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:
Mar. 10, 2015

Filed:

Apr. 07, 2011
Applicants:

Nikolaus Ohrloff, Buxtehude, DE;

Thomas Beumler, Jork, DE;

Derk Daverschot, Bremen, DE;

Matthijs Plokker, Harsefeld, DE;

Inventors:

Nikolaus Ohrloff, Buxtehude, DE;

Thomas Beumler, Jork, DE;

Derk Daverschot, Bremen, DE;

Matthijs Plokker, Harsefeld, DE;

Assignee:

Airbus Operations GmbH, Hamburg, DE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B32B 3/00 (2006.01); B32B 5/00 (2006.01); B64C 1/00 (2006.01); B64C 1/06 (2006.01); B64C 1/12 (2006.01);
U.S. Cl.
CPC ...
B64C 1/065 (2013.01); B64C 1/12 (2013.01); B64C 2001/0072 (2013.01); Y02T 50/433 (2013.01); Y02T 50/43 (2013.01);
Abstract

A structural element for reinforcing a fuselage cell of an aircraft is provided. The structural element comprises a reinforcement profile which is made in one piece from a metallic material. The profile is provided with a strap at least in regions. As a result of the strap which is made of a fiber-reinforced layer material or fiber metal laminate and is adhesively bonded, at least in regions, to a flange of the reinforcement profile the structural element has high damage tolerance and advantageous fatigue properties. The fiber metal laminate or layer material is made of a plurality of metal layers and fiber-reinforced plastics material layers which are stacked in alternating fashion and adhesively bonded to one another over the entire surface. The reinforcement profile and the strap are joined by means of a joining layer. Said joining layer is preferably constructed from two prepreg layers and a non-fiber-reinforced adhesive layer.


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