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. 02, 2024

Filed:

Mar. 12, 2021
Applicant:

Airbus Operations Gmbh, Hamburg, DE;

Inventor:

Paul Jörn, Hamburg, DE;

Assignee:

AIRBUS OPERATIONS GMBH, Hamburg, DE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B29C 70/46 (2006.01); B29C 70/08 (2006.01); B64C 1/00 (2006.01); B32B 5/02 (2006.01); B32B 5/12 (2006.01); B32B 27/12 (2006.01); B32B 15/14 (2006.01); B32B 15/08 (2006.01); B32B 15/20 (2006.01); B29K 101/12 (2006.01); B29K 71/00 (2006.01); B29L 31/30 (2006.01);
U.S. Cl.
CPC ...
B29C 70/465 (2013.01); B29C 70/086 (2013.01); B32B 5/024 (2013.01); B32B 5/12 (2013.01); B32B 15/08 (2013.01); B32B 15/14 (2013.01); B32B 15/20 (2013.01); B32B 27/12 (2013.01); B64C 1/00 (2013.01); B29K 2065/00 (2013.01); B29K 2071/00 (2013.01); B29K 2101/12 (2013.01); B29L 2031/3076 (2013.01); B32B 2250/20 (2013.01); B32B 2260/023 (2013.01); B32B 2260/046 (2013.01); B32B 2262/106 (2013.01); B32B 2605/18 (2013.01); B64C 2001/0072 (2013.01); Y10T 442/3447 (2015.04);
Abstract

A textile fiber-composite material precursor and method for producing a component from fiber-composite material. Aircraft components can be produced from polymer fiber-composite materials, a matrix of which can be a high-performance plastics material such as polyether ketone ketone wherein a reinforcement of a non-crimp fabric of carbon fibers is embedded. Large-area non-crimp fabrics and large-area polymer films can be consolidated while being heated and pressed forming simple components. The flexible textile fiber-composite material precursor includes a stack of woven-fabric tiers from a polymer and of non-crimp fabric tiers from carbon fibers. Since both components are capable of draping, the fiber-composite material precursor can be deposited over a large area on curved shape-imparting surfaces and subsequently be consolidated under pressure and heated to form the fiber-composite material.


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