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    System and Method for Modulating Premature Descent Protection Envelope
    11.
    发明申请
    System and Method for Modulating Premature Descent Protection Envelope 审中-公开

    公开(公告)号：US20200148385A1

    公开(公告)日：2020-05-14

    申请号：US16735261

    申请日：2020-01-06

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Yasuo Ishihara ,  Steve Johnson ,  Kevin J Conner

    IPC: B64D45/04 ,  G05D1/06 ,  G08G5/00 ,  G08G5/02 ,  G01C23/00

    Abstract: A system and method of shifting a premature descent protection envelope for an aircraft has been developed. First, a premature descent protection envelope (PDP) is determined including a first boundary at a first distance from the runway. Next, a nominal approach path is determined for approaching the runway and an approach path angle. Also, a flight path angle of the aircraft is determined. The first boundary is shifted in an upward direction from the runway in response to the aircraft being below the nominal approach path, and the flight path angle being greater than the nominal approach path angle.

    Maintenance assistant system
    12.
    发明授权
    Maintenance assistant system 有权
    维修辅助系统

    公开(公告)号：US09530057B2

    公开(公告)日：2016-12-27

    申请号：US14090106

    申请日：2013-11-26

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Kevin J Conner ,  Santosh Mathan

    IPC: G06K9/00 ,  G06F3/03 ,  G09B9/00 ,  G06Q10/00 ,  G06K9/32 ,  G06F3/01

    CPC classification number: G06K9/00671 ,  G05B2219/32014 ,  G06F3/0304 ,  G06K9/3216 ,  G06Q10/20 ,  G09B9/006

    Abstract: A maintenance assistance system and method of operating are provided. The maintenance assistance system may include, but is not limited to, a camera, a speaker, a technician marker, a memory configured to store a location of a plurality of tags and a location of at least one component relative to at least one of the plurality of tags, and a processor communicatively coupled to the camera, the speaker and the memory, the processor configured to receive an indication of one of the components, determine a location of the technician marker relative to the location of the indicated component based upon data from the camera and the location of the indicated component relative to the at least one of the plurality of tags, and output position information to the speaker based upon the determined location of the technician marker relative to the location of the indicated component.

    Abstract translation: 提供维护辅助系统和操作方法。 维护辅助系统可以包括但不限于相机，扬声器，技术人员标记，被配置为存储多个标签的位置的存储器以及相对于至少一个标签的至少一个部件的位置 多个标签和通信地耦合到相机，扬声器和存储器的处理器，处理器被配置为接收组件之一的指示，基于数据确定技术人员标记相对于所指示部件的位置的位置 根据相对于指示的组件相对于所指示的组件的位置确定的位置，从照相机和所指示的组件相对于多个标签中的至少一个标签的位置输出位置信息到扬声器。

    SYSTEM AND METHOD FOR ALERTING OF REMAINING RUNWAY UPON LANDING BASED ON DECELERATION
    14.
    发明申请
    SYSTEM AND METHOD FOR ALERTING OF REMAINING RUNWAY UPON LANDING BASED ON DECELERATION 审中-公开
    系统和方法，用于基于减速度对着陆运行进行后续运行

    公开(公告)号：US20150127196A1

    公开(公告)日：2015-05-07

    申请号：US14072899

    申请日：2013-11-06

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Yasuo Ishihara ,  Steve Johnson ,  Kevin J Conner

    IPC: G08G5/02

    CPC classification number: G08G5/02 ,  G01C23/00 ,  G05D1/0676 ,  G08G5/0021 ,  G08G5/025

    Abstract: A system and method are provided for alerting of remaining runway based on deceleration, following, for example, a landing or discontinued takeoff. An advisory system compares the current aircraft deceleration value to a predetermined threshold value when proceeding down the runway. If the current aircraft deceleration is less than the threshold value, the runway distance remaining callouts are triggered.

