Abstract: A ground obstacle collision-avoidance system includes a plurality of radar sensor modules that each receive at a radar detector radar return signals corresponding to reflections of the emitted signal from a ground obstacle, and transmits radar information associated with the received radar signal reflections reflected from the ground obstacle, wherein each of the plurality of radar sensor modules are uniquely located on a surface of an aircraft that is at risk for collision with a ground obstacle if the aircraft is moving; a gateway unit that receives the radar information transmitted from the radar sensor module and transmits information associated with the received radar information; a processing system configured to determine a distance from the installation aircraft to a detected ground object detected; and a display configured to present a plan view indicating an aircraft icon and a graphical ground obstacle icon that is associated with the detected ground obstacle.
Abstract translation: 地面障碍物碰撞避免系统包括多个雷达传感器模块，每个雷达传感器模块在雷达检测器处接收雷达对应于来自地面障碍物的发射信号的反射的返回信号，并发射与从雷达信号反射的接收的雷达信号反射相关联的雷达信息 地面障碍物，其中所述多个雷达传感器模块中的每一个唯一地位于飞机的表面上，如果所述飞行器正在移动，则所述飞机的表面处于与地面障碍物碰撞的风险中; 接收从雷达传感器模块发送的雷达信息并发送与所接收的雷达信息相关联的信息的网关单元; 被配置为确定从所述安装飞行器到检测到的检测到的地面物体的距离的处理系统; 以及显示器，被配置为呈现指示飞行器图标的平面图和与所检测的地面障碍物相关联的图形地面障碍物图标。
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公开(公告)号：US09898003B2
公开(公告)日：2018-02-20
申请号：US14711952
申请日：2015-05-14
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Matthew Warpinski , Andrew Fannon Lamkin , Duke Buster
CPC classification number: G05D1/0022 , B64C19/00 , B64C25/405 , B64F1/002 , B64F1/22 , G05D1/0016 , G05D1/0083 , G08G5/0013 , G08G5/0026 , G08G5/0043 , G08G5/065 , Y02T50/823
Abstract: Embodiments of the subject matter described herein provide an innovative method and system capable of enabling external ground control of a manned aircraft without a pilot or crew, in order to (i) move the aircraft, and (ii) command various subsystems of the aircraft. The provided method and system supports secure wireless communication between the aircraft and a remote device.
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Patent Agency Ranking
6.发明授权公开(公告)号：US09842388B2
公开(公告)日：2017-12-12
申请号：US14790328
申请日：2015-07-02
Applicant: Honeywell International Inc.
Inventor： Andrew Fannon Lamkin , Matthew Warpinski , Duke Buster
CPC classification number: G06T7/0002 , G01C21/206 , G01C23/00 , G06F3/011 , G06F3/012 , G06T7/70 , G06T11/60
Abstract: Systems and methods for location aware augmented vision aircraft monitoring and inspection are provided. In one embodiment, a method for location aware augmented vision assisted aircraft inspection and monitoring comprises: obtaining status information regarding an aircraft from an on-board aircraft network; obtaining a user location from a user carried augmented vision display device; refining a first data set from the status information based at least in part on the user location; wirelessly transmitting the first data set to the user carried augmented vision display device; determining an orientation of the user carried augmented vision display device with respect to the aircraft; and displaying at least a subset of the first data set on the user carried augmented vision display device, wherein the subset of the first data set is determined at least in part based on the orientation of the user carried augmented vision display device.
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7.发明申请WIRELESS DATA COMMUNICATION USING AIRBORNE LIGHTING AND GROUND SUPPORT SYSTEMS 审中-公开使用AIRBORNE照明和接地支持系统进行无线数据通信公开(公告)号：US20150349882A1
公开(公告)日：2015-12-03
申请号：US14287844
申请日：2014-05-27
Applicant: Honeywell International Inc.
Inventor： Andrew Fannon Lamkin , Joseph Nutaro , Duke Buster , Craig Giffen
IPC: H04B10/112 , H04B10/40
CPC classification number: H04B10/1123
Abstract: A system for wireless optical data communications comprises a first gateway device including a processor onboard a first aircraft, and a first set of light sources onboard the aircraft in operative communication with the gateway device. The light sources comprise a plurality of light emitting diodes. A first optical receiver is onboard the aircraft and in operative communication with the gateway device. In a transmission mode, the gateway device is configured to monitor a databus onboard the aircraft for digital data selected for wireless optical transmission, encode the digital data selected for wireless optical transmission with a compatible optical modulation scheme, and broadcast the encoded digital data through modulated light emitted from the set of light sources. In a reception mode, the gateway device is configured to decode digital data from modulated light captured by the optical receiver from a wireless optical transmission from the ground or another aircraft.
