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:
Jan. 25, 2022

Filed:

May. 06, 2013
Applicant:

Airbus Operations Gmbh, Hamburg, DE;

Inventors:

Niko Naumann, Hamburg, DE;

Michaela Willamowski, Hamburg, DE;

Assignee:

Airbus Operations GmbH, Hamburg, DE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B29C 43/20 (2006.01); B29C 33/12 (2006.01); B29C 70/46 (2006.01); B32B 37/00 (2006.01); B32B 37/10 (2006.01); B29C 70/54 (2006.01); B29C 43/58 (2006.01); B32B 37/20 (2006.01); B32B 37/08 (2006.01); B64F 5/10 (2017.01);
U.S. Cl.
CPC ...
B29C 33/12 (2013.01); B29C 43/203 (2013.01); B29C 43/58 (2013.01); B29C 70/46 (2013.01); B29C 70/543 (2013.01); B32B 37/0007 (2013.01); B32B 37/10 (2013.01); B32B 37/08 (2013.01); B32B 37/203 (2013.01); B32B 2305/07 (2013.01); B32B 2309/02 (2013.01); B32B 2309/10 (2013.01); B32B 2309/72 (2013.01); B32B 2605/18 (2013.01); B64F 5/10 (2017.01); Y02T 50/40 (2013.01);
Abstract

A method for producing an aircraft structural component includes the steps of introducing a plurality of semi-finished product layers for producing a component from a fibre-reinforced, thermoplastic plastic material into a compression mould, applying pressure to the stacked semi-finished product layers, the stacked semi-finished product layers being fixed, before pressure is applied, at particular points in their position in the compression mould and/or relative to one another in such a way that, while pressure is being applied to the semi-finished product layers stacked in the compression mould, a sliding movement of the semi-finished product layers relative to one another and/or relative to the compression mould, preventing wrinkling in the semi-finished product layers, takes place, and removing the aircraft structural component from the compression mould.


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