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.
Patent No.:
Date of Patent:
May. 21, 2019
Filed:
Aug. 23, 2014
Applicant:
The Boeing Company, Chicago, IL (US);
Inventors:
Douglas A. McCarville, Orting, WA (US);
Juan C. Guzman, Seattle, WA (US);
Michael L. Hand, Huntington Beach, CA (US);
Assignee:
The Boeing Company, Chicago, IL (US);
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B29C 65/48 (2006.01); B32B 3/20 (2006.01); B29C 65/50 (2006.01); B29C 65/00 (2006.01); B64C 1/06 (2006.01); B32B 3/06 (2006.01); B29L 31/30 (2006.01); B29L 31/00 (2006.01); B64C 1/00 (2006.01); B29L 24/00 (2006.01);
U.S. Cl.
CPC ...
B32B 3/20 (2013.01); B29C 65/505 (2013.01); B29C 66/1122 (2013.01); B29C 66/1142 (2013.01); B29C 66/1162 (2013.01); B29C 66/301 (2013.01); B29C 66/43 (2013.01); B29C 66/496 (2013.01); B29C 66/543 (2013.01); B29C 66/547 (2013.01); B29C 66/636 (2013.01); B29C 66/721 (2013.01); B29C 66/72523 (2013.01); B32B 3/06 (2013.01); B64C 1/069 (2013.01); B29C 65/4835 (2013.01); B29C 66/432 (2013.01); B29C 66/435 (2013.01); B29C 66/438 (2013.01); B29C 66/81455 (2013.01); B29C 66/919 (2013.01); B29C 66/91411 (2013.01); B29C 66/929 (2013.01); B29L 2024/006 (2013.01); B29L 2031/3082 (2013.01); B29L 2031/3097 (2013.01); B29L 2031/7172 (2013.01); B32B 2605/00 (2013.01); B32B 2605/18 (2013.01); B64C 2001/0072 (2013.01); Y02T 50/43 (2013.01); Y10T 428/13 (2015.01); Y10T 428/19 (2015.01);
Abstract
Fluted core sandwich panels are joined together to form a composite structure. Variations in panel ends are accommodated by a core stiffener insert installed in a joint between ends of the panels.