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. 03, 2019

Filed:

Feb. 19, 2016
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Brittany A. Friedland, Seattle, WA (US);

Robert L. Malone, Mukilteo, WA (US);

John R. Herrold, Goodyear, AZ (US);

Gregory P. Green, Kent, WA (US);

Assignee:

THE BOEING COMPANY, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G06F 3/048 (2013.01); G06F 3/0481 (2013.01); G06F 17/22 (2006.01); G06F 17/50 (2006.01); H04L 12/24 (2006.01); H04L 29/08 (2006.01); G06F 8/34 (2018.01); G06F 9/445 (2018.01); G08G 5/00 (2006.01); H04B 7/185 (2006.01);
U.S. Cl.
CPC ...
G06F 3/0481 (2013.01); G06F 8/34 (2013.01); G06F 9/44505 (2013.01); G06F 17/2247 (2013.01); G06F 17/5095 (2013.01); G08G 5/0021 (2013.01); H04B 7/18506 (2013.01); H04L 41/12 (2013.01); H04L 41/22 (2013.01); H04L 67/12 (2013.01);
Abstract

An improved system and method for modeling the data paths amongst the multiple avionic components inside an aircraft is described. A graphical user interface (GUI) operable to depict an interactive environment representing avionic components and data paths between the avionic components is generated, where the graphical user interface depicts a representation of an input, output, and operation associated with the avionic components. Using the GUI, data indicative of the input, output, and operation is received. The data is stored in a machine readable form, and translated into binary form usable to control on-aircraft communication between the avionic components.


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