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:
Jan. 29, 2019

Filed:

Nov. 03, 2015
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Nick S. Evans, Lynnwood, WA (US);

Faraón Torres, Seattle, WA (US);

Ryan G. Ziegler, Mill Creek, WA (US);

Samuel F. Harrison, Bothell, WA (US);

Ciro J. Grijalva, III, Seattle, WA (US);

Hayden S. Osborn, Seattle, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B05D 1/34 (2006.01); B33Y 70/00 (2015.01); B29C 69/00 (2006.01); B29C 70/28 (2006.01); B05D 1/26 (2006.01); B05D 3/06 (2006.01); B05D 3/12 (2006.01); B29C 35/16 (2006.01); B29C 70/16 (2006.01); B29C 70/38 (2006.01); B29C 70/54 (2006.01); C09D 5/00 (2006.01); B29B 11/00 (2006.01); B29B 11/16 (2006.01); C09D 201/00 (2006.01); B29C 47/00 (2006.01); B29C 64/106 (2017.01); B29K 105/00 (2006.01); B33Y 10/00 (2015.01); B29L 31/30 (2006.01); B29L 31/00 (2006.01); B33Y 30/00 (2015.01); B33Y 40/00 (2015.01); B29K 63/00 (2006.01); B29K 105/08 (2006.01); B29K 105/10 (2006.01); B33Y 50/02 (2015.01); B29K 101/10 (2006.01); B29K 105/12 (2006.01); B29C 35/08 (2006.01); B29K 105/06 (2006.01); B29C 64/135 (2017.01); B29C 64/129 (2017.01); B29C 64/25 (2017.01);
U.S. Cl.
CPC ...
B33Y 70/00 (2014.12); B05D 1/265 (2013.01); B05D 1/34 (2013.01); B05D 3/06 (2013.01); B05D 3/067 (2013.01); B05D 3/068 (2013.01); B05D 3/12 (2013.01); B29B 11/00 (2013.01); B29B 11/16 (2013.01); B29C 35/16 (2013.01); B29C 47/0002 (2013.01); B29C 64/106 (2017.08); B29C 69/001 (2013.01); B29C 70/16 (2013.01); B29C 70/28 (2013.01); B29C 70/38 (2013.01); B29C 70/545 (2013.01); C09D 5/00 (2013.01); C09D 201/00 (2013.01); B29C 35/0805 (2013.01); B29C 64/129 (2017.08); B29C 64/135 (2017.08); B29C 64/25 (2017.08); B29C 2035/0822 (2013.01); B29C 2035/0827 (2013.01); B29C 2035/0833 (2013.01); B29C 2035/0838 (2013.01); B29C 2035/0844 (2013.01); B29K 2063/00 (2013.01); B29K 2101/10 (2013.01); B29K 2105/0058 (2013.01); B29K 2105/06 (2013.01); B29K 2105/0872 (2013.01); B29K 2105/10 (2013.01); B29K 2105/101 (2013.01); B29K 2105/12 (2013.01); B29K 2105/25 (2013.01); B29K 2105/253 (2013.01); B29K 2995/005 (2013.01); B29L 2031/00 (2013.01); B29L 2031/3076 (2013.01); B33Y 10/00 (2014.12); B33Y 30/00 (2014.12); B33Y 40/00 (2014.12); B33Y 50/02 (2014.12);
Abstract

A method of additively manufacturing a composite part is disclosed. The method comprises pushing a continuous flexible line through a delivery guide. The continuous flexible line comprises a non-resin component and a thermosetting-epoxy-resin component that is partially cured. The method also comprises depositing, via the delivery guide, a segment of the continuous flexible line along a print path. The method further comprises maintaining the thermosetting-epoxy-resin component of at least the continuous flexible line being pushed through the delivery guide below a threshold temperature prior to depositing the segment of the continuous flexible line along the print path.


Find Patent Forward Citations

Loading…