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    Display systems and methods for providing displays indicating a required time of arrival
    1.
    发明授权
    Display systems and methods for providing displays indicating a required time of arrival 有权
    显示系统和方法，用于提供显示所需的到达时间

    公开(公告)号：US09266621B2

    公开(公告)日：2016-02-23

    申请号：US13964759

    申请日：2013-08-12

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Michal Polansky ,  Jiri Vasek ,  Bretislav Passinger ,  Jiri Svoboda

    IPC: B64D45/00 ,  G01C23/00

    CPC classification number: B64D45/00 ,  G01C23/00

    Abstract: A method for providing a display to a flight crew of an aircraft includes receiving a required time of arrival (RTA) control instruction for arriving at a particular waypoint at a particular time, calculating an initial required aircraft speed at which the aircraft is required to fly in order to arrive at the particular waypoint at the particular time, and providing a flight display comprising a speed tape. The method further includes receiving an input accepting the RTA control instruction and calculating an updated required aircraft speed at which the aircraft is required to fly in order to arrive at the particular waypoint at the particular time. Still further, the method includes updating the flight display comprising displaying the updated RTA target speed on the speed tape using a second symbology that is different from the first symbology and discontinuing the display of the first symbology.

    Abstract translation: 向飞行员的飞行机组提供显示器的方法包括在特定时间接收到达到特定航点的所需时间（RTA）控制指令，计算飞机需要飞行的初始所需飞行器速度 以便在特定时间到达特定的航点，并提供包括速度磁带的飞行显示。 该方法还包括接收接受RTA控制指令并计算飞机需要飞行的更新的所需飞行器速度以便在特定时间到达特定航路点的输入。 此外，该方法包括更新飞行显示，其包括使用与第一符号系统不同的第二符号系统在速度磁带上显示更新的RTA目标速度并停止第一符号系统的显示。

    SYSTEM AND METHOD FOR MANAGING SPEED CONSTRAINTS DURING REQUIRED TIME OF ARRIVAL OPERATIONS
    3.
    发明申请
    SYSTEM AND METHOD FOR MANAGING SPEED CONSTRAINTS DURING REQUIRED TIME OF ARRIVAL OPERATIONS 有权
    在需要运行的时间内管理速度限制的系统和方法

    公开(公告)号：US20160069688A1

    公开(公告)日：2016-03-10

    申请号：US14477476

    申请日：2014-09-04

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Michal Polansky ,  Erwan Paricaud ,  Dorothee De Villele ,  Zdenek Jancik

    IPC: G01C21/00

    CPC classification number: G01C21/00 ,  G05D1/0005 ,  G05D1/0202 ,  G05D1/101 ,  G08G5/00 ,  G08G5/0021 ,  G08G5/0052

    Abstract: A method and apparatus includes strategies for improving required time of arrival reliability by an aircraft comprising determining a speed correction for one of AT speed constraints or an AT or ABOVE speed constraints, wherein the determining is selected from one or more of the mechanisms from the group consisting of continuous RTA speed management between constraints, padding of the AT speed constraints and the AT or ABOVE speed constraints; decelerating proactively; and using a variable guidance margin, wherein the guidance margin is a speed change not reflected in a flight plan prediction.

    Abstract translation: 一种方法和装置包括用于改进飞机所需的到达时间可靠性的策略，包括确定AT速度约束或AT或上述速度约束之一的速度校正，其中所述确定是从所述组中的一个或多个机构中选择的 包括连续的RTA速度管理约束，AT速度限制的填充和AT或ABOVE速度约束; 主动减速 并且使用可变引导边缘，其中所述引导边距是未被反映在飞行计划预测中的速度变化。

    Methods and systems for representing time of arrival information on a cockpit display
    4.
    发明授权
    Methods and systems for representing time of arrival information on a cockpit display 有权
    用于在驾驶舱显示器上表示到达时间信息的方法和系统

    公开(公告)号：US09047763B2

    公开(公告)日：2015-06-02

    申请号：US13843634

    申请日：2013-03-15

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Bretislav Passinger ,  Jiri Vasek ,  Jiri Svoboda ,  Michal Polansky

    IPC: G01C21/12 ,  G06G7/00 ,  G08G5/00 ,  G01C23/00

    CPC classification number: G08G5/0021 ,  G01C23/00 ,  G08G5/0052

    Abstract: A method is provided for displaying information on a display device of an aircraft. The method comprises receiving data indicating a point selected from a trajectory of a flight path; determining an estimated time of arrival minimum and an estimated time of arrival maximum based on the point; and displaying in a dialogue box associated with the trajectory of the flight path the estimated time of arrival minimum and the estimated time of arrival maximum for the point.

