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    System and method for volumetric computing
    1.
    发明授权
    System and method for volumetric computing 有权

    公开(公告)号：US09671868B2

    公开(公告)日：2017-06-06

    申请号：US13915232

    申请日：2013-06-11

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Amit Nishikant Kawalkar

    IPC: G09G5/00 ,  G06F3/01 ,  G06F3/00 ,  G06F3/0488

    CPC classification number: G06F3/017 ,  G06F3/005 ,  G06F3/04883 ,  G06F3/04886 ,  G06F2203/04108

    Abstract: A system and method is provided for analyzing the movement of an object. The system is comprised of a sensor that is coupled to a processor that is configured to generate a volume that corresponds to a predefined area and the location of the object. The sensor detects the movement of the object and determines if the object's movement is within the volume. If the movement is within the volume, then an information channel is created between the volume and the user defined algorithm. The movement is then compared with the requirements of the user defined algorithm and accepted if the movement meets the requirements. Otherwise, the object's movement is discarded if the movement is not within the volume or does not meet the requirements of the user defined algorithm.

    COCKPIT DISPLAY SYSTEMS AND METHODS FOR GENERATING NAVIGATION DISPLAYS INCLUDING LANDING DIVERSION SYMBOLOGY
    2.
    发明申请
    COCKPIT DISPLAY SYSTEMS AND METHODS FOR GENERATING NAVIGATION DISPLAYS INCLUDING LANDING DIVERSION SYMBOLOGY 有权
    用于生成导航显示的COCKPIT显示系统和方法，包括着陆分析符号

    公开(公告)号：US20160229554A1

    公开(公告)日：2016-08-11

    申请号：US14619849

    申请日：2015-02-11

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Amit Nishikant Kawalkar ,  Rajesh Chaubey ,  Rajeev Mohan

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

    CPC classification number: G08G5/0056 ,  G01C23/00 ,  G01C23/005 ,  G08G5/00 ,  G08G5/0021 ,  G08G5/0039 ,  G08G5/025

    Abstract: Cockpit display systems and methods for generating navigation displays including landing diversion symbology are provided. In one embodiment, the cockpit display system includes a cockpit monitor and a controller coupled to the cockpit monitor. The controller is configured to assess the current feasibility of landing at one or more diversion airports in a range of an aircraft on which the cockpit display system is deployed. The controller is further configured to assign each diversion airport to one of a plurality of predetermined landing feasibility categories, and generate a horizontal navigation display on the cockpit monitor including symbology representative of the feasibility category assigned to one or more of the diversion airports.

    Abstract translation: 提供了用于产生导航显示器的驾驶舱显示系统和方法，包括着陆转向符号系统。 在一个实施例中，驾驶舱显示系统包括驾驶舱监视器和耦合到驾驶舱监视器的控制器。 控制器被配置为评估在部署驾驶舱显示系统的飞机的范围内的一个或多个转向机场降落的当前可行性。 控制器还被配置为将每个引水机构分配到多个预定着陆可行性类别中的一个，并且在驾驶舱监视器上生成水平导航显示器，其包括代表分配给一个或多个转向机场的可行性类别的符号系统。

    SYSTEM AND METHOD FOR VOLUMETRIC COMPUTING
    3.
    发明申请
    SYSTEM AND METHOD FOR VOLUMETRIC COMPUTING 有权
    用于体积计算的系统和方法

    公开(公告)号：US20140361972A1

    公开(公告)日：2014-12-11

    申请号：US13915232

    申请日：2013-06-11

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Amit Nishikant Kawalkar

    IPC: G06F3/01

    CPC classification number: G06F3/017 ,  G06F3/005 ,  G06F3/04883 ,  G06F3/04886 ,  G06F2203/04108

    Abstract: A system and method is provided for analyzing the movement of an object. The system is comprised of a sensor that is coupled to a processor that is configured to generate a volume that corresponds to a predefined area and the location of the object. The sensor detects the movement of the object and determines if the object's movement is within the volume. If the movement is within the volume, then an information channel is created between the volume and the user defined algorithm. The movement is then compared with the requirements of the user defined algorithm and accepted if the movement meets the requirements. Otherwise, the object's movement is discarded if the movement is not within the volume or does not meet the requirements of the user defined algorithm.

    Abstract translation: 提供了一种用于分析物体运动的系统和方法。 该系统包括耦合到处理器的传感器，该处理器被配置为生成对应于预定义区域的物体和物体的位置。 传感器检测物体的运动，并确定物体的运动是否在体积内。 如果移动在卷内，则在卷和用户定义的算法之间创建信息通道。 然后将移动与用户定义的算法的要求进行比较，并且如果移动满足要求则被接受。 否则，如果移动不在卷内或不符合用户定义的算法的要求，则物体的移动被丢弃。

    SYSTEM AND METHOD FOR INTERACTING WITH A TOUCH SCREEN INTERFACE UTILIZING AN INTELLIGENT STENCIL MASK
    4.
    发明申请
    SYSTEM AND METHOD FOR INTERACTING WITH A TOUCH SCREEN INTERFACE UTILIZING AN INTELLIGENT STENCIL MASK 有权
    使用触觉屏幕接口的触摸屏界面的系统和方法

    公开(公告)号：US20140164983A1

    公开(公告)日：2014-06-12

    申请号：US13708320

    申请日：2012-12-07

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Amit Nishikant Kawalkar ,  Hans Roth

    IPC: G06F3/048

    CPC classification number: G06F3/048 ,  G06F3/04886

    Abstract: A system and method are provided for employing an intelligent stencil mask to interact with a touch screen interface and thereby reduce the probability of accidental control function activation. A touch screen interface onboard an aircraft is coupled to a processor and is configured to generate a first virtual mask having a first region and a second region. A user interaction is then detected with one of the first region and the second region. A first reconfigured virtual mask is generated if the user interacted with the second region. However, an aircraft control function is activated if the user interacted with the first region.

