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:
Aug. 13, 2019

Filed:

Nov. 01, 2016
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Lisa Carlson, Chicago, IL (US);

Kanna M. Pham, Renton, WA (US);

Joseph Sweetin, Chicago, IL (US);

Garrett C. Hanson, Mukilteo, WA (US);

Jake Adam Reeves, Seattle, WA (US);

Chilip Chan, Seattle, WA (US);

Kiet Nguyen, Seattle, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B29C 53/04 (2006.01); B29C 70/54 (2006.01); B29C 70/34 (2006.01); B64C 3/18 (2006.01); B29C 33/68 (2006.01); B29C 70/20 (2006.01); B29C 70/22 (2006.01); B29C 70/46 (2006.01); B29D 99/00 (2010.01); B64C 1/06 (2006.01); B29K 61/04 (2006.01); B29K 63/00 (2006.01); B29K 105/00 (2006.01); B29K 307/04 (2006.01); B29L 31/08 (2006.01);
U.S. Cl.
CPC ...
B29C 70/34 (2013.01); B29C 33/68 (2013.01); B29C 53/04 (2013.01); B29C 70/20 (2013.01); B29C 70/22 (2013.01); B29C 70/46 (2013.01); B29C 70/545 (2013.01); B29D 99/0003 (2013.01); B64C 3/18 (2013.01); B29D 99/0014 (2013.01); B29K 2061/04 (2013.01); B29K 2063/00 (2013.01); B29K 2105/256 (2013.01); B29K 2307/04 (2013.01); B29L 2031/082 (2013.01); B64C 1/064 (2013.01); B64C 3/182 (2013.01); Y10T 156/1044 (2015.01); Y10T 156/1049 (2015.01); Y10T 156/1051 (2015.01);
Abstract

An example method for forming a flat composite charge into a composite blade stiffener includes cutting a flat composite charge along a cut line into a first piece and a second piece having an angle, positioning the first piece and the second piece of the flat composite charge on a forming mandrel about a tooling plunger, activating the tooling plunger to drive the first piece and the second piece into a cavity of the forming mandrel resulting in the first piece and the second piece folding at the cut line, withdrawing the tooling plunger from the cavity of the forming mandrel, compressing the forming mandrel to apply a lateral pressure to the first piece and the second piece folded into the cavity, and applying a vertical pressure to a first flange and a second flange of the first piece and the second piece, respectively, to form the composite blade stiffener.


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