公开(公告)号：US20220068149A1

公开(公告)日：2022-03-03

申请号：US17070212

申请日：2020-10-14

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Ratan Khatwa ,  Mohammed Ibrahim Mohideen ,  Vineetha Chandran ,  Dhivagar Palanisamy ,  Niranjan Kalyandurg

IPC: G08G5/06 ,  B64D43/00 ,  G08G5/00

Abstract: A flight deck system for providing progressive taxiing guidance is provided. The flight deck system comprises a controller configured to: generate a graphical insert to overlay a small portion of an active navigation display, the graphical insert providing a progressive depiction of upcoming travel surfaces on a cleared taxi route. The graphical insert comprises a non-linear map with non-linear scaling, a current travel surface alphanumeric indicator, and a current travel surface stick character representative of a current travel surface. The controller is further configured to position, on the graphical insert, a crossing travel surface sign, a first-turn travel surface stick character, and a second-turn travel surface stick character; update the position of the crossing travel surface sign, the first-turn travel surface stick character, and/or the second-turn travel surface stick character as the aircraft travels; and cause the graphical insert to be displayed as an overlay on the active navigation display.

公开(公告)号：US11749127B2

公开(公告)日：2023-09-05

申请号：US17070212

申请日：2020-10-14

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Ratan Khatwa ,  Mohammed Ibrahim Mohideen ,  Vineetha Chandran ,  Dhivagar Palanisamy ,  Niranjan Kalyandurg

IPC: G08G5/06 ,  B64D43/00 ,  G08G5/00

CPC classification number: G08G5/065 ,  B64D43/00 ,  G08G5/0013 ,  G08G5/0043

Abstract: A flight deck system for providing progressive taxiing guidance is provided. The flight deck system comprises a controller configured to: generate a graphical insert to overlay a small portion of an active navigation display, the graphical insert providing a progressive depiction of upcoming travel surfaces on a cleared taxi route. The graphical insert comprises a non-linear map with non-linear scaling, a current travel surface alphanumeric indicator, and a current travel surface stick character representative of a current travel surface. The controller is further configured to position, on the graphical insert, a crossing travel surface sign, a first-turn travel surface stick character, and a second-turn travel surface stick character; update the position of the crossing travel surface sign, the first-turn travel surface stick character, and/or the second-turn travel surface stick character as the aircraft travels; and cause the graphical insert to be displayed as an overlay on the active navigation display.

公开(公告)号：US20220392358A1

公开(公告)日：2022-12-08

申请号：US17443288

申请日：2021-07-23

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Harisha Bangalore Manjunath ,  Rushoth Kumar M C ,  Venu Puttam ,  Murali Kadeppagari ,  Prashant Hegde ,  Chandana Venigalla ,  Supratik Gon ,  Brad H. Miller ,  Gary Ostrom ,  Ricardo Darif Bortolini ,  Dhivagar Palanisamy ,  David Kolbet ,  John Vo

IPC: G08G5/00 ,  B64D45/00

Abstract: A system and method for implementing an autonomous distress tracking (ADT) triggering function is provided. The method comprises receiving a configuration file containing a plurality of user configurable parameters from a ground-based system, configuring an aircraft condition and monitoring function (ACMF) engine to apply trigger logic specified by the plurality of user configurable parameters to aircraft sensor and/or system data and monitoring for a plurality of distress conditions specified by the plurality of user configurable parameters; executing the configured ACMF engine to detect the occurrence of a distress condition; automatically generating a data message when a distress condition occurrence has been detected wherein the data message can include aircraft position data specified in the user configurable parameters, the aircraft sensor and/or system data on which the detection of the one or more trigger conditions was based, and the identity of the detected distress condition; and automatically sending the data message to a transmission system onboard the aircraft that is configured to transmit a search and rescue signal.

公开(公告)号：US09142133B2

公开(公告)日：2015-09-22

申请号：US14065655

申请日：2013-10-29

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Dhivagar Palanisamy ,  Saravanakumar Gurusamy ,  Vishnu Vardhan Reddy Annapureddy

IPC: G08G1/0967 ,  G08G5/00

CPC classification number: G08G5/0021

Abstract: A system and method are provided for displaying an enhanced longitudinal scale providing user interface and awareness for executing the Next Gen Flight Deck Interval Management (FIM) and the Cockpit Display of Traffic Information (CDTI) application Enhanced Visual Separation on Approach (VSA) to provide a required spacing between aircraft based on distance and time. An own-ship and a reference aircraft are displayed in relation to a desired flight path. A symbol indicates the desired separation of the own-ship from the aircraft.

Abstract translation: 提供了一种系统和方法，用于显示增强的纵向尺度，以提供用于执行下一代飞行甲板间隔管理（FIM）和驾驶舱显示交通信息（CDTI）应用增强视觉分离方法（VSA）的用户界面和意识，以提供 基于距离和时间的飞机之间所需的间距。 相对于所需的飞行路径显示自己的船和参考飞机。 一个符号表示自己与飞机的分离。

公开(公告)号：US20150120177A1

公开(公告)日：2015-04-30

申请号：US14065655

申请日：2013-10-29

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Dhivagar Palanisamy ,  Saravanakumar Gurusamy ,  Vishnu Vardhan Reddy Annapureddy

IPC: G08G5/00

CPC classification number: G08G5/0021

Abstract: A system and method are provided for displaying an enhanced longitudinal scale providing user interface and awareness for executing the Next Gen Flight Deck Interval Management (FIM) and the Cockpit Display of Traffic Information (CDTI) application Enhanced Visual Separation on Approach (VSA) to provide a required spacing between aircraft based on distance and time. An own-ship and a reference aircraft are displayed in relation to a desired flight path. A symbol indicates the desired separation of the own-ship from the aircraft.

Abstract translation: 提供了一种系统和方法，用于显示增强的纵向尺度，以提供用于执行下一代飞行甲板间隔管理（FIM）和驾驶舱显示交通信息（CDTI）应用增强视觉分离方法（VSA）的用户界面和意识，以提供 基于距离和时间的飞机之间所需的间距。 相对于所需的飞行路径显示自己的船和参考飞机。 一个符号表示自己与飞机的分离。