公开(公告)号：US20220108620A1

公开(公告)日：2022-04-07

申请号：US17061060

申请日：2020-10-01

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Tomas Bouda ,  Petra Machackova ,  Stepan Dopita ,  Ivan Lacko

IPC: G08G5/00

Abstract: A flight display system for providing a visualization of an assumed lateral and vertical flight path on an avionic display for an aircraft performing energy management during an approach procedure, and methods for producing the same. The system improves upon available human-machine interfaces (HMI) by providing information not otherwise available; that being, a visualization of an assumed lateral and vertical flight path to assist the flight crew in making adjustments to the configuration of the aircraft when the aircraft is making an approach to an airport.

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.

公开(公告)号：US20170168658A1

公开(公告)日：2017-06-15

申请号：US14967557

申请日：2015-12-14

Applicant: HONEYWELL INTERNATIONAL INC.

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

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

CPC classification number: G06F3/0481 ,  G01C23/005 ,  G08G5/0021 ,  G08G5/025

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.