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公开(公告)号：US08798815B1
公开(公告)日：2014-08-05
申请号：US13800017
申请日：2013-03-13
Applicant: Honeywell International Inc.
Inventor： Roger W. Burgin , Dave Pepitone , Jerry Ball , Pramod Kumar Malviya
CPC classification number: B64D45/00 , G08G5/0021 , G08G5/0052
Abstract: A system and method display general terrain clearance awareness, whether the aircraft is off route, on airway, off procedure, or on procedure, so altitude thresholds are not violated and EGPWS alerts are avoided, while reducing clutter in displaying the information. Altitude, location, and rate of change in altitude are considered in determining whether the aircraft will exceed the threshold altitude. A flight path or an area to be entered is highlighted when the threshold altitude will be violated by the aircraft with the current flight path. The threshold altitude may be a minimum or maximum allowed altitude, or the terrain.
Abstract translation: 系统和方法显示一般的地形清除意识，飞机是否在路线，气道，关闭程序或程序上，因此不会违反高度阈值，避免EGPWS警报，同时减少显示信息的杂乱。 在确定飞机是否超过阈值高度时，会考虑高度，位置和高度变化率。 飞行路线或要输入的区域突出显示，当航空器的当前飞行路径违反阈值高度时。 阈值高度可以是最小或最大允许的高度或地形。
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公开(公告)号：US11307051B2
公开(公告)日：2022-04-19
申请号：US16426764
申请日：2019-05-30
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Thea Feyereisen , Rakshit Ramakrishna , Gang He , Pramod Kumar Malviya , Rui Wang
Abstract: A system and method for operating a dynamic vertical situation display on an aircraft includes generating display data for a dynamic vertical situation display displayed on a display based upon flight plan data from a flight management system, where the flight plan data includes a plurality of waypoints and one or more phases of flight. A current phase of flight of the aircraft and a number of waypoints currenting displayed on the dynamic vertical situation display on the display is determined, and instructions to dynamically change a size of the dynamic vertical situation display on the display are generated based upon at least one of the number of waypoints currenting displayed on the display and the current phase of flight of the aircraft.
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公开(公告)号：US20180158343A1
公开(公告)日：2018-06-07
申请号：US15370029
申请日：2016-12-06
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Pramod Kumar Malviya , Pradeep Huncha , Vinay Somashekar , Sreenivasan Govindillam K , Nathan K , Anoop S , Sunitha Panchangam
CPC classification number: G08G5/0034 , B64D43/00 , B64D45/08 , G01C21/00 , G01C21/20 , G01C23/005 , G08G5/0021 , G08G5/0052 , G08G5/025
Abstract: Systems and methods are provided for displaying portions of a route on a coverage map that are non-compliant for a Global Navigation Satellite System (GNSS) navigation system in an aircraft. A route compliance module defines a geodetic reference datum standard based on the GNSS navigation system. A navigation system database has compliance information corresponding to each of a plurality of airports. A flight management system determines the route of the aircraft and a visual display displays the route and the coverage map. The route compliance module identifies a non-compliant region of the coverage map that is not compliant with the geodetic reference datum standard based on the compliance information and adjusts the visual display to differentiate a non-compliant portion of the route extending within the non-compliant region of the coverage map.
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公开(公告)号：US20200378790A1
公开(公告)日：2020-12-03
申请号：US16426764
申请日：2019-05-30
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Thea Feyereisen , Rakshit Ramakrishna , Gang He , Pramod Kumar Malviya , Rui Wang
Abstract: A system and method for operating a dynamic vertical situation display on an aircraft includes generating display data for a dynamic vertical situation display displayed on a display based upon flight plan data from a flight management system, where the flight plan data includes a plurality of waypoints and one or more phases of flight. A current phase of flight of the aircraft and a number of waypoints currenting displayed on the dynamic vertical situation display on the display is determined, and instructions to dynamically change a size of the dynamic vertical situation display on the display are generated based upon at least one of the number of waypoints currenting displayed on the display and the current phase of flight of the aircraft.
