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    Systems and methods for for presenting an RTA waypoint with associated time constraints
    1.
    发明授权
    Systems and methods for for presenting an RTA waypoint with associated time constraints 有权

    公开(公告)号：US11676497B2

    公开(公告)日：2023-06-13

    申请号：US17207010

    申请日：2021-03-19

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Subash Samuthirapandian ,  Thea Feyereisen

    IPC: G08G5/00

    CPC classification number: G08G5/0047 ,  G08G5/0004 ,  G08G5/0021 ,  G08G5/0034

    Abstract: Systems and methods for presenting an RTA waypoint with associated time constraints. The system includes a flight management system (FMS) providing an assigned flight plan with a plurality of waypoints; a display device configured to render a current location and trajectory of the aircraft in a navigation display and in a vertical display; and a controller circuit. The system locates the RTA waypoint among the plurality of waypoints, as a function of the flight plan and the current location and trajectory of the aircraft. The system identifies a time constraint associated with the RTA waypoint. The system uses the time constraint to determine a type, from among an “at”, a “before”, and an “after”, for the RTA waypoint; and, assigns a preprogrammed visual encoding scheme for the type to the RTA waypoint. The system presents the RTA waypoint, using the visual encoding scheme, on the display device.

    SYSTEMS AND METHODS FOR PROVIDING LOCATION INFORMATION FOR A USER-SELECTED FEATURE ON AN ACTIVE VERTICAL SITUATION DISPLAY (VSD)
    3.
    发明申请
    SYSTEMS AND METHODS FOR PROVIDING LOCATION INFORMATION FOR A USER-SELECTED FEATURE ON AN ACTIVE VERTICAL SITUATION DISPLAY (VSD) 有权

    公开(公告)号：US20220144445A1

    公开(公告)日：2022-05-12

    申请号：US17138311

    申请日：2020-12-30

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Subash Samuthirapandian ,  Ivan Wyatt

    IPC: B64D43/00 ,  G06F3/0482 ,  G08G5/00 ,  G01C21/20

    Abstract: Methods and systems for providing location information for a user-selected feature on an active vertical situation display (VSD) in a cockpit of an aircraft. The method includes rendering the VSD having a plurality of terrain and weather features; receiving, from a user interface, the user-selected feature from among the plurality of features on the VSD, the plurality of features including terrain features and weather features; causing a reticle to be displayed as an overlay, centered, on the user-selected feature on the VSD, responsive to receiving the user-selected feature; rendering a horizontal extension from a center of the reticle to an intersection on a vertical axis of the VSD, and a vertical extension from the center of the reticle to an intersection on a horizontal axis of the VSD. An elevation label and a distance label are positioned on the respective extensions.

    FLIGHT DECK DISPLAY SYSTEMS AND METHODS FOR GENERATING IN-TRAIL PROCEDURE WINDOWS INCLUDING AIRCRAFT FLIGHT PATH SYMBOLOGY
    4.
    发明申请
    FLIGHT DECK DISPLAY SYSTEMS AND METHODS FOR GENERATING IN-TRAIL PROCEDURE WINDOWS INCLUDING AIRCRAFT FLIGHT PATH SYMBOLOGY 有权
    飞行装甲显示系统和用于生成包括航空飞行轨迹符号在内的行程窗口的方法

    公开(公告)号：US20140210648A1

    公开(公告)日：2014-07-31

    申请号：US13752782

    申请日：2013-01-29

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Subash Samuthirapandian ,  Fazurudheen A ,  Markus Johnson

    IPC: G08G5/00

    CPC classification number: G08G5/0008 ,  G08G5/0021 ,  G08G5/0078

    Abstract: Embodiments of a flight deck display system for deployment onboard a host aircraft are provided, as are embodiments of a method carried-out by a flight deck display system. In one embodiment, the flight deck display system includes a cockpit display, a wireless communication module, and a controller operatively coupled to the cockpit display and to the wireless communication module. The controller is configured to generate a vertical In-Trail Procedure (ITP) window on the cockpit display, which includes graphics representative of the current position of the host aircraft, the current position of an intruder aircraft when present within a predetermined distance of the host aircraft, and a plurality of flight levels. The controller is further configured to receive data from which the current flight path of the intruder aircraft can be derived; and periodically update the vertical ITP window to include flight path symbology indicative of the current flight path of the intruder aircraft.

