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. 27, 2023

Filed:

May. 04, 2020
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Forouzan Behzadpour, Mukilteo, WA (US);

Waeil M. Ashmawi, Bellevue, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 1/06 (2006.01); B29C 70/30 (2006.01); B29C 70/54 (2006.01); B29C 65/48 (2006.01); B29C 65/00 (2006.01); B29C 53/02 (2006.01); B29L 31/30 (2006.01); B64C 1/00 (2006.01);
U.S. Cl.
CPC ...
B64C 1/064 (2013.01); B29C 53/02 (2013.01); B29C 65/48 (2013.01); B29C 66/729 (2013.01); B29C 70/30 (2013.01); B29C 70/545 (2013.01); B29L 2031/3076 (2013.01); B64C 2001/0072 (2013.01);
Abstract

Described herein are stringer assemblies, such as blade stringers, and methods of forming thereof. A stringer assembly comprises a first fabric composite stiffener, a second fabric composite stiffener, and an intermediate tape composite stiffener, disposed between and connected to each of the first and second stiffeners. Using three separate components allows forming sharp bends, eliminating voids and gap fillers, and adding new features, such as edge reinforcements. Each of the first and second fabric composite stiffeners comprises a web portion, a flange portion, and a curved portion, positioned between the web and flange portions. The web portions surround and are attached to the intermediate tape composite stiffener and, in some examples, include tapered-out edges for additional rigidity. The flange portions are attached to the composite base. The curved portions conform to the flared-out edges of the intermediate tape composite stiffener, which extends and connects to the composite base.


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