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. 05, 2019

Filed:

Jan. 02, 2015
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Vladimir Balabanov, Mukilteo, WA (US);

Olaf Weckner, Seattle, WA (US);

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

Abdelhai Maysara Saadi, Snohomish, WA (US);

Mostafa Rassaian, Bellevue, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B32B 5/12 (2006.01); B32B 5/02 (2006.01); G06F 17/18 (2006.01); G06F 17/50 (2006.01);
U.S. Cl.
CPC ...
B32B 5/12 (2013.01); B32B 5/02 (2013.01); G06F 17/18 (2013.01); G06F 17/50 (2013.01); G06F 17/5009 (2013.01); G06F 17/5018 (2013.01); B32B 2250/20 (2013.01); B32B 2307/544 (2013.01); B32B 2307/546 (2013.01); B32B 2605/18 (2013.01); Y10T 428/24504 (2015.01);
Abstract

Composite skin-stringer structures which reduce or eliminate the risk of delamination at the skin-stringer interface. This can be accomplished by arranging ply directions (i.e., the angles of the fiber paths of the ply) in a layup in a way such that for the dominant loading, the skin and stringer will each deform in a way that reduces relative opening (fracture Mode I) and/or sliding (fracture Mode II) and/or scissoring (fracture Mode III) at the skin-stringer interface. This is possible when coupling between specific deformations modes is purposefully activated instead of being suppressed. The ply directions in the stringer are adjusted so that the stringer deforms in a controlled fashion to suppress or 'close' cracks that are about to form—before the undesirable modes of failure form—as load is applied.


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