    Abstract translation: 提供了用于部署在主机上的飞行甲板显示系统的实施例，由飞行甲板显示系统执行的方法的实施例。 在一个实施例中，驾驶舱显示系统包括驾驶舱显示器，无线通信模块和可操作地耦合到驾驶舱显示器和无线通信模块的控制器。 控制器被配置为在驾驶舱显示器上生成垂直行进步骤（ITP）窗口，该窗口包括代表主机飞行器当前位置的图形，当存在于主机的预定距离内时入侵者飞行器的当前位置 飞机和多个飞行高度。 所述控制器还被配置为接收可从其导出入侵者飞行器的当前飞行路径的数据; 并定期更新垂直ITP窗口，以包括指示入侵者飞机当前飞行路径的飞行路线符号系统。

    ELECTRIC TAXI MOTIVE CONTROL SYSTEM AND METHOD OF AN AIRCRAFT
    6.
    发明申请
    ELECTRIC TAXI MOTIVE CONTROL SYSTEM AND METHOD OF AN AIRCRAFT 有权
    电动汽车动力控制系统和飞机方法

    公开(公告)号：US20160117935A1

    公开(公告)日：2016-04-28

    申请号：US14502957

    申请日：2014-09-30

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Subash Samuthirapandian ,  Markus A. Johnson

    IPC: G08G5/04 ,  G08G5/06 ,  B64C25/34 ,  B64C25/40

    CPC classification number: G08G5/04 ,  B64C25/34 ,  B64C25/405 ,  B64D45/00 ,  G08G5/0008 ,  G08G5/0021 ,  G08G5/0078 ,  G08G5/0091 ,  G08G5/045 ,  G08G5/065 ,  Y02T50/823

    Abstract: An electric taxi motive control system of a first aircraft comprises a first aircraft position determining system configured to generate a first aircraft position signal, a first aircraft receiver, configured to receive transmissions of a second aircraft position signal, a first aircraft pilot interface configured to accept an input indicative of a first aircraft desired speed, and a first aircraft electronic controller configured to; determine a aircraft separation distance indicative of the distance between the first aircraft and the second aircraft, compare the aircraft separation distance with a safe distance value; and generate a modified first aircraft commanded speed signal when the aircraft separation distance is less than the safe distance value.

    Abstract translation: 第一飞行器的电动出租车动力控制系统包括被配置为产生第一飞行器位置信号的第一飞行器位置确定系统，被配置为接收第二飞行器位置信号的传输的第一飞行器接收器，被配置为接受的第一飞行器接口 指示第一飞行器期望速度的输入;以及第一飞行器电子控制器，其被配置为： 确定指示第一飞机和第二飞机之间的距离的飞机间隔距离，将飞机间隔距离与安全距离值进行比较; 并且当飞行器分离距离小于安全距离值时，生成修改的第一飞机命令速度信号。

    System and method for graphically displaying aircraft traffic information using aircraft symbology
    7.
    发明授权
    System and method for graphically displaying aircraft traffic information using aircraft symbology 有权
    使用飞机符号表示图形显示飞机交通信息的系统和方法

    公开(公告)号：US09105183B2

    公开(公告)日：2015-08-11

    申请号：US13919572

    申请日：2013-06-17

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Subash Samuthirapandian ,  Markus Alan Johnson ,  Ronald Brian Wayman

    IPC: G08B21/00 ,  G08G5/00

    CPC classification number: G08G5/0004 ,  G08G5/0013 ,  G08G5/0021

    Abstract: Presented herein is a system and method for graphically displaying aircraft traffic information. The system comprises an Operating Company Symbology database and a display system coupled to a processor that is configured to (1) receive traffic information; (2) determine the Operating Company Symbology from the received traffic information; (3) receive a selection of an aircraft or traffic information including at least one of the Flight ID, Operating Company, or Surface Traffic; (4) graphically render aircraft symbology and the associated traffic information on the display.

