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:
Jun. 04, 2019

Filed:

Nov. 26, 2014
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Mostafa Rassaian, Bellevue, WA (US);

Jonathan H. Gosse, Issaquah, WA (US);

Stephen Christensen, Sammamish, WA (US);

Assignee:

THE BOEING COMPANY, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G06F 17/50 (2006.01); G01N 3/32 (2006.01); G01N 29/04 (2006.01); G01N 29/12 (2006.01); B29C 65/00 (2006.01); B64C 1/00 (2006.01);
U.S. Cl.
CPC ...
G01N 3/32 (2013.01); G01N 29/045 (2013.01); G01N 29/12 (2013.01); G06F 17/5009 (2013.01); G06F 17/5018 (2013.01); G06F 17/5086 (2013.01); G06F 17/5095 (2013.01); B29C 66/721 (2013.01); B29C 66/7212 (2013.01); B64C 2001/0072 (2013.01); G01N 2291/02827 (2013.01); G06F 2217/44 (2013.01); Y02T 50/43 (2013.01);
Abstract

A method of analyzing the durability of a structure. Load-controlled testing is performed on samples of a composite material of the structure to relate critical strain invariants of the material to cyclic rates of strain invariant accumulation and frequencies associated with the cyclic rates. The material is characterized based on effective properties of the material, including the cyclic rates of strain invariant accumulation. Laminate properties and a geometrical definition of the structure are used to obtain a parametric model. Material characterizations are used to determine model element frequency responses to applied load conditions. Each element's frequency responses and critical strain invariants are used to determine whether damage is indicated at the element. Progression of damage is tracked and accounted for in the model.


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