The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Dec. 20, 2022

Filed:

Oct. 10, 2019
Applicant:

Honeywell International Inc., Morris Plains, NJ (US);

Inventors:

Barbara Holder, Deer Valley, AZ (US);

Stephen Whitlow, St. Louis Park, MN (US);

Christopher Heine, Mesa, AZ (US);

Steven Crouch, Mesa, AZ (US);

Kelsey Keberle, Tempe, AZ (US);

Assignee:

HONEYWELL INTERNATIONAL INC., Charlotte, NC (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G08G 5/00 (2006.01); B64D 45/00 (2006.01); G01C 21/20 (2006.01); G06F 3/0482 (2013.01); G06F 3/04815 (2022.01);
U.S. Cl.
CPC ...
G08G 5/0039 (2013.01); B64D 45/00 (2013.01); G01C 21/20 (2013.01); G06F 3/0482 (2013.01); G08G 5/0013 (2013.01); G08G 5/0021 (2013.01); G08G 5/0026 (2013.01); G08G 5/0056 (2013.01); B64D 2045/0075 (2013.01); B64D 2045/0085 (2013.01); G06F 3/04815 (2013.01);
Abstract

A flight deck system for providing task management assistance in managing the flight path to the flight crew is provided. The system is configured to: mine flight plan data for a current flight plan, navigational data, and vertical situation display (VSD) data; obtain notification data items originating from onboard avionics systems and systems external to the aircraft that indicate upcoming conditions that will affect the current flight plan; automatically analyze the mined flight plan data and the notification data items to identify a sensed deviation condition; automatically identify an aircraft-related deviation condition from an aircraft failure event; receive flight crew notification of a non-sensed deviation condition; automatically generate a plurality of flight plan deviation options to accommodate a sensed deviation condition, an aircraft-related deviation condition, or a non-sensed deviation condition; and present graphical elements representative of the flight plan deviation options to the flight crew on an integrated interactive graphical user interface.


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