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:
Sep. 19, 2017

Filed:

Sep. 16, 2014
Applicant:

Airbus Operations Gmbh, Hamburg, DE;

Inventors:

Hermann Benthien, Sottrum, DE;

Cord Haack, Beckdorf, DE;

Andreas Poppe, Reeβum, DE;

Michael Burrichter, Stuhr-Brinkum, DE;

Torsten Abraham, Hildesheim, DE;

Michael Brinckmann, Bremen, DE;

Christoph Dierker, Bremen, DE;

Frank Werth, Stuhr, DE;

Wulf Bindewald, Syke, DE;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 1/26 (2006.01); B64C 1/06 (2006.01);
U.S. Cl.
CPC ...
B64C 1/068 (2013.01); B64C 1/26 (2013.01);
Abstract

An aircraft fuselage structure is disclosed herein and includes an outer skin, with circumferential ribs, such that a recess is provided for receiving a wing torsion box in the outer skin, and the ribs are interrupted in the region of the recess. An object of the disclosure includes providing an aircraft fuselage structure designed such that the wing torsion box is able to extend at least partially through the upper region of the fuselage, without the stability of the fuselage being significantly reduced. This can include providing first longitudinal members which are adjacent to the recess and which extend along the longitudinal edges beyond the entire length thereof. End regions of the first longitudinal members are connected to ribs which extend circumferentially at intervals from the transverse edges of the recess along the outer skin over the vertical longitudinal central plane.


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