Abstract translation: 一种用于无线光学数据通信的系统包括：第一网关设备，其包括第一飞行器上的处理器和与所述网关设备可操作地通信的飞行器上的第一组光源。 光源包括多个发光二极管。 第一光接收器在飞机上并与网关设备进行操作性通信。 在传输模式中，网关设备被配置为监视飞机上用于无线光传输的数字数据的数据总线，用兼容的光调制方案对被选择用于无线光传输的数字数据进行编码，并通过调制方式广播编码的数字数据 从该组光源发出的光。 在接收模式中，网关设备被配置为从来自地面或另一飞行器的无线光传输器从由光接收器捕获的调制光解码数字数据。
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公开(公告)号：US20160334786A1
公开(公告)日：2016-11-17
申请号：US14711952
申请日：2015-05-14
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Matthew Warpinski , Andrew Fannon Lamkin , Duke Buster
CPC classification number: G05D1/0022 , B64C19/00 , B64C25/405 , B64F1/002 , B64F1/22 , G05D1/0016 , G05D1/0083 , G08G5/0013 , G08G5/0026 , G08G5/0043 , G08G5/065 , Y02T50/823
Abstract: Embodiments of the subject matter described herein provide an innovative method and system capable of enabling external ground control of a manned aircraft without a pilot or crew, in order to (i) move the aircraft, and (ii) command various subsystems of the aircraft. The provided method and system supports secure wireless communication between the aircraft and a remote device.
Abstract translation: 本文所描述的主题的实施例提供了一种创新的方法和系统，其能够在没有飞行员或机组人员的情况下对载人飞机进行外部地面控制，以便（i）移动飞行器，以及（ii）命令飞机的各种子系统。 所提供的方法和系统支持飞机和远程设备之间的安全无线通信。
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公开(公告)号：US09269205B1
公开(公告)日：2016-02-23
申请号：US14504092
申请日：2014-10-01
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Andrew Fannon Lamkin , Matthew Warpinski , Duke Buster , Joseph J. Nutaro
CPC classification number: G07C5/0808 , G06Q10/04 , G06Q30/0201 , G07C5/0825 , G07C5/0841 , G08G5/0021 , G08G5/0052
Abstract: An environmental impact measurement system for an aircraft includes a one-way data interface and a processing system. The one-way data interface is adapted to continuously receive and transmit aircraft data and flight plan data. The processing system is in operable communication with the one-way data interface to receive the aircraft data and the flight plan data transmitted therefrom. The processing system is configured, upon receipt of the aircraft data and the flight plan data, to generate at least data representative of real-time environmental impact of the aircraft, and recommendations for improving the real-time environmental impact of the aircraft.
Abstract translation: 飞机的环境影响测量系统包括单向数据接口和处理系统。 单向数据接口适用于连续接收和发送飞机数据和飞行计划数据。 处理系统与单向数据接口可操作地通信以接收飞行器数据和从其发送的飞行计划数据。 在接收到飞机数据和飞行计划数据之后，处理系统被配置为产生至少表示飞行器的实时环境影响的数据，以及用于改善飞机的实时环境影响的建议。
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公开(公告)号：US20130321192A1
公开(公告)日：2013-12-05
申请号：US13689495
申请日：2012-11-29
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Jeffrey W. Starr , Andrew Fannon Lamkin , Duke Buster
IPC: G01S13/93
Abstract: A ground crew collision-avoidance system includes a plurality of radar sensor modules that each emit a radar signal, receives at a radar detector radar return signals corresponding to reflections of the emitted signal from a ground object, and transmits radar information associated with the received radar signal reflections reflected from the ground object, wherein each of the plurality of radar sensor modules are uniquely located on a surface of an aircraft that is at risk for collision with a ground object while the aircraft is being towed; a gateway unit that receives the radar information transmitted from the radar sensor module and transmits information associated with the received radar information; and a ground crew alert indicator that receives the information transmitted by the gateway unit and that presents a graphical alert icon on a display. The display indicates a likelihood of collision between the aircraft and the ground object.
Abstract translation: 地面机组碰撞避免系统包括多个雷达传感器模块，每个雷达传感器模块各自发射雷达信号，在雷达检测器处接收雷达对应于来自地面物体的发射信号的反射的返回信号，并发射与接收的雷达相关的雷达信息 从地面物体反射的信号反射，其中多个雷达传感器模块中的每一个独特地位于飞行器的表面上，该飞机表面在飞机被拖曳的同时有与地面物体碰撞的危险; 接收从雷达传感器模块发送的雷达信息并发送与所接收的雷达信息相关联的信息的网关单元; 以及接收由网关单元发送的信息并且在显示器上呈现图形警报图标的地勤人员警报指示器。 显示屏显示飞机与地面物体之间发生碰撞的可能性。
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