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31.发明申请公开(公告)号：US20190137326A1
公开(公告)日：2019-05-09
申请号：US16235923
申请日：2018-12-28
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： John G. Suddreth , Marisela Mendez Tapia , Jerry Ball , Mark Giddings
Abstract: Avionic display systems and methods are provided for generating avionic displays, which include symbology and other graphics pertaining to forecast overpressure events, which are forecast to occur during supersonic aircraft flight. In various embodiments, the avionic display system includes a display device on which an avionic display is produced. A controller architecture is operably coupled to the display device. Storage media contains computer-readable code or instructions that, when executed by the controller architecture, cause the avionic display system to determine whether an overpressure event is forecast to occur due to the predicted future occurrence of a sonic boom, which has a magnitude exceeding a boom tolerance threshold. When the controller architecture determines that an overpressure event is forecast to occur, the avionic display system further generates symbology on the avionic display indicative of or visually signifying the forecast overpressure event.
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公开(公告)号：US09864194B2
公开(公告)日：2018-01-09
申请号：US14950245
申请日：2015-11-24
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Subash Samuthirapandian , John G. Suddreth
CPC classification number: G02B27/0101 , G02B27/0093 , G02B27/01 , G02B27/017 , G02B27/0179 , G02B2027/0141 , G02B2027/0181 , G02B2027/0183 , G02B2027/0187 , G06F3/013
Abstract: A visual display system is provided for a vehicle having a windshield. The system includes a controller configured to receive information associated with an operating environment of the vehicle and to generate display commands representing the operating environment; a first operator tracking unit configured to collect data associated with a primary vision field of view of an operator; and a first display system coupled to the controller and configured to receive the display commands. The first display system includes a first display unit configured to display at least a portion of a border representing a boundary of the primary vision field of view of the operator and first symbology representing the operating environment of the vehicle.
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公开(公告)号：US09666085B2
公开(公告)日：2017-05-30
申请号：US14541649
申请日：2014-11-14
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Aaron Gannon , Thea L. Feyereisen , Troy Nichols , Jerry Ball , Sean Caufield , John G. Suddreth , Ivan Sandy Wyatt
CPC classification number: G08G5/065 , B60K35/00 , G08G5/0021
Abstract: Methods and systems are provided for displaying a taxi clearance for an aircraft at an airport. One exemplary method involves receiving user input indicative of a constraining taxi path of a plurality of taxi paths at the airport, determining a first taxi portion between an initial location for the taxi clearance and the constraining taxi path, determining a second taxi portion between the constraining taxi path and a destination location for the taxi clearance, and displaying, on a display device associated with the aircraft, a taxi route comprising the first taxi portion, the second taxi portion, and the constraining taxi path between the first taxi portion and the second taxi portion.
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Patent Agency Ranking
公开(公告)号：US09594248B2
公开(公告)日：2017-03-14
申请号：US13858739
申请日：2013-04-08
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Brent D. Larson , John G. Suddreth , Frank Cupero
CPC classification number: G02B27/017 , G02B2027/0118 , G02B2027/014 , G02B2027/0187 , G06F3/012 , G06F3/013 , G09G2380/12
Abstract: Methods and systems for operating a vehicular near-to-eye (NTE) display screen operable within an operational range limit are provided. An image is rendering on the NTE display screen within a predefined visibility range. The predefined visibility range is within the operational range limit. A luminance of at least a portion of the image is reduced in response to the NTE display screen being moved outside of the predefined visibility range and within the operational range limit.
Abstract translation: 提供了用于在可操作范围限制内操作的车辆近视（NTE）显示屏的操作方法和系统。 图像在NTE显示屏幕上呈现在预定义的可见范围内。 预定义的可见范围在操作范围内。 响应于NTE显示屏幕移动到预定的可视范围之外并且在操作范围限度内，图像的至少一部分的亮度被减小。
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35.发明申请SYSTEM AND DISPLAY ELEMENT FOR DISPLAYING WAYPOINT MARKERS WITH INTEGRATED ALTITUDE CONSTRAINT INFORMATION 审中-公开用于显示具有集成高度约束信息的方位标记的系统和显示元件公开(公告)号：US20160138936A1
公开(公告)日：2016-05-19
申请号：US15002579
申请日：2016-01-21
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Gang He , John G. Suddreth , Thea L. Feyereisen
CPC classification number: G01C23/005 , G01C21/00 , G01C23/00 , G06T7/70 , G06T11/20 , G06T19/003 , G08G5/0021
Abstract: A flight deck display system for an aircraft includes a processor architecture configured to receive aircraft instrument data, waypoint restriction information, and position data for the aircraft and, based upon the received data, generate image rendering display commands. The system also includes a display element configured to receive the image rendering display commands and, in response thereto, to render a display that includes a perspective view of terrain and at least one waypoint marker corresponding to an approaching waypoint. The waypoint marker includes visually distinguishable characteristics that convey waypoint restriction information (e.g., altitude or airspeed constraint information that governs the waypoint).