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5.发明申请公开(公告)号：US20160217693A1
公开(公告)日：2016-07-28
申请号：US14606337
申请日：2015-01-27
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Subash Samuthirapandian , Markus Alan Johnson , Pramod Kumar Malviya , Jayasenthilnathan B , Bretislav Passinger
CPC classification number: G08G5/0021 , G01C23/00 , G08G5/0013 , G08G5/003 , G08G5/0039 , G08G5/06
Abstract: A flight display system or method in accordance with this disclosure involves the presentation, on an aircraft, of a “quick preview” notice to airmen (“NOTAM”) display that includes a plurality of stacked flight route portion boxes, each of the plurality of flight route portion boxes pertaining to and being labeled as one of: a departure taxiing portion, a standard instrument departure portion, an en route portion, a standard terminal arrival route portion, an approach portion, and an arrival taxiing portion; each of the plurality of flight route portion boxes graphically displaying flight route symbology pertaining to and labeled as each airport taxiing reference point and/or each aeronautical waypoint that falls within its labeled flight route portion; and wherein at least one of the plurality of flight route portion boxes further graphically displays NOTAM symbology pertaining to at least one of the NOTAMs that are relevant to the flight route.
Abstract translation: 根据本公开的飞行显示系统或方法涉及在飞行器上呈现包括多个堆叠飞行路线部分框的飞行员（“NOTAM”）显示器的“快速预览”通知， 飞行路线部分框属于以下之一，并被标记为以下之一：起跑滑行部分，标准仪表离开部分，途中部分，标准终点站到达路线部分，接近部分和到达滑行部分; 多个飞行路线部分框中的每一个图形地显示属于并标记为每个机场滑行参考点的飞行路线符号系和/或落在其标记的飞行路线部分内的每个航空航路点; 并且其中所述多个飞行路线部分框中的至少一个进一步图形地显示与与所述飞行路线相关的至少一个所述NOTAM有关的NOTAM符号系统。
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Patent Agency Ranking
公开(公告)号：US11347463B2
公开(公告)日：2022-05-31
申请号：US16458890
申请日：2019-07-01
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Thea Feyereisen , Rakshit Ramakrishna , Pramod Kumar Malviya , Bryan Weaver , Brock Graham , Gang He , Emmanuel Letsu-Dake , Rui Wang , Subash Samuthirapandian
Abstract: A system and method of operating a correlative display system for a plurality of display systems on an aircraft includes receiving, by a processor, an identification of a feature from a user interface associated with a first display system of the plurality of display systems. The processor determines a location of the identified feature relative to data displayed on each other display system of the plurality of display systems, wherein the identified feature is not previously displayed on at least one of the other display systems of the plurality of display systems. The processor generates instructions to highlight the identified feature on each other display system of the plurality of display systems at the determine location relative to data displayed on each other display system.
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公开(公告)号：US10997769B2
公开(公告)日：2021-05-04
申请号：US16525087
申请日：2019-07-29
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Pramod Kumar Malviya , Thea Feyereisen , Gang He , Rui Wang
Abstract: Methods and systems are provided for generating an animated display for an aircraft. The method comprises receiving a user request for a change in a layer shown on a display that shows a view of the flight plan data for the aircraft. The user request is received by a user interface (UI) that is part of a map layer display system located onboard the aircraft. The system determines which specific layer corresponds to user request for a change to the display. When the user request is to add the layer to the display, the opaqueness of the layer increases from zero percent to one-hundred percent. When the user request is to remove the layer from the display, the opaqueness of the layer decreases from one-hundred percent to zero percent. Finally, the system generates instructions to display the layer at the opaqueness on the display.
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8.发明授权Methods and systems for displaying procedure information on an aircraft display 有权用于在飞行器显示器上显示程序信息的方法和系统公开(公告)号：US09020664B2
公开(公告)日：2015-04-28
申请号：US13862633
申请日：2013-04-15
Applicant: Honeywell International Inc.