    Abstract translation: 提供了一种用于使用智能模板掩模与触摸屏界面交互从而降低意外控制功能激活的可能性的系统和方法。 飞机上的触摸屏接口耦合到处理器，并且被配置为生成具有第一区域和第二区域的第一虚拟掩模。 然后用第一区域和第二区域之一检测用户交互。 如果用户与第二区域交互，则生成第一重新配置的虚拟掩码。 然而，如果用户与第一区域交互，飞机控制功能被激活。

    Thrust management and interface for aircraft taxi operations
    6.
    发明授权
    Thrust management and interface for aircraft taxi operations 有权

    公开(公告)号：US09688392B2

    公开(公告)日：2017-06-27

    申请号：US14316606

    申请日：2014-06-26

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Amit Nishikant Kawalkar

    IPC: B64C25/50 ,  B64C25/40 ,  B64D31/04 ,  B64D31/06 ,  B64D43/02

    CPC classification number: B64C25/405 ,  B64D31/04 ,  B64D31/06 ,  B64D43/02 ,  Y02T50/823

    Abstract: An aircraft electric taxi drive system may provide electric taxiing of an aircraft by integrating control of an electric drive and an engine during the taxi phase of a flight plan. In some embodiments, the engine may provide supplemental drive to the aircraft's wheels during electric taxiing. The engine may be maintained on while the electric drive provides the main driving force to the wheels. A controller may determine the criteria to operate the engine as the electric drive taxis the aircraft to achieve a target ground speed. In some embodiments, a pilot interface may integrate control of the electric drive and the engine into a single throttle control providing the pilot an intuitive and singular point to throttle the aircraft without having to decide which taxi source is providing the taxi driving force.

    Speed change and acceleration point enhancement system and method
    7.
    发明授权
    Speed change and acceleration point enhancement system and method 有权

    公开(公告)号：US09663241B1

    公开(公告)日：2017-05-30

    申请号：US15132873

    申请日：2016-04-19

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Amit Nishikant Kawalkar

    IPC: B64D43/02

    CPC classification number: B64D43/02 ,  G01C21/00 ,  G01C23/00 ,  G01C23/005 ,  G08G5/0021 ,  G08G5/0052

    Abstract: A vehicle display system includes a display device and a processor. The processor is in operable communication with the display device and is coupled to receive vehicle path data and vehicle state data. The vehicle path data are representative of a planned vehicle path of the vehicle, and the vehicle state data are representative of current vehicle state. The processor is configured, upon receipt of these data, to command the display device to render at least a portion of the planned vehicle path and to selectively render one or both of a speed change point symbol and an acceleration point symbol on the current vehicle path. The symbols are rendered in a manner that is more intuitive for vehicle pilots.

    THRUST MANAGEMENT AND INTERFACE FOR AIRCRAFT TAXI OPERATIONS
    9.
    发明申请
    THRUST MANAGEMENT AND INTERFACE FOR AIRCRAFT TAXI OPERATIONS 有权
    航空运输管理和接口

    公开(公告)号：US20150375853A1

    公开(公告)日：2015-12-31

    申请号：US14316606

    申请日：2014-06-26

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Amit Nishikant Kawalkar

    IPC: B64C25/40 ,  B64D45/00

    CPC classification number: B64C25/405 ,  B64D31/04 ,  B64D31/06 ,  B64D43/02 ,  Y02T50/823

    Abstract: An aircraft electric taxi drive system may provide electric taxiing of an aircraft by integrating control of an electric drive and an engine during the taxi phase of a flight plan. In some embodiments, the engine may provide supplemental drive to the aircraft's wheels during electric taxiing. The engine may be maintained on while the electric drive provides the main driving force to the wheels. A controller may determine the criteria to operate the engine as the electric drive taxis the aircraft to achieve a target ground speed. In some embodiments, a pilot interface may integrate control of the electric drive and the engine into a single throttle control providing the pilot an intuitive and singular point to throttle the aircraft without having to decide which taxi source is providing the taxi driving force.

    Abstract translation: 飞机电动出租车司机系统可以通过在飞行计划的出租车阶段集成电驱动和发动机的控制来提供飞机的电滑行。 在一些实施例中，发动机可以在电滑行期间向飞行器的车轮提供补充驱动。 当电驱动器向车轮提供主要驱动力时，可以维持发动机。 当电动驾驶员乘坐飞机以实现目标地面速度时，控制器可以确定操作发动机的标准。 在一些实施例中，驾驶员接口可以将电力驱动器和发动机的控制集成到单个节气门控制中，从而为飞行员提供直观和奇点以遏制飞机，而不必决定哪个出租车提供出租车驱动力。

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