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:
Feb. 22, 2022

Filed:

Oct. 31, 2016
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Gary E. Georgeson, Tacoma, WA (US);

Jill P. Bingham, Seattle, WA (US);

Hong Hue Tat, Redmond, WA (US);

Yuan-Jye Wu, Issaquah, WA (US);

John M. Pryor, Lake Forest Park, WA (US);

Sadie L. Fieni, Charleston, SC (US);

Mark D. Winters, Maple Valley, WA (US);

Kathryn T. Moore, Los Alamitos, CA (US);

James C. Kennedy, Renton, WA (US);

Clayton M. Little, Mount Pleasant, SC (US);

John Z. Lin, Renton, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G01N 29/30 (2006.01); G01N 29/06 (2006.01); G01N 21/88 (2006.01); G01N 29/04 (2006.01); G01N 29/11 (2006.01); G01N 29/44 (2006.01); G06F 30/23 (2020.01); G01N 29/07 (2006.01); G01N 21/84 (2006.01);
U.S. Cl.
CPC ...
G01N 29/30 (2013.01); G01N 21/88 (2013.01); G01N 29/043 (2013.01); G01N 29/0645 (2013.01); G01N 29/07 (2013.01); G01N 29/11 (2013.01); G01N 29/4445 (2013.01); G06F 30/23 (2020.01); G01N 2021/8472 (2013.01); G01N 2291/011 (2013.01); G01N 2291/015 (2013.01); G01N 2291/0231 (2013.01); G01N 2291/0289 (2013.01); G01N 2291/044 (2013.01); G01N 2291/051 (2013.01); G01N 2291/106 (2013.01); G01N 2291/2632 (2013.01); G01N 2291/2694 (2013.01);
Abstract

Methods that provide wrinkle characterization and performance prediction for wrinkled composite structures using automated structural analysis. In accordance with some embodiments, the method combines the use of B-scan ultrasound data, automated optical measurement of wrinkles and geometry of cross-sections, and finite element analysis of wrinkled composite structure to provide the ability to assess the actual significance of a detected wrinkle relative to the intended performance of the structure. The disclosed method uses an ultrasonic inspection system that has been calibrated by correlating ultrasonic B-scan data acquired from reference standards with measurements of optical cross sections (e.g., micrographs) of those reference standards.


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