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公开(公告)号：US20240282200A1
公开(公告)日：2024-08-22
申请号：US18295083
申请日：2023-04-03
CPC分类号： G08G5/0021 , B64D43/02 , G08G5/0047
摘要： Systems and methods are provided for displaying differential ground speed for traffic surrounding an aircraft. The system includes an aircraft control panel in a cockpit of an ownship aircraft and a digital traffic display located on the control panel. The digital traffic display provides cockpit display of traffic information (CDTI) that shows a speed scale with a graphical display of the ground speed of the ownship aircraft and the ground speed of traffic to follow (TTF). The separation scale also shows a graphical display of a separation distance between the ownship aircraft and the TTF. A change in separation distance is calculated based of the difference in ground speed between the ownship aircraft and the TTF. An advisory/warning indicator that shows a color-coded status of the change in separation distance in comparison a pre-determined desired separation distance between the ownship aircraft and the TTF.
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公开(公告)号：US11476921B2
公开(公告)日：2022-10-18
申请号：US17097934
申请日：2020-11-13
摘要： A method for sending environmental data to a vehicle in transit is disclosed. The method is performed by a ground system. The method includes receiving new environmental data from a plurality of environmental data providers. The method also includes synthesizing an update template that identifies recommended portions of relevant data that are available to be uploaded for at least one of a plurality of environmental data services. The method also includes sending the update template to the vehicle using a low-bandwidth connection, wherein the update template is sent by the ground system without first receiving a request for the update template. The method also includes receiving, from the vehicle, a request for the recommended portions of relevant data. The method also includes sending the recommended portions of relevant data to the vehicle in an update package using a high-bandwidth connection.
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公开(公告)号：US10854092B1
公开(公告)日：2020-12-01
申请号：US16577708
申请日：2019-09-20
发明人： Muthusankar Subramaniyan , Sivakumar Kanagarajan , Visvanathan Thanigai Nathan , Kiran Gopala Krishna , Mohammed Ibrahim Mohideen
IPC分类号： G08G5/00
摘要： A method and system for time-based viewing to coordinate airport collaborative decision making (A-CDM) events between a pilot and ground personnel on a cockpit display of an aircraft of generating a time scale with a list of A-CDM events of the aircraft during inbound, turnaround and outbound flight operations to an airport based sensor data contributed by aircraft systems and data of A-CDM event related to airport operations to generate a current time moving window in the time scale for identifying A-CDM events; generating a graphic user interface using the sensor data for positioning the current time moving window on the time scale; and collaboratively communicating with ground personnel decisions based on an aircraft state and a current A-CDM event identified by the positioning of the current time moving window in the time scale to expedite completion of a particular A-CDM event.
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公开(公告)号：US20200051441A1
公开(公告)日：2020-02-13
申请号：US16100763
申请日：2018-08-10
发明人： Sripathi Ramachandra , Greg Carlucci , Richard Snyder , Mohammed Ibrahim Mohideen , Mark Pearson , Hyden Lopez , Christopher Raj Mariadoss
摘要： An aircraft and a method for operating the same are provided. The aircraft, for example, may include, but is not limited to, a flight management system, a vertical situation display, and a processor configured to determine a first variable, a second variable and a third variable, determine flight plan data for the first, second and third variables, generate display data for the vertical situation display, the display data including the scale of the first second and third variables and a vector corresponding to the flight plan data of the first variable and second variable scaled to the first scale and the second scale, wherein the scale of the third variable is non-linear and varies based upon the flight plan data corresponding to the third variable relative to the vector, and output the generated display data to the vertical situation display for display on the vertical situation display.
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5.发明授权公开(公告)号：US10179655B2
公开(公告)日：2019-01-15
申请号：US15582216
申请日：2017-04-28
摘要： A system is provided for generating an alert to the presence of emission vapors for a low altitude in-flight aircraft. An obstacle database and a terrain database provide parameters for obstacles and terrain features to a synthetic vision processor. The processor creates a graphic overlay of the terrain and obstacles that is combined with thermal images of emission vapors by a combined vision processor to create a combined synthetic image. An emissions threat calculator analyzes the synthetic image for the presence of emission vapors. If any emission vapors are detected in proximity to the aircraft, an alert and suggested maneuvers to avoid the emission vapors are sent to the aircraft.