    Abstract translation: 这里提出的是用于图形地显示飞行器交通信息的系统和方法。 该系统包括操作公司符号学数据库和耦合到处理器的显示系统，其被配置为（1）接收交通信息; （2）从收到的交通信息中确定运营公司符号; （3）接收选择的航空器或交通信息，包括航班编号，运营公司或地面交通中的至少一个; （4）在显示器上以图形方式呈现飞行器符号系统和相关联的交通信息。

    Flight deck display systems and methods for generating in-trail procedure windows including aircraft flight path symbology
    8.
    发明授权
    Flight deck display systems and methods for generating in-trail procedure windows including aircraft flight path symbology 有权
    飞行甲板显示系统和方法，用于产生包括飞行器飞行路径符号系统在内的步进程序窗口

    公开(公告)号：US09070283B2

    公开(公告)日：2015-06-30

    申请号：US13752782

    申请日：2013-01-29

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Subash Samuthirapandian ,  Fazurudheen A ,  Markus Johnson

    IPC: G08G5/04 ,  G08G5/00

    CPC classification number: G08G5/0008 ,  G08G5/0021 ,  G08G5/0078

    Abstract: Embodiments of a flight deck display system for deployment onboard a host aircraft are provided, as are embodiments of a method carried-out by a flight deck display system. In one embodiment, the flight deck display system includes a cockpit display, a wireless communication module, and a controller operatively coupled to the cockpit display and to the wireless communication module. The controller is configured to generate a vertical In-Trail Procedure (ITP) window on the cockpit display, which includes graphics representative of the current position of the host aircraft, the current position of an intruder aircraft when present within a predetermined distance of the host aircraft, and a plurality of flight levels. The controller is further configured to receive data from which the current flight path of the intruder aircraft can be derived; and periodically update the vertical ITP window to include flight path symbology indicative of the current flight path of the intruder aircraft.

    Abstract translation: 提供了用于部署在主机上的飞行甲板显示系统的实施例，由飞行甲板显示系统执行的方法的实施例。 在一个实施例中，驾驶舱显示系统包括驾驶舱显示器，无线通信模块和可操作地耦合到驾驶舱显示器和无线通信模块的控制器。 控制器被配置为在驾驶舱显示器上生成垂直行进步骤（ITP）窗口，该窗口包括代表主机飞行器当前位置的图形，当存在于主机的预定距离内时入侵者飞行器的当前位置 飞机和多个飞行高度。 所述控制器还被配置为接收可从其导出入侵者飞行器的当前飞行路径的数据; 并定期更新垂直ITP窗口，以包括指示入侵者飞机当前飞行路径的飞行路线符号系统。

    METHOD AND SYSTEM FOR GENERATING AN ALERT FOR AN AIRCRAFT POTENTIALLY EXCEEDING SPEED LIMITS IN RESTRICTED AIRSPACE
    10.
    发明申请
    METHOD AND SYSTEM FOR GENERATING AN ALERT FOR AN AIRCRAFT POTENTIALLY EXCEEDING SPEED LIMITS IN RESTRICTED AIRSPACE 审中-公开

    公开(公告)号：US20190291889A1

    公开(公告)日：2019-09-26

    申请号：US15935943

    申请日：2018-03-26

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Thea L. Feyereisen ,  Gang He ,  Jary Engels ,  Subash Samuthirapandian

    IPC: B64D45/00 ,  B64D43/00 ,  G01C23/00 ,  G08G5/00

    Abstract: Methods and systems are provided for generating an alert for an aircraft potentially exceeding speed limits in airspace with speed limitations. The method comprises retrieving a flight plan for the aircraft and identifying airspace with speed limitations along the flight plan. A speed profile is generated based on the in-flight aircraft's current position, speed and trajectory. Any predicted speed violations are identified by comparing the speed profile with the airspace with speed limitations along the flight plan. A predictive time window is calculated that allows for the in-flight aircraft to decelerate sufficiently to comply with the speed limits of the airspace with speed limitations. The predictive time window includes a zone for the aircraft to reduce its airspeed and a reaction buffer zone to allow the aircrew sufficient time to comply with instructions to decelerate the aircraft. Finally, an alert is generated for the crew of the in-flight aircraft upon entering the predictive time window.

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