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:
Feb. 25, 2020

Filed:

Sep. 24, 2018
Applicant:

Airbus Operations Gmbh, Hamburg, DE;

Inventor:

Manuel Jung, Hamburg, DE;

Assignee:

AIRBUS OPERATIONS GMBH, Hamburg, DE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 3/18 (2006.01); B29C 65/54 (2006.01); B29C 65/48 (2006.01); B29C 65/00 (2006.01); B29C 70/30 (2006.01); B29C 70/44 (2006.01); B29D 99/00 (2010.01); B29L 31/30 (2006.01); B29L 31/00 (2006.01); B29C 70/36 (2006.01); B29C 65/50 (2006.01); B64C 1/12 (2006.01);
U.S. Cl.
CPC ...
B29C 65/54 (2013.01); B29C 65/483 (2013.01); B29C 66/1312 (2013.01); B29C 66/721 (2013.01); B29C 70/30 (2013.01); B29C 70/446 (2013.01); B29D 99/0003 (2013.01); B29D 99/0007 (2013.01); B64C 3/182 (2013.01); B29C 65/4815 (2013.01); B29C 65/5014 (2013.01); B29C 65/546 (2013.01); B29C 66/5241 (2013.01); B29C 66/54 (2013.01); B29C 66/7212 (2013.01); B29C 66/73921 (2013.01); B29C 66/73941 (2013.01); B29C 70/36 (2013.01); B29C 70/443 (2013.01); B29L 2031/003 (2013.01); B29L 2031/3076 (2013.01); B29L 2031/3085 (2013.01); B32B 2605/18 (2013.01); B64C 1/12 (2013.01); Y10T 428/24182 (2015.01);
Abstract

A fiber composite component having a first and a second fiber composite element each bent along a transverse axis opf the fiber composite component to have, respectively, in succession, a first and second base flange, a first and second web section, a first and second top flange and a first and second stiffening web. Respectively, the first and second base flanges are parallel to the first and second top flanges, the first and second web sections are angled with respect to each of the first and second base flanges and the first and second top flanges, the first and second stiffening webs are at right angles with respect to the first and second top flanges, and the first stiffening web and the second stiffening web are congruent with respect to one another, and are connected to one another, along a longitudinal axis of the fiber composite component.


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