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    Systems and methods for dynamic readouts for primary flight displays
    1.
    发明授权
    Systems and methods for dynamic readouts for primary flight displays 有权

    公开(公告)号：US10883851B2

    公开(公告)日：2021-01-05

    申请号：US16132934

    申请日：2018-09-17

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Thea L. Feyereisen ,  Gang He

    IPC: G01C23/00 ,  B64D43/02

    Abstract: Improved systems and methods for dynamic readouts on a primary flight display are provided. The system includes a computer system configured to receive and process aircraft status data and flight plan data to command a display system to overlay on the image, (i) an analog indicator of the airspeed, (ii) an analog indicator of altitude, (iii) a digital airspeed indicator, and (iv) a digital altitude indicator. The system continuously determines whether steady flight conditions are occurring. Steady flight conditions include one or both of: constant airspeed and constant rate of change of airspeed. When the steady flight conditions are occurring, (i) and (ii) are removed from the image. When the steady flight conditions are no longer occurring, (i) and (ii) again overlaid on the image.

    Water encoding for vision systems
    2.
    发明授权
    Water encoding for vision systems 有权

    公开(公告)号：US10794725B2

    公开(公告)日：2020-10-06

    申请号：US15861865

    申请日：2018-01-04

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Gang He ,  Thea L. Feyereisen

    IPC: G01C23/00 ,  G01C21/16 ,  G09B29/00 ,  G09B29/10 ,  G01S19/42 ,  G08B5/02 ,  G02B27/01 ,  G08G5/02

    Abstract: Technologically improved vision systems and methods that provide enhanced water encoding are provided. The vision system receives terrain data from a terrain database and aircraft state data from a navigation system. The vision system commands a display system to display a map image that is reflective of a view from a current location of the platform. The vision system processes terrain data and aircraft state data to identify a water feature, determine a distance between the platform and the water feature, and determine a textural representation for the water feature. The textural representation comprises a symbol and an associated symbol pattern. The vision system commands a display system to overlay, on the map image, the water feature with the textural representation.

    WATER ENCODING FOR VISION SYSTEMS
    3.
    发明申请
    WATER ENCODING FOR VISION SYSTEMS 审中-公开

    公开(公告)号：US20190204113A1

    公开(公告)日：2019-07-04

    申请号：US15861865

    申请日：2018-01-04

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Gang He ,  Thea L. Feyereisen

    IPC: G01C23/00 ,  G01C21/16

    Abstract: Technologically improved vision systems and methods that provide enhanced water encoding are provided. The vision system receives terrain data from a terrain database and aircraft state data from a navigation system. The vision system commands a display system to display a map image that is reflective of a view from a current location of the platform. The vision system processes terrain data and aircraft state data to identify a water feature, determine a distance between the platform and the water feature, and determine a textural representation for the water feature. The textural representation comprises a symbol and an associated symbol pattern. The vision system commands a display system to overlay, on the map image, the water feature with the textural representation.

    SYSTEMS AND METHODS FOR DESTINATION SELECTION FOR VEHICLE INDICATIONS AND ALERTS
    4.
    发明申请
    SYSTEMS AND METHODS FOR DESTINATION SELECTION FOR VEHICLE INDICATIONS AND ALERTS 有权
    用于车辆指示和警报的目的地选择的系统和方法

    公开(公告)号：US20170053539A1

    公开(公告)日：2017-02-23

    申请号：US14831032

    申请日：2015-08-20

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Thea L. Feyereisen ,  Steve Johnson ,  Gang He ,  Yasuo Ishihara ,  Ivan Sandy Wyatt

    IPC: G08G5/02 ,  G08G5/00

    CPC classification number: G08G5/025 ,  G08G5/0021

    Abstract: A method for providing alerts or indications to an aircrew of an aircraft that is in-flight and approaching a destination airport includes receiving an aircrew runway selection from the aircrew of the aircraft, automatically generating a probable runway selection by the aircraft, and determining a position of the in-flight aircraft with reference to a threshold point. If the aircraft is prior to the threshold point, the method includes generating alerts and indications to the aircrew based solely on the received runway selection into the FMS from the aircrew of the aircraft and not on the automatically-generated probable runway selection from the aircraft. Alternatively, if the aircraft is past the threshold point, the method includes generating alerts and indications to the aircrew based solely on the automatically-generated probable runway selection from the aircraft and not on the received runway selection into the FMS from the aircrew of the aircraft.

    Abstract translation: 用于向飞行中和接近目的地机场的飞机的机组人员提供警报或指示的方法包括从飞行器的机组人员接收机组跑道选择，自动产生飞行器可能的跑道选择，以及确定位置 参考一个临界点。 如果飞行器在阈值点之前，则该方法仅仅基于从飞机的机组人员接收的进入FMS的跑道选择而不是从飞行器自动生成的可能的跑道选择来向机组人员生成警报和指示。 或者，如果飞行器超过阈值点，则该方法包括仅基于从飞行器自动生成的可能的跑道选择而不是在从飞机的机组人员接收的进入FMS的跑道选择中产生对机组人员的警报和指示 。

    Aircraft flight deck displays and systems and methods for enhanced display of obstacles in a combined vision display
    6.
    发明授权
    Aircraft flight deck displays and systems and methods for enhanced display of obstacles in a combined vision display 有权
    飞机驾驶舱显示器和用于增强在组合视觉显示中显示障碍物的系统和方法

    公开(公告)号：US09390559B2

    公开(公告)日：2016-07-12

    申请号：US13797730

    申请日：2013-03-12

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Thea L. Feyereisen ,  Gang He ,  John G. Suddreth ,  Patricia May Ververs