    Abstract translation: 提供一种用于在飞行器的显示装置上显示信息的方法。 该方法包括接收指示从飞行路径的轨迹中选择的点的数据; 基于该点确定估计的到达时间最小值和估计到达时间最大值; 并且在与飞行路径的轨迹相关联的对话框中显示估计的到达时间最小值和该点的估计到达时间最大值。

    System and method for determining and displaying optimized aircraft energy level
    5.
    发明授权
    System and method for determining and displaying optimized aircraft energy level 有权

    公开(公告)号：US11113978B2

    公开(公告)日：2021-09-07

    申请号：US15265330

    申请日：2016-09-14

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Dorothee De Villele ,  Erwan Paricaud ,  Daniel Corbel ,  Michal Polansky ,  Zdenek Jancik

    IPC: G08G5/02 ,  B64D43/02 ,  G01C23/00 ,  G08G5/00 ,  B64D45/08

    Abstract: A system and method of displaying optimized aircraft energy level to a flight crew includes processing flight plan data, in a processor, to determine the optimized aircraft energy level along a descent profile of the aircraft from cruise altitude down to aircraft destination, and continuously processing aircraft data, in the processor, to continuously determine, in real-time, an actual aircraft energy level. The actual aircraft energy level of the aircraft is continuously compared, in the processor, to the optimized aircraft energy level. The processor is use to command a display device to render an image that indicates: (i) the optimized aircraft energy level, (ii) how the actual aircraft energy level differs from the optimized aircraft energy level, and (iii) how the actual aircraft energy level is trending relative to the optimized aircraft energy level.

    SPEED-CONSTRAINED FLIGHT MANAGEMENT METHODS AND SYSTEMS
    6.
    发明申请
    SPEED-CONSTRAINED FLIGHT MANAGEMENT METHODS AND SYSTEMS 审中-公开

    公开(公告)号：US20200058226A1

    公开(公告)日：2020-02-20

    申请号：US16453470

    申请日：2019-06-26

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Dorothee De Villele ,  Michal Polansky ,  Marek Batelka ,  Laurent Villacampa

    IPC: G08G5/00 ,  G01C21/14 ,  G01C21/34 ,  G05D1/10 ,  G05D1/06 ,  G01C23/00 ,  G01C21/20 ,  G01C21/00

    Abstract: Systems and methods are provided for managing speed-constrained vehicle operations. One exemplary method of operating an aircraft involves identifying a speed constraint associated with a navigational reference point, determining a speed envelope region en route to the navigational reference point based at least in part on the first speed constraint, identifying a target speed en route to the navigational reference point, and determining a speed profile for autonomously operations en route to the navigational reference point within the speed envelope region. The speed profile intersects the target speed within the speed envelope region and a slope of the speed profile is influenced by the target speed, for example, to effectuate or approximate the target speed by increasing the duration of time operation at or around the target speed is achieved. In one or more embodiments, multiple different target speeds associated with different flight levels or operating regions are accounted for.

    SPEED-CONSTRAINED FLIGHT MANAGEMENT METHODS AND SYSTEMS
    7.
    发明申请
    SPEED-CONSTRAINED FLIGHT MANAGEMENT METHODS AND SYSTEMS 审中-公开

    公开(公告)号：US20190051189A1

    公开(公告)日：2019-02-14

    申请号：US15676003

    申请日：2017-08-14

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Dorothee De Villele ,  Michal Polansky ,  Marek Batelka ,  Laurent Villacampa

    IPC: G08G5/00 ,  G01C21/34 ,  G01C21/14

    CPC classification number: G08G5/0052 ,  G01C21/00 ,  G01C21/14 ,  G01C21/20 ,  G01C21/3492 ,  G01C23/00 ,  G05D1/101 ,  G08G5/0021 ,  G08G5/0034

    Abstract: Systems and methods are provided for managing speed-constrained vehicle operations. One exemplary method of operating an aircraft involves identifying a speed constraint associated with a navigational reference point, determining a speed envelope region en route to the navigational reference point based at least in part on the first speed constraint, identifying a target speed en route to the navigational reference point, and determining a speed profile for autonomously operations en route to the navigational reference point within the speed envelope region. The speed profile intersects the target speed within the speed envelope region and a slope of the speed profile is influenced by the target speed, for example, to effectuate or approximate the target speed by increasing the duration of time operation at or around the target speed is achieved. In one or more embodiments, multiple different target speeds associated with different flight levels or operating regions are accounted for.

    Speed-constrained flight management methods and systems
    10.
    发明授权
    Speed-constrained flight management methods and systems 有权

    公开(公告)号：US11137774B2

    公开(公告)日：2021-10-05

    申请号：US16453470

    申请日：2019-06-26

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Dorothee De Villele ,  Michal Polansky ,  Marek Batelka ,  Laurent Villacampa

    IPC: G05D1/10 ,  G08G5/00 ,  G01C21/34 ,  G01C21/14 ,  G01C21/00 ,  G01C21/20 ,  G01C23/00

    Abstract: Systems and methods are provided for managing speed-constrained vehicle operations. One exemplary method of operating an aircraft involves identifying a speed constraint associated with a navigational reference point, determining a speed envelope region en route to the navigational reference point based at least in part on the first speed constraint, identifying a target speed en route to the navigational reference point, and determining a speed profile for autonomously operations en route to the navigational reference point within the speed envelope region. The speed profile intersects the target speed within the speed envelope region and a slope of the speed profile is influenced by the target speed, for example, to effectuate or approximate the target speed by increasing the duration of time operation at or around the target speed is achieved. In one or more embodiments, multiple different target speeds associated with different flight levels or operating regions are accounted for.

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