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：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.