Airbus Operations Gmbh

Fraunhofer-gesellschaft Zur Foerderung Der Angewandten Forschung E.v.

Thomas Lemckau

Armin Fangmeier

Rouven Kott

Peter Plagemann

Andreas Brinkmann

Anja Zockoll

Simone Schroder

Simone Schroeder

Sönke Harders

Sophie Kerchnawe

A component made of carbon fiber reinforced plastic is described, consisting of or comprising a matrix material (M) and carbon fibers embedded into the matrix material (M), wherein the component has at least one surface portion (A), having one or a plurality of exposed regions of the carbon fibers, characterized in that the exposed regions(s) of the carbon fibers is or are selectively coated with a layer (S). A process for producing such a component and also an assembly comprising such a component and one or a plurality of further components comprising or consisting of a material such as steel, iron, copper, magnesium or aluminum or alloys thereof are also described.

Selectively coated CRP components and process for the production thereof

A process of repairing defects on a carbon fiber reinforced plastic (CFRP) component wherein defects on a surface of a CFRP component are selectively repaired by electrodeposition coating. With this process a reduction of coating material and work force as well as weight of the repaired CFRP component can be achieved.

Process for selective isolation of CFRP parts by electrodeposition coatings

Disclosed is a method for placing fiber-reinforced, pre-impregnated, planar semi-finished products on a placement tool for the manufacture of a non-crimp fabric, wherein a placement film is clamped on the placement tool for purposes of holding the non-crimp fabric, and by means of evacuation and/or the application of pressure is fixed in position on the placement tool and/or can be released from the latter. Also disclosed is a placement tool for the execution of such a method.

Method and a placement tool for the manufacture of a non-crimp fabric

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Buxtehude, Germany

Thomas Lemckau