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:
Dec. 16, 2025

Filed:

Feb. 11, 2025
Applicant:

Airbus Operations Gmbh, Hamburg, DE;

Inventors:

Thomas Beumler, Jork, DE;

Andreas Poppe, Reeßum, DE;

Assignee:

Airbus Operations GmbH, Hamburg, DE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 1/00 (2006.01); B32B 3/08 (2006.01); B32B 5/02 (2006.01); B32B 7/08 (2019.01); B32B 15/04 (2006.01); B32B 15/14 (2006.01); B32B 15/20 (2006.01); B32B 37/18 (2006.01); B62B 3/08 (2006.01);
U.S. Cl.
CPC ...
B64C 1/00 (2013.01); B32B 3/08 (2013.01); B32B 5/02 (2013.01); B32B 7/08 (2013.01); B32B 15/043 (2013.01); B32B 15/14 (2013.01); B32B 15/20 (2013.01); B32B 37/18 (2013.01); B32B 2250/44 (2013.01); B32B 2260/021 (2013.01); B32B 2262/101 (2013.01); B32B 2305/22 (2013.01); B32B 2311/24 (2013.01); B32B 2315/085 (2013.01); B32B 2605/18 (2013.01); B64C 2001/0072 (2013.01);
Abstract

An aircraft structure part having a stacked arrangement of layers with the layers being one of an at least first doubler and a basic layer of the outer skin of an aircraft fuselage, with the first doubler and the basic layer being bonded by a first intermediate bond film layer to form a step-shaped configuration of the aircraft structure part, wherein the first doubler includes a first fiber prepreg layer, in particular glass fiber prepreg layer, arranged at the perimeter of the first doubler and wherein the first fiber prepreg layer is bonded to the basic layer by at least one first bond-film segment deposited adjacent to the first fiber prepreg layer in a first wedge-shaped element at least partially incorporating the first fiber prepreg layer. A method is disclosed for providing an aircraft structure part and an aircraft fuselage provided with the aircraft structure part.


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