Inventor： Roger W. Burgin , Pramod Kumar Malviya , Dave Pepitone , Jerry Ball
CPC classification number: B64D45/00 , G08G5/0021 , G08G5/0039 , G08G5/0078 , G08G5/0086 , G08G5/0091 , G08G5/025
Abstract: A method for displaying a flight path navigational procedure includes, but is not limited to, detecting with a position detecting system a current location of the aircraft, obtaining from an electronic storage device a plurality of flight path navigation procedures available for a geographic location, determining with a flight path analysis system a preferred flight path that will be taken by the aircraft, and displaying on a display unit a moving map corresponding with the current location of the aircraft and further displaying a depiction of the plurality of flight path navigation procedures on the moving map. The preferred flight path is displayed with a visual cue that visually differentiates the preferred flight path from the other flight paths of the plurality of flight path navigation procedures.
Abstract translation: 用于显示飞行路径导航过程的方法包括但不限于用位置检测系统检测飞行器的当前位置，从电子存储设备获得可用于地理位置的多个飞行航路导航程序，确定 飞行路径分析系统将由飞行器采用的优选飞行路径，并且在显示单元上显示与飞行器的当前位置相对应的移动地图，并且进一步显示对飞行路线导航程序的描绘 移动地图。 优选的飞行路径以视觉提示显示，其视觉上区分了多个飞行航路导航程序中的其他飞行路径的首选飞行路径。
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9.发明申请METHODS AND SYSTEMS FOR SELECTING A DISPLAYED AIRCRAFT APPROACH OR DEPARTURE 有权用于选择显示的飞行方法或出发的方法和系统公开(公告)号：US20140337796A1
公开(公告)日：2014-11-13
申请号：US13889493
申请日：2013-05-08
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Roger W. Burgin , Pramod Kumar Malviya , Dave Pepitone , Keith Hughes
IPC: G06F3/0484
CPC classification number: G06F3/04842 , G01C23/00
Abstract: A system and method are provided for highlighting and selecting one of a plurality of graphical IFR procedure depiction on an aircraft display. A displayed legend includes a plurality of textual procedure identifications, one each for each of the graphical IFR procedure depictions. Movement of a cursor over either a graphical IFR procedure depiction or a textual procedure identification highlights both, and selection thereof removes all other graphical IFR procedure depictions and textual procedure identifications from being displayed.
Abstract translation: 提供了一种用于在飞行器显示器上突出显示和选择多个图形IFR程序描绘中的一个的系统和方法。 显示的图例包括多个文本过程标识，每个用于图形IFR程序描述中的每一个。 光标在图形IFR程序描述或文本过程标识上的移动突出显示，并且其选择移除所有其他图形IFR过程描述和文本过程标识以被显示。
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10.发明申请SYSTEM AND METHOD FOR DISPLAYING TERRAIN ALTITUDES ON AN AIRCRAFT DISPLAY 审中-公开用于在飞机显示器上显示海带高度的系统和方法公开(公告)号：US20140222327A1
公开(公告)日：2014-08-07
申请号：US13758040
申请日：2013-02-04
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Roger W. Burgin , Pramod Kumar Malviya , Dave Pepitone
IPC: G08G5/00
CPC classification number: G08G5/0047 , G01C23/00
Abstract: A system and method are provided for displaying terrain altitudes on an aircraft display that are easily understood by the pilot. A plurality of bands are defined, wherein each band defines a range of altitudes of terrain in the vicinity of the aircraft. A list of altitudes representing each band is displayed in a legend. A band is highlighted when a number associated therewith is selected, and a number is highlighted when the band associated therewith is selected. The band or number may be selected, for example, by cursor, or the band may be selected by position of the aircraft.
Abstract translation: 提供了一种用于在飞行器显示器上显示飞行员容易理解的地形高度的系统和方法。 定义了多个频带，其中每个频带限定飞机附近的地形高度范围。 表示每个频带的高度列表显示在图例中。 当与其相关联的数字被选择时，频带被突出显示，并且当选择与其相关联的频带时，数字被突出显示。 可以例如通过光标来选择频带或数字，或者可以通过飞行器的位置来选择频带。
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