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    ENERGY MANAGEMENT VISUALIZATION METHODS AND SYSTEMS
    11.
    发明申请
    ENERGY MANAGEMENT VISUALIZATION METHODS AND SYSTEMS 审中-公开

    公开(公告)号：US20200013295A1

    公开(公告)日：2020-01-09

    申请号：US16026423

    申请日：2018-07-03

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Zdenek Moravek ,  Ivan Lacko

    IPC: G08G5/00 ,  G08G5/02 ,  G05D1/06

    Abstract: Methods and systems are provided for guiding or otherwise assisting a stabilized approach to a destination by presenting an energy state associated with an aircraft with respect to a target energy state for the stabilized approach. One method involves providing a graphical indication of a targeted energy state at a first position, a second graphical indication of a current energy state at a second position, and a third graphical indication of a configuration change at a third position. The distance with respect to a reference axis between the first position and the second position corresponds to a difference between a target parameter value associated with the targeted energy state and a current parameter value associated with the current energy state, and while a second distance between the first position and the third position with respect to the reference axis corresponds to an estimated amount of time before the configuration change.

    AIRCRAFT SYSTEMS AND METHODS FOR DETECTING NON-COMPLIANT PILOT ACTION
    15.
    发明申请
    AIRCRAFT SYSTEMS AND METHODS FOR DETECTING NON-COMPLIANT PILOT ACTION 有权
    用于检测不合格引导作用的飞机系统和方法

    公开(公告)号：US20150081138A1

    公开(公告)日：2015-03-19

    申请号：US14030426

    申请日：2013-09-18

    Applicant: Honeywell International Inc.

    Inventor： Ivan Lacko ,  Jiri Vasek ,  Petr Uhlir

    IPC: B64D45/00

    CPC classification number: B64D45/00 ,  G08G5/0013 ,  G08G5/0021

    Abstract: Aircraft systems and methods for detecting non-compliant pilot action are provided. The method comprises analyzing an outbound communication from an aircraft to recognize a word or phrase corresponding to a parameter associated with a prior request for pilot action. If the word or phrase is recognized, the method further comprises storing data corresponding to the outbound communication in a data storage device. The stored data and pilot action taken are compared to determine if there is a discrepancy between the pilot action and the stored data. A discrepancy alert is outputted if the discrepancy is determined to exist. A predetermined time interval is timed from the outbound communication. A timeout alert is outputted at a timeout of the predetermined time interval unless the requested pilot action is taken within the predetermined time interval.

    Abstract translation: 提供了用于检测不合规导频动作的飞行器系统和方法。 该方法包括分析来自飞行器的出站通信以识别与先前对先导动作请求相关联的参数相对应的单词或短语。 如果该单词或短语被识别，则该方法还包括将对应于出站通信的数据存储在数据存储设备中。 比较所存储的数据和导频操作，以确定导频操作和存储的数据之间是否存在差异。 如果确定存在差异，则输出差异警报。 从出站通信定时预定的时间间隔。 在预定时间间隔的超时时间内输出超时警报，除非在预定的时间间隔内进行所请求的导频操作。

    Energy management visualization methods and systems
    17.
    发明授权
    Energy management visualization methods and systems 有权

    公开(公告)号：US10854091B2

    公开(公告)日：2020-12-01

    申请号：US16026423

    申请日：2018-07-03

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Zdenek Moravek ,  Ivan Lacko

    IPC: G08G5/00 ,  G05D1/06 ,  G08G5/02

    Abstract: Methods and systems are provided for guiding or otherwise assisting a stabilized approach to a destination by presenting an energy state associated with an aircraft with respect to a target energy state for the stabilized approach. One method involves providing a graphical indication of a targeted energy state at a first position, a second graphical indication of a current energy state at a second position, and a third graphical indication of a configuration change at a third position. The distance with respect to a reference axis between the first position and the second position corresponds to a difference between a target parameter value associated with the targeted energy state and a current parameter value associated with the current energy state, and while a second distance between the first position and the third position with respect to the reference axis corresponds to an estimated amount of time before the configuration change.

    Aircraft display system pertaining to energy management
    18.
    发明授权
    Aircraft display system pertaining to energy management 有权

    公开(公告)号：US10152195B2

    公开(公告)日：2018-12-11

    申请号：US14967557

    申请日：2015-12-14

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Ivan Lacko ,  Yujia Cao ,  Zdenek Moravek ,  Stepan Dopita

    IPC: G06F3/048 ,  G06F3/0481 ,  G01C23/00 ,  G08G5/00 ,  G08G5/02

    Abstract: A computer-implemented flight display system including a computer processor that is capable of determining a current energy situation of an aircraft, an electronic display device, and a graphical user interface (GUI) provided on the electronic display device. The GUI includes a current aircraft position symbol, an optimal aircraft position symbol, and at least one symbol indicating a position for changing aircraft configuration. Relative positioning on the GUI of the optimal aircraft position system and the at least one symbol indicating a position for changing aircraft configuration is based at least in part on the determined current energy situation of the aircraft.

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