公开(公告)号：US10761674B2

公开(公告)日：2020-09-01

申请号：US15874066

申请日：2018-01-18

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Sripathi Ramachandra ,  Mark Pearson ,  PraveenKumar Ayyathurai

IPC: G06F3/048 ,  G06F3/0481 ,  G06F3/0484 ,  G06F3/0485 ,  B64D43/00 ,  G06F3/0488 ,  G01C23/00

Abstract: A method for providing flight data onboard an aircraft is provided. The method obtains avionics data, by a processor communicatively coupled to a display device onboard the aircraft; presents a graphical user interface (GUI), by the display device, wherein the GUI comprises at least a speed tape graphical element and an altitude tape graphical element; receives user input manipulations via a user interface communicatively coupled to the processor; executes the user input manipulations for the altitude tape graphical element or the speed tape graphical element, to generate a revised altitude tape graphical element or a revised speed tape graphical element; generates a revised GUI comprising the revised altitude tape graphical element or the revised speed tape graphical element; and presents the revised GUI, via the display device.

公开(公告)号：US20210018333A1

公开(公告)日：2021-01-21

申请号：US16512151

申请日：2019-07-15

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Sripathi Ramachandra ,  Greg Carlucci ,  Karel Mundel ,  Richard Snyder ,  Mark Pearson ,  Udipi Ranga Ananthram ,  PraveenKumar Ayyathurai ,  Samrat Kar

IPC: G01C23/00 ,  G06F3/0484 ,  G06F3/14 ,  B64D43/02

Abstract: Methods and systems are provided for presenting an energy state associated with an aircraft with respect to an operating envelope region for a procedure to restart an engine of the aircraft. One method involves providing a graphical user interface display having a first reference axis corresponding to a first energy state parameter and a second reference axis corresponding to a second energy state parameter different from the first energy state parameter, providing a graphical representation of an operating envelope region associated with a procedure for starting an engine of the aircraft with respect to the first and second reference axes, obtaining current values for the first and second energy state parameters for the aircraft, and providing a graphical representation of the aircraft positioned with respect to the first and second reference axes based on the current values for the first and second energy state parameters.

公开(公告)号：US11385072B2

公开(公告)日：2022-07-12

申请号：US16512151

申请日：2019-07-15

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Sripathi Ramachandra ,  Greg Carlucci ,  Karel Mundel ,  Richard Snyder ,  Mark Pearson ,  Udipi Ranga Ananthram ,  PraveenKumar Ayyathurai ,  Samrat Kar

IPC: G01C23/00 ,  G06F3/0484 ,  G06F3/14 ,  B64D43/02 ,  G06F3/04847 ,  G06F3/0482

Abstract: Methods and systems are provided for presenting an energy state associated with an aircraft with respect to an operating envelope region for a procedure to restart an engine of the aircraft. One method involves providing a graphical user interface display having a first reference axis corresponding to a first energy state parameter and a second reference axis corresponding to a second energy state parameter different from the first energy state parameter, providing a graphical representation of an operating envelope region associated with a procedure for starting an engine of the aircraft with respect to the first and second reference axes, obtaining current values for the first and second energy state parameters for the aircraft, and providing a graphical representation of the aircraft positioned with respect to the first and second reference axes based on the current values for the first and second energy state parameters.

公开(公告)号：US20190220152A1

公开(公告)日：2019-07-18

申请号：US15874066

申请日：2018-01-18

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Sripathi Ramachandra ,  Mark Pearson ,  PraveenKumar Ayyathurai

IPC: G06F3/0481 ,  G06F3/0484 ,  G06F3/0485 ,  G06F3/0488 ,  B64D43/00

Abstract: A method for providing flight data onboard an aircraft is provided. The method obtains avionics data, by a processor communicatively coupled to a display device onboard the aircraft; presents a graphical user interface (GUI), by the display device, wherein the GUI comprises at least a speed tape graphical element and an altitude tape graphical element; receives user input manipulations via a user interface communicatively coupled to the processor; executes the user input manipulations for the altitude tape graphical element or the speed tape graphical element, to generate a revised altitude tape graphical element or a revised speed tape graphical element; generates a revised GUI comprising the revised altitude tape graphical element or the revised speed tape graphical element; and presents the revised GUI, via the display device.