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公开(公告)号：US20180322792A1
公开(公告)日：2018-11-08
申请号：US15588944
申请日：2017-05-08
发明人： Sachin Pratap , Jagadeesh Shankar , Visvanathan Thanigai Nathan , Mohammed Ibrahim Mohideen , Shobana Arumugam
IPC分类号： G08G5/00 , B64D43/00 , G06F3/0484
CPC分类号： G08G5/0021 , B64D43/00 , G06F3/04845 , G06F3/04847 , G08G5/0013 , G08G5/0047 , G08G5/0052 , G08G5/0078 , G08G5/0091
摘要： A display system is configured to provide a display to an aircraft flight crew. The system includes an image display device, a data storage device, a flight management system, a processing unit in operable electronic communication with the image display device, the data storage device, and the flight management system. The processing unit includes a computer processor that is configured to receive a time-based requirement to a point of interest associated with operation of the aircraft. Via the image display device, a flight display includes a graphically depicted time tape. The time tape includes a time scale. Also graphically depicted within the time tape is the point of interest using a first symbology and the time-based requirement using a second symbology. Operational parameter data of the aircraft allows determination of the ability of the aircraft to achieve the time-based requirement and graphical depiction within the time tape of the ability of the aircraft to achieve the time-based requirement using a third symbology.
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公开(公告)号：US20180276598A1
公开(公告)日：2018-09-27
申请号：US15542344
申请日：2016-01-05
发明人： Venkata Subbaiah Y , Ashok Giri , Kuldeep Sharma , Rachana K. J , Sudeesh Thatha , Neal Anthony Muggleton , Sudhir Kamath , Vishnu Vardhan , Kushagra Thakur , Praveen Galagali , Pierre Van Neste , Chinmaya Kar , Liana Maria Kiff , Mohammed Ibrahim Mohideen
CPC分类号： G06Q10/087 , A41D1/002 , A41D13/00 , A41D13/11 , A41D2600/20 , A61F2011/145 , B65G43/00 , G05B15/02 , G06Q20/18 , G06Q50/265 , G07F17/0042 , G07F17/18
摘要： Embodiments relate generally to a system having one or more computerized kiosks (102, 150, 160, 180, 192) operable to associate a personal protection device (104) to a worker's personal information. In some embodiments, the kiosk (102, 150, 160, 180, 192) can use the worker's personal information to custom configure the personal protection device (104), so that the device (104) will better suit the needs of the specific worker.
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公开(公告)号：US10041673B2
公开(公告)日：2018-08-07
申请号：US13951235
申请日：2013-07-25
CPC分类号： F23N5/242 , F23G7/085 , G06T7/0002 , G06T7/269 , G06T2207/10016 , G06T2207/10048 , G06T2207/20081
摘要： Methods, systems, and computer-readable and executable instructions are described herein. One method includes receiving a sequence of images of a flare stack area from a thermal imaging component, identifying a first portion of the flare stack area moving at a first threshold optical flow using the sequence of images of the flare stack area, and identifying a second portion of the flare stack area moving at a second threshold optical flow using the sequence of images of the flare stack area.
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公开(公告)号：US09752893B2
公开(公告)日：2017-09-05
申请号：US14813957
申请日：2015-07-30
CPC分类号： G01C23/005 , B64D45/04 , G05D1/0684 , G06K9/00637 , G08G5/0021 , G08G5/025
摘要： A display system for an aircraft includes a sensor configured to capture data associated with a landing platform on a movable carrier. The data includes current energy parameters of the movable carrier. The display system further includes a processing unit configured to receive the data representative of the landing platform. The processing unit is further configured to generate display commands associated with the landing platform. The display system further includes a display device coupled the processing unit for receiving the display commands and operable to render first symbology representing the landing platform.
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公开(公告)号：US20150058003A1
公开(公告)日：2015-02-26
申请号：US13974399
申请日：2013-08-23
IPC分类号： G10L15/20
CPC分类号： G10L15/20 , G10L2015/226 , G10L2015/227 , G10L2021/02166
摘要： A system includes a speech recognition processor, a depth sensor coupled to the speech recognition processor, and an array of microphones coupled to the speech recognition processor. The depth sensor is operable to calculate a distance and a direction from the array of microphones to a source of audio data. The speech recognition processor is operable to select an acoustic model as a function of the distance and the direction from the array of microphones to the source of audio data. The speech recognition processor is operable to apply the distance measure in the microphone array beam formation so as to boost portions of the signals originating from the source of audio data and to suppress portions of the signals resulting from noise.
摘要翻译： 系统包括语音识别处理器，耦合到语音识别处理器的深度传感器以及耦合到语音识别处理器的麦克风阵列。 深度传感器可操作以计算从麦克风阵列到音频数据源的距离和方向。 语音识别处理器可操作以根据从麦克风阵列到音频数据源的距离和方向来选择声学模型。 语音识别处理器可操作以将麦克风阵列波束形成中的距离测量应用于升高来自音频数据源的信号的部分，并抑制由噪声引起的信号的部分。
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