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:
Apr. 04, 2023

Filed:

Aug. 29, 2019
Applicant:

Airbus Operations Gmbh, Hamburg, DE;

Inventors:

Peter Linde, Hamburg, DE;

Norbert Heltsch, Hamburg, DE;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B29C 64/165 (2017.01); B33Y 10/00 (2015.01); B33Y 80/00 (2015.01); B29C 64/118 (2017.01); B29C 70/38 (2006.01); B33Y 70/10 (2020.01); B29L 31/30 (2006.01); B29K 101/12 (2006.01);
U.S. Cl.
CPC ...
B29C 64/165 (2017.08); B29C 64/118 (2017.08); B29C 70/38 (2013.01); B33Y 10/00 (2014.12); B33Y 70/10 (2020.01); B33Y 80/00 (2014.12); B29K 2101/12 (2013.01); B29L 2031/3082 (2013.01);
Abstract

A method for manufacturing a fuselage component for an aircraft includes building up, on a surface of a two-dimensional shell part composed of a fibre composite material, stiffening profiles crossing at an intersection from a plurality of layers, superimposed on one another in a thickness direction, which are each formed by applying filaments, which each comprise a fibre bundle embedded in a thermoplastic material. Stabilising layers, within which the filaments extend beyond the intersection, are formed from the filaments in each of the stiffening profiles. A fuselage component and an aircraft, which comprises at least one such fuselage component, are furthermore described.


Find Patent Forward Citations

Loading…