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:
Sep. 29, 2026

Filed:

Apr. 19, 2022
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Edgardo E. Estavillo-Torrellas, Tucson, AZ (US);

Benjamin Westin, Charleston, SC (US);

Terry R. Vogler, Charleston, SC (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G06F 30/15 (2020.01); B64F 5/60 (2017.01);
U.S. Cl.
CPC ...
G06F 30/15 (2020.01); B64F 5/60 (2017.01);
Abstract

A method for analysis of electromagnetic effects (EME) on a structural section of an aircraft is provided. The method includes producing a computer-aided design (CAD) model of the structural section of the aircraft including a plurality of ribs defining bays, and identifiers of designated routing of system wiring through one or more of the bays. An engineering analysis of the structural section is performed based on the CAD model to determine electrical threshold values for locations for the one or more of the bays. The method includes identifying any of the locations at which an electrical threshold value exceeds a predetermined threshold associated with a keep-out distance relative to the system wiring. And the method includes generating an output including information of those of the locations that are identified, and indicia for indicating a recommended modification to address the EME threat.


Find Patent Forward Citations

Estavillo-Torrellas, Edgardo. (2026). Electromagnetic effects analysis on a structural section of an aircraft (U.S. Patent No. 12748899). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/12748899

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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