    Abstract translation: 提供了一种系统和方法，用于基于减速来警报剩余的跑道，例如，着陆或停止起飞。 咨询系统将当前的飞机减速度值与沿跑道行驶时的预定阈值进行比较。 如果当前飞机减速度小于阈值，则会触发跑道距离剩余标注。

    SYSTEM AND METHOD FOR PROVIDING MODEL-BASED ALERTING OF SPATIAL DISORIENTATION TO A PILOT
    15.
    发明申请
    SYSTEM AND METHOD FOR PROVIDING MODEL-BASED ALERTING OF SPATIAL DISORIENTATION TO A PILOT 有权
    用于向导航提供基于模型的空间分辨率的系统和方法

    公开(公告)号：US20150022380A1

    公开(公告)日：2015-01-22

    申请号：US13943549

    申请日：2013-07-16

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Kevin J Conner ,  Santosh Mathan ,  Steve Johnson

    IPC: B64D45/00

    CPC classification number: B64D45/00 ,  A61B5/00 ,  A61B5/4023 ,  A61B2503/22 ,  B64D2045/004

    Abstract: A system and method monitor aircraft state parameters, for example, aircraft movement and flight parameters, applies those inputs to a spatial disorientation model, and makes a prediction of when pilot may become spatially disoriented. Once the system predicts a potentially disoriented pilot, the sensitivity for alerting the pilot to conditions exceeding a threshold can be increased and allow for an earlier alert to mitigate the possibility of an incorrect control input.

    Abstract translation: 监视飞机状态参数（例如飞机运动和飞行参数）的系统和方法将这些输入应用于空间定向模型，并且对飞行员何时可能变得空间迷失方向进行预测。 一旦系统预测潜在迷失方向的飞行员，可以增加提醒飞行员超出阈值条件的灵敏度，并允许更早的警报来减轻错误的控制输入的可能性。

    Flight deck display systems and methods for visually indicating low speed change conditions during takeoff and landing
    19.
    发明授权
    Flight deck display systems and methods for visually indicating low speed change conditions during takeoff and landing 有权
    飞行甲板显示系统和视觉指示起飞和着陆时低速变化条件的方法

    公开(公告)号：US09529010B2

    公开(公告)日：2016-12-27

    申请号：US13919431

    申请日：2013-06-17

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Steve Johnson ,  Yasuo Ishihara ,  Kevin J Conner

    IPC: G08B21/00 ,  G08B5/00 ,  G01P1/10 ,  G01P5/00 ,  G01C23/00

    CPC classification number: G01P1/10 ,  G01C23/00 ,  G01P5/00

    Abstract: Embodiments of a flight deck display system deployed onboard an 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 device and a controller. The controller is configured to: (i) establish the speed trend of the aircraft over a predetermined time period; (ii) generate a primary flight display on the cockpit display device including a speed trend vector graphic representative of the established speed trend; and (iii) alter the appearance of the speed trend vector graphic in a first predetermined manner if a low speed change condition is detected during at least one of aircraft takeoff and landing.

    Abstract translation: 提供了部署在飞行器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也是如此。 在一个实施例中，驾驶舱显示系统包括驾驶舱显示装置和控制器。 控制器被配置为：（i）在预定时间段内建立飞机的速度趋势; （ii）在驾驶舱显示装置上产生代表所建立的速度趋势的速度趋势矢量图形的主飞行显示; 以及（iii）如果在飞机起飞和着陆期间的至少一个中检测到低速变化条件，则以第一预定方式改变速度趋势矢量图形的外观。

    RUNWAY LOCATION DETERMINATION
    20.
    发明申请
    RUNWAY LOCATION DETERMINATION 有权
    跑道位置确定

    公开(公告)号：US20150294573A1

    公开(公告)日：2015-10-15

    申请号：US14250022

    申请日：2014-04-10

    Applicant: Honeywell International Inc.

    Inventor： Kevin J Conner ,  Christine Marie Haissig ,  Ruy C. Brandao

    IPC: G08G5/04 ,  G08G5/00 ,  G01C21/00

    CPC classification number: G08G5/0017 ,  G01C21/00 ,  G01C21/30 ,  G08G5/0013 ,  G08G5/0082 ,  G08G5/065

    Abstract: In some examples described herein, a runway location is determined based on aircraft state information from at least one aircraft. For example, a processor may determine the coordinates of one or more points of a runway based on aircraft state information generated by one or more aircraft using the runway. In some examples, the processor may aggregate coordinates determined from the aircraft state information provided by a plurality of different aircraft in order to determine the location of the runway. The processor can be located onboard an aircraft providing the state information, onboard a different aircraft, or external to any aircraft.

    Abstract translation: 在本文描述的一些示例中，基于来自至少一架飞行器的飞机状态信息来确定跑道位置。 例如，处理器可以基于由使用跑道的一个或多个飞行器产生的飞行器状态信息来确定跑道的一个或多个点的坐标。 在一些示例中，处理器可以聚集由多个不同飞行器提供的飞行器状态信息确定的坐标，以便确定跑道的位置。 处理器可以位于提供状态信息的飞机上，在不同的飞机上或在任何飞机外部。

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