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:
Oct. 20, 2020

Filed:

Nov. 29, 2017
Applicant:

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

Inventors:

John G. Suddreth, Cave Creek, AZ (US);

Jerry Ball, Peoria, AZ (US);

Assignee:

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

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01C 23/00 (2006.01); G08G 5/00 (2006.01); B64D 43/00 (2006.01); B64D 45/00 (2006.01); G06F 30/15 (2020.01); B64C 23/04 (2006.01); B64C 30/00 (2006.01); G06F 119/10 (2020.01);
U.S. Cl.
CPC ...
G08G 5/0021 (2013.01); B64D 43/00 (2013.01); B64D 45/00 (2013.01); G01C 23/00 (2013.01); G06F 30/15 (2020.01); G08G 5/0039 (2013.01); B64C 23/04 (2013.01); B64C 30/00 (2013.01); G06F 2119/10 (2020.01);
Abstract

Avionic display systems and methods are provided for generating avionic displays including symbology decreasing the likelihood of boom tolerance threshold exceedance (an overpressure events) due to potential constructive interference between pressure waves occurring during supersonic flight. In various embodiments, the avionic display system includes a display device on which an avionic display is generated. A controller architecture is operably coupled to the display device and configured to determine when there exists a possibility for an overpressure event to occur in a future timeframe due to constructive interference between colliding pressure waves, which are forecast to occur during the impending supersonic flight of one or more A/C. When determining that there exists a possibility for an overpressure event to occur in the future timeframe due to constructive interference between pressure waves, the controller architecture further generates symbology or other graphics on the avionic display indicative of the potential occurrence of the overpressure event.


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