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:
Dec. 20, 2022

Filed:

Aug. 01, 2019
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Davis Tran, Seattle, WA (US);

Richard Jameson Langabeer, Jr., Everett, WA (US);

Weidong Song, Woodinville, WA (US);

Assignee:

THE BOEING COMPANY, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B29C 70/50 (2006.01); B64F 5/10 (2017.01); B64C 3/18 (2006.01); B29K 63/00 (2006.01); B29K 307/04 (2006.01); B29L 31/30 (2006.01);
U.S. Cl.
CPC ...
B29C 70/50 (2013.01); B64C 3/182 (2013.01); B64F 5/10 (2017.01); B29K 2063/00 (2013.01); B29K 2307/04 (2013.01); B29L 2031/3085 (2013.01);
Abstract

A method for fabricating a composite wing structural component for an aircraft is described. The method comprises extruding a filler material into each mold channel of a plurality of mold channels of a die to form a plurality of filler segments, removing the plurality of filler segments from the plurality of mold channels of the die, and arranging the plurality of filler segments in a space in the composite structural component, the space being defined by a radius of the composite structural component, such that the filler segments are in end-to-end contact. The method further comprises curing the plurality of filler segments in the space to fuse the plurality of filler segments.


Find Patent Forward Citations

Loading…