Abstract translation: 用于飞行器的飞行甲板显示系统包括被配置为接收飞行器仪表数据，航路点限制信息和飞机的位置数据的处理器架构，并且基于接收的数据生成图像渲染显示命令。 该系统还包括被配置为接收图像呈现显示命令的显示元件，并且响应于此，呈现包括地形的透视图和至少一个对应于接近航点的航路点标记的显示。 航路点标记包括传达路点限制信息（例如，管理航点的高度或空速约束信息）的视觉上可区分的特征。
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36.发明授权System and display element for displaying waypoint markers with integrated altitude constraint information 有权用于显示具有综合高度约束信息的航点标记的系统和显示元件公开(公告)号：US09273964B2
公开(公告)日：2016-03-01
申请号：US14077266
申请日：2013-11-12
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Gang He , John G. Suddreth , Thea L. Feyereisen
CPC classification number: G01C23/005 , G01C21/00 , G01C23/00 , G06T7/70 , G06T11/20 , G06T19/003 , G08G5/0021
Abstract: A flight deck display system for an aircraft includes a processor architecture configured to receive aircraft instrument data, waypoint restriction information, and position data for the aircraft and, based upon the received data, generate image rendering display commands. The system also includes a display element configured to receive the image rendering display commands and, in response thereto, to render a display that includes a perspective view of terrain and at least one waypoint marker corresponding to an approaching waypoint. The waypoint marker includes visually distinguishable characteristics that convey waypoint restriction information (e.g., altitude or airspeed constraint information that governs the waypoint).
Abstract translation: 用于飞行器的飞行甲板显示系统包括被配置为接收飞行器仪表数据，航路点限制信息和飞机的位置数据的处理器架构，并且基于接收的数据生成图像渲染显示命令。 该系统还包括被配置为接收图像呈现显示命令的显示元件，并且响应于此，呈现包括地形的透视图和至少一个对应于接近航点的航路点标记的显示。 航路点标记包括传达路点限制信息（例如，管理航点的高度或空速约束信息）的视觉上可区分的特征。
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公开(公告)号：US20150371545A1
公开(公告)日：2015-12-24
申请号：US14840908
申请日：2015-08-31
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Aaron Gannon , Ivan Sandy Wyatt , Troy Nichols , John G. Suddreth
IPC: G08G5/02
CPC classification number: G08G5/025 , G08G5/0021 , G08G5/0047
Abstract: A dynamic runway indicator is displayed overlying a conformal runway for assisting a pilot in completing an approach to landing on a runway. The dynamic runway indicator includes a polygon, that by changing position with respect to the conformal runway, provides advanced instrumentation cues to the pilot for adjusting the aircraft flight path to a normal, or recommended, path to the runway for landing, thereby assisting the pilot to improve the accuracy and safety of the approach and landing.
Abstract translation: 一个动态跑道指示器显示在一个保形跑道上，以协助飞行员完成在跑道上着陆的方法。 动态跑道指示器包括多边形，其通过相对于保形跑道改变位置，向飞行员提供高级仪表线索，用于调整飞行器飞行路径到达跑道的正常或推荐路径以降落，从而辅助飞行员 提高进场和落地的准确性和安全性。
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38.发明申请SYSTEM AND DISPLAY ELEMENT FOR DISPLAYING WAYPOINT MARKERS WITH INTEGRATED ALTITUDE CONSTRAINT INFORMATION 审中-公开用于显示具有集成高度约束信息的方位标记的系统和显示元件公开(公告)号：US20140058675A1
公开(公告)日：2014-02-27
申请号：US14077266
申请日：2013-11-12
Applicant: Honeywell International Inc.
Inventor： Gang He , John G. Suddreth , Thea L. Feyereisen
IPC: G01C21/00
CPC classification number: G01C23/005 , G01C21/00 , G01C23/00 , G06T7/70 , G06T11/20 , G06T19/003 , G08G5/0021
Abstract: A flight deck display system for an aircraft includes a processor architecture configured to receive aircraft instrument data, waypoint restriction information, and position data for the aircraft and, based upon the received data, generate image rendering display commands. The system also includes a display element configured to receive the image rendering display commands and, in response thereto, to render a display that includes a perspective view of terrain and at least one waypoint marker corresponding to an approaching waypoint. The waypoint marker includes visually distinguishable characteristics that convey waypoint restriction information (e.g., altitude or airspeed constraint information that governs the waypoint).
Abstract translation: 用于飞行器的飞行甲板显示系统包括被配置为接收飞行器仪表数据，航路点限制信息和飞机的位置数据的处理器架构，并且基于接收的数据生成图像渲染显示命令。 该系统还包括被配置为接收图像呈现显示命令的显示元件，并且响应于此，呈现包括地形的透视图和至少一个对应于接近航点的航路点标记的显示。 航路点标记包括传达路点限制信息（例如，管理航点的高度或空速约束信息）的视觉上可区分的特征。
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