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:
Jul. 07, 2020

Filed:

Mar. 06, 2018
Applicant:

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

Inventors:

Sripathi Ramachandra, Karnataka, IN;

Mark Pearson, Peoria, AZ (US);

Greg Carlucci, Phoenix, AZ (US);

Richard Snyder, Phoenix, AZ (US);

Balaji Srinivasan, Karnataka, IN;

Assignee:

HONEYWELL INTERNATIONAL INC., Morris Plains, NJ (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G08G 5/00 (2006.01); G01C 23/00 (2006.01);
U.S. Cl.
CPC ...
G08G 5/0021 (2013.01); G01C 23/00 (2013.01); G01C 23/005 (2013.01); G08G 5/003 (2013.01); G08G 5/0039 (2013.01); G08G 5/0052 (2013.01); G08G 5/0078 (2013.01);
Abstract

Methods and systems for a flight display system are provided. The method includes: commanding a vertical situation display (VSD) and a lateral navigation display (ND) to render, concurrently, a viewing segment of a flight plan. The method includes receiving a user input selecting a section of the viewing segment, the user input being received on only one of the VSD and the ND. The method continues by commanding, concurrently, the VSD and the ND to visually distinguish the section, and to demark the section on the VSD with starting points and ending points. The method identifies a flight parameter, and for the flight parameter, includes (a) determining which display, among the VSD and the ND, is appropriate for the rendering of flight parameter information; (b) generating flight parameter information based on (a); and (c) overlaying the flight parameter information on the appropriate display.


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