公开(公告)号：US20160161283A1

公开(公告)日：2016-06-09

申请号：US14559755

申请日：2014-12-03

Applicant: Honeywell International Inc.

Inventor： Raghu Shamasundar ,  Prasadrao Rao Piradi ,  Thomas D. Judd ,  David Pepitone ,  Abhishek Gupta ,  Adib Bouanani ,  Prashanth Ramanna

IPC: G01C23/00 ,  G06F3/0484 ,  H04L29/08 ,  G06F3/0481

CPC classification number: G01C23/005 ,  G06F3/0481

Abstract: Systems and methods for displaying position sensitive datalink messages on avionics displays are provided. In one embodiment, a flight deck instrument display system for an aircraft comprises: a flight plan display screen that displays a graphical representation of at least a part of an aircraft's planned flight path together with symbology representing a position of the aircraft with respect to the aircraft's planned flight path; wherein the flight plan display screen further displays at least one symbol positioned along the graphical representation of at least a part of the aircraft's planned flight path that indicates a point of applicability for a received uplink datalink message.

Abstract translation: 提供了在航空电子显示屏上显示位置敏感数据链路消息的系统和方法。 在一个实施例中，用于飞行器的飞行甲板仪表显示系统包括：飞行计划显示屏幕，其显示飞行器的计划飞行路径的至少一部分的图形表示，以及表示飞行器相对于飞机的飞行器的位置的符号 计划飞行路线; 其中所述飞行计划显示屏幕还显示沿着所述飞行器的计划飞行路径的至少一部分的图形表示定位的至少一个符号，其指示所接收的上行链路数据链路消息的适用点。

公开(公告)号：US20180273200A1

公开(公告)日：2018-09-27

申请号：US15469763

申请日：2017-03-27

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Dorothee De Villele ,  Rajesh Chaubey ,  Sharanabasappa Advani ,  Veeralla Sai V Yashodhar ,  Ranju Thomas Pulikot ,  Abhishek Gupta

IPC: B64D45/08 ,  G08G5/00 ,  B64C9/32

CPC classification number: B64D45/08 ,  B64C9/32 ,  G08G5/0021 ,  G08G5/0091 ,  G08G5/025

Abstract: Avionic display systems and methods are provided for generating avionic displays including instability prediction and avoidance symbology, such as dynamically-adjusted drag device deployment cues. In one embodiment, the avionic display system includes a controller and an avionic display device, which is coupled to the controller and on which an avionic display, such as a Vertical Situation Display (VSD), is generated. The controller is configured to: (i) project whether an unstable aircraft state will occur during an approach flown by an aircraft; (ii) when an unstable aircraft state is projected to occur, determine whether implementation of an optimized drag device deployment scheme can prevent the projected occurrence of the unstable aircraft state; and (iii) if determining that the implementation of the optimized drag device deployment scheme can prevent occurrence of the projected unstable aircraft state, generating symbology on the avionic display indicative of the optimized drag device deployment scheme.

公开(公告)号：US10654589B2

公开(公告)日：2020-05-19

申请号：US15469763

申请日：2017-03-27

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Dorothee De Villele ,  Rajesh Chaubey ,  Sharanabasappa Advani ,  Veeralla Sai V Yashodhar ,  Ranju Thomas Pulikot ,  Abhishek Gupta

IPC: B64D45/08 ,  G08G5/00 ,  B64C9/32 ,  G08G5/02

Abstract: Avionic display systems and methods are provided for generating avionic displays including instability prediction and avoidance symbology, such as dynamically-adjusted drag device deployment cues. In one embodiment, the avionic display system includes a controller and an avionic display device, which is coupled to the controller and on which an avionic display, such as a Vertical Situation Display (VSD), is generated. The controller is configured to: (i) project whether an unstable aircraft state will occur during an approach flown by an aircraft; (ii) when an unstable aircraft state is projected to occur, determine whether implementation of an optimized drag device deployment scheme can prevent the projected occurrence of the unstable aircraft state; and (iii) if determining that the implementation of the optimized drag device deployment scheme can prevent occurrence of the projected unstable aircraft state, generating symbology on the avionic display indicative of the optimized drag device deployment scheme.

公开(公告)号：US10330493B2

公开(公告)日：2019-06-25

申请号：US14559755

申请日：2014-12-03

Applicant: Honeywell International Inc.

Inventor： Raghu Shamasundar ,  Prasad Rao Piradi ,  Thomas D. Judd ,  David Pepitone ,  Abhishek Gupta ,  Adib Bouanani ,  Prashanth Ramanna

IPC: G01C23/00 ,  G06F3/0481

Abstract: Systems and methods for displaying position sensitive datalink messages on avionics displays are provided. In one embodiment, a flight deck instrument display system for an aircraft comprises: a flight plan display screen that displays a graphical representation of at least a part of an aircraft's planned flight path together with symbology representing a position of the aircraft with respect to the aircraft's planned flight path; wherein the flight plan display screen further displays at least one symbol positioned along the graphical representation of at least a part of the aircraft's planned flight path that indicates a point of applicability for a received uplink datalink message.