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:
Oct. 21, 2025

Filed:

Jul. 19, 2022
Applicant:

Airbus Operations Gmbh, Hamburg, DE;

Inventors:

Scott Clair, Hamburg, DE;

Andreas Jespersen, Hamburg, DE;

Paul Jörn, Hamburg, DE;

Norbert Heltsch, Hamburg, DE;

Assignee:

Airbus Operations GmbH, Hamburg, DE;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 1/12 (2006.01); B29C 70/22 (2006.01); B29C 70/30 (2006.01); B29K 105/00 (2006.01); B29K 105/10 (2006.01); B29L 31/30 (2006.01); B64C 1/00 (2006.01);
U.S. Cl.
CPC ...
B64C 1/12 (2013.01); B29C 70/22 (2013.01); B29C 70/30 (2013.01); B29K 2105/102 (2013.01); B29K 2105/253 (2013.01); B29L 2031/3082 (2013.01); B64C 2001/0072 (2013.01);
Abstract

A method for manufacturing a structural element for a fuselage of an aircraft. To improve the manufacture of structural elements, a method includes laying up textile material members on a mandrel to form a plurality of structural element preforms that are space apart along an extended direction of the mandrel. The structural element preforms form closed loops and are subsequently cured to obtain annular structural elements. The annular structural elements are used as basic building blocks for stiffening panel members or are directly used as structural frame elements reinforcing cut-outs in a fuselage for windows and/or doors.


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