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:
Sep. 10, 2019
Filed:
Mar. 27, 2013
Applicant:
Airbus Operations Gmbh, Hamburg, DE;
Inventors:
Wolf-Dietrich Dolzinski, Ganderkesee, DE;
Michael Kolax, Hamburg, DE;
Assignee:
Airbus Operations GmbH, Hamburg, DE;
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 1/12 (2006.01); B29C 70/08 (2006.01); B29C 70/86 (2006.01); B29D 99/00 (2010.01); B29C 65/62 (2006.01); B32B 7/08 (2019.01); B29C 65/48 (2006.01); B29C 65/56 (2006.01); B29C 65/72 (2006.01); B29C 65/00 (2006.01); B32B 5/06 (2006.01); B32B 5/18 (2006.01); B32B 5/24 (2006.01); B32B 3/06 (2006.01); B32B 3/08 (2006.01); B29C 70/24 (2006.01); B29K 105/04 (2006.01); B29L 31/30 (2006.01); B64C 1/00 (2006.01);
U.S. Cl.
CPC ...
B64C 1/12 (2013.01); B29C 65/483 (2013.01); B29C 65/564 (2013.01); B29C 65/62 (2013.01); B29C 65/72 (2013.01); B29C 66/1122 (2013.01); B29C 66/45 (2013.01); B29C 66/472 (2013.01); B29C 66/721 (2013.01); B29C 66/727 (2013.01); B29C 66/72141 (2013.01); B29C 70/086 (2013.01); B29C 70/24 (2013.01); B29C 70/865 (2013.01); B29D 99/0017 (2013.01); B32B 3/06 (2013.01); B32B 3/08 (2013.01); B32B 5/06 (2013.01); B32B 5/18 (2013.01); B32B 5/245 (2013.01); B32B 7/08 (2013.01); B29C 66/5326 (2013.01); B29C 66/71 (2013.01); B29C 66/7212 (2013.01); B29C 66/72525 (2013.01); B29C 66/7392 (2013.01); B29C 66/7394 (2013.01); B29K 2105/04 (2013.01); B29L 2031/3082 (2013.01); B32B 2260/021 (2013.01); B32B 2260/046 (2013.01); B32B 2307/102 (2013.01); B32B 2307/304 (2013.01); B32B 2307/50 (2013.01); B32B 2605/18 (2013.01); B64C 2001/0072 (2013.01); Y02T 50/43 (2013.01); Y10T 428/24496 (2015.01);
Abstract
A structural component for an aircraft or spacecraft, comprising: a planar member; a reinforcing member which projects from the planar member and is rigidly connected thereto; the reinforcing member comprising at least a foam layer and a cover layer, a plurality of pins extending at least through the foam layer and the cover layer, and at least the pins and the cover layer comprising a curable matrix.