    IPC: G09G5/00 ,  G06T19/00 ,  G01C23/00 ,  B64D45/00

    CPC classification number: G06T19/00 ,  B64D45/00 ,  G01C23/005 ,  Y02B10/30

    Abstract: Systems and methods for enhanced display of obstacles in a combined vision display are provided. The system comprises a display unit and an enhanced vision system configured to generate first signals representative of enhanced vision images. Data storage device contains obstacle data representative of obstacles. Synthetic vision system is configured to selectively retrieve obstacle data from data storage device and generate second signals representative of synthetic vision images of one or more obstacles. Processor is in operable communication with display unit and coupled to receive first and second signals and configured, in response thereto, to: overlay the synthetic vision images of the one or more obstacles over the enhanced vision images and command display unit to display the synthetic vision images of the one or more obstacles overlaid over the enhanced vision images. The overlaid synthetic vision images of the one or more obstacles may be visually highlighted.

    Abstract translation: 提供了用于在组合视觉显示中增强显示障碍物的系统和方法。 该系统包括显示单元和被配置为生成表示增强视觉图像的第一信号的增强视觉系统。 数据存储装置包含代表障碍物的障碍物数据。 合成视觉系统被配置为从数据存储装置选择性地检索障碍物数据，并产生代表一个或多个障碍物的合成视觉图像的第二信号。 处理器与显示单元可操作地通信并被耦合以接收第一和第二信号，并且响应于此配置：将增强的视觉图像和命令显示单元上的一个或多个障碍物的合成视觉图像叠加以显示合成视觉 覆盖在增强视觉图像上的一个或多个障碍物的图像。 一个或多个障碍物的重叠的合成视觉图像可以被视觉上突出显示。

    SYSTEM AND METHOD FOR DISPLAYING RUNWAY APPROACH INFORMATION
    7.
    发明申请
    SYSTEM AND METHOD FOR DISPLAYING RUNWAY APPROACH INFORMATION 有权
    显示运行方式信息的系统和方法

    公开(公告)号：US20160090193A1

    公开(公告)日：2016-03-31

    申请号：US14497565

    申请日：2014-09-26

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Gang He ,  Steve Johnson ,  Thea L. Feyereisen

    IPC: B64D45/04 ,  G08G5/02

    CPC classification number: B64D45/04 ,  G08G5/0021 ,  G08G5/025

    Abstract: A system and method are disclosed for indicating to an aircrew of an aircraft an unstable approach to a desired landing. When the energy state of the aircraft exceeds a threshold, a suggested airspeed in consideration of the energy state is displayed. Additionally, a landing spots on a displayed runway are shown indicating where the aircraft would land in view of the energy state and where the aircraft is recommended to land in view of the current aircraft type and weight. A text message may also be displayed that conveys the ability of the aircraft to land.

    Abstract translation: 公开了一种系统和方法，用于向飞机的机组人员指示对期望着陆的不稳定方法。 当飞行器的能量状态超过阈值时，显示考虑能量状态的建议空速。 另外，显示的跑道上的着陆点被示出表明飞机将考虑到能量状态而降落在哪里，并且考虑到目前的飞机类型和重量，飞机被推荐降落在哪里。 还可以显示一条传达航空器着陆能力的短信。

    METHOD AND APPARATUS FOR GENERATING A VIRTUAL INNER MARKER FOR AN AIRCRAFT LANDING APPROACH
    9.
    发明申请
    METHOD AND APPARATUS FOR GENERATING A VIRTUAL INNER MARKER FOR AN AIRCRAFT LANDING APPROACH 有权
    用于生成虚拟内标用于航空器接地方法的方法和装置

    公开(公告)号：US20140222257A1

    公开(公告)日：2014-08-07

    申请号：US13759408

    申请日：2013-02-05

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Ivan Sandy Wyatt ,  Gang He ,  Thea L. Feyereisen

    IPC: B64D45/08

    CPC classification number: B64D45/08 ,  G08G5/0021 ,  G08G5/02 ,  G08G5/025

    Abstract: A system and method is disclosed for anticipating a missed approach point (MAP) during an instrument landing of an aircraft. Symbology is generated and displayed that graphically represents a lateral distance between a runway threshold and a virtual inner marker. The MAP is identified as the location of the aircraft when the symbology reaches a displayed runway threshold.

    Abstract translation: 公开了一种用于在飞机的仪表着陆期间预期错过的接近点（MAP）的系统和方法。 生成和显示符号学，其以图形方式表示跑道阈值和虚拟内标记之间的横向距离。 当符号系统达到显示的跑道阈值时，MAP被标识为飞机的位置。

    Systems and methods for associating critical flight reference data with a flight path vector symbol
    10.
    发明授权
    Systems and methods for associating critical flight reference data with a flight path vector symbol 有权

    公开(公告)号：US10957207B2

    公开(公告)日：2021-03-23

    申请号：US16143789

    申请日：2018-09-27

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Thea L. Feyereisen ,  Gang He

    IPC: G07C1/10 ,  G08G5/00 ,  B64D43/02 ,  G07C5/00

    Abstract: Systems and methods for associating critical flight reference data with a flight path vector symbol are provided. The system displays a continuously updated image with a symbol for a flight path vector. The system displays a first readout arrangement, in which the airspeed indicator and the altitude indicator are (i) each located in relationship to boundary edges of the display device, and (ii) their locations are substantially static. The system detects a deviation between the flight path vector and the heading, and when the deviation exceeds a threshold, the system toggles to a second readout arrangement, in which the airspeed indicator and the altitude indicator are (i) each located a distance measured from the flight path vector, and (ii) dynamically change location responsive to movement of the flight path vector.

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