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. 13, 2017

Filed:

Mar. 09, 2015
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Lyle R. Deobald, Shoreline, WA (US);

Kenneth L. Brook, Seattle, WA (US);

Timothy D. Jackson, Everett, WA (US);

Kenneth J. Duffie, Mercer Island, WA (US);

Gregory B. Doty, Edmonds, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 1/06 (2006.01); B64C 1/12 (2006.01); B29D 99/00 (2010.01); B29C 70/30 (2006.01); B64C 3/18 (2006.01); B64C 3/20 (2006.01); B64C 3/26 (2006.01); B32B 37/18 (2006.01); B32B 38/00 (2006.01); B64C 1/00 (2006.01);
U.S. Cl.
CPC ...
B64C 1/12 (2013.01); B29C 70/30 (2013.01); B29D 99/0014 (2013.01); B32B 37/18 (2013.01); B32B 38/0004 (2013.01); B64C 1/064 (2013.01); B64C 3/182 (2013.01); B64C 3/20 (2013.01); B64C 3/26 (2013.01); B32B 2607/00 (2013.01); B64C 2001/0072 (2013.01); Y02T 50/433 (2013.01); Y10T 156/1062 (2015.01); Y10T 156/1064 (2015.01); Y10T 428/24174 (2015.01); Y10T 428/24182 (2015.01);
Abstract

The disclosure herein provides for disbond resistant stringer runouts. Various aspects may be used independently or in combination to mitigate disbonding associated with the stiffener runout under operational loads. Aspects include a stiffener runout having rounded base flange corners. A recessed notch may be incorporated within the base flange to provide a flange termination point that is forward of the web termination point, allowing the web to terminate prior to the base flange. The web may be trimmed from a full height to a reduced height at the web termination point. The base flange may be co-bonded to the underlying composite structure via a scarf joint. Perimeter clamp radius fillers may be used to concentrate a clamping force around the perimeter of the base flange.


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