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:
May. 02, 2017

Filed:

May. 27, 2014
Applicant:

Airbus Operations Gmbh, Hamburg, DE;

Inventors:

Paul Joern, Hamburg, DE;

Markus Mueller, Hamburg, DE;

Assignee:

Airbus Operations GmbH, Hamburg, DE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 1/12 (2006.01); B64C 1/06 (2006.01); B29C 65/48 (2006.01); B29C 65/56 (2006.01); B29C 65/62 (2006.01); B29C 65/72 (2006.01); B29C 65/00 (2006.01); B29C 70/24 (2006.01); B29D 99/00 (2010.01); B32B 7/08 (2006.01); B32B 37/00 (2006.01); B29L 31/30 (2006.01); B64C 1/00 (2006.01); B32B 38/00 (2006.01);
U.S. Cl.
CPC ...
B64C 1/06 (2013.01); B29C 65/48 (2013.01); B29C 65/562 (2013.01); B29C 65/62 (2013.01); B29C 65/72 (2013.01); B29C 66/1122 (2013.01); B29C 66/474 (2013.01); B29C 66/721 (2013.01); B29C 70/24 (2013.01); B29D 99/0014 (2013.01); B32B 7/08 (2013.01); B32B 37/00 (2013.01); B64C 1/12 (2013.01); B29C 66/7212 (2013.01); B29C 66/72141 (2013.01); B29C 66/73752 (2013.01); B29L 2031/3076 (2013.01); B32B 2038/008 (2013.01); B32B 2038/0052 (2013.01); B64C 2001/0072 (2013.01); Y02T 50/433 (2013.01); Y10T 428/24281 (2015.01);
Abstract

A segment and a method for producing such a segment, in particular for an aircraft, having a skin field and a skin field stiffening structure. The skin field and stiffening structure are made from fiber-reinforced plastic materials. The stiffening structure is bonded to an inner surface of the skin field and comprises a multiplicity of first stiffeners and mounts which are formed integrally with the first stiffeners and extend in a transverse direction of the first stiffeners for the connection of second stiffeners to form an integral lattice structure. Reinforcement elements are provided for mechanically fixing the mounts to the skin field. Each reinforcement element has a connection section and a blocking section having an extension in a direction inclined to the connection section. The connection section penetrates the skin field and the mounts, and the blocking section is in contact with an outer surface of the skin field.


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