Airbus Operations Gmbh

Carsten Rowedder

Alexander Gillessen

Ichwan Zuardy

Karim Grase

Johannes Born

Markus Mueller

M Ichwan Zuardy

Claas De Jong

Mathias Jessrang

In a method for producing a rail-shaped hybrid component, in particular for an aircraft or spacecraft, a second rail component made of a titanium material is positioned on a first bar of a first profile rail that is made of a carbon-fiber reinforced plastic material and moved in an advancing direction, in a fixed position relative to the first profile rail, such that a bar portion of the first bar is arranged between a first connecting portion of the second rail component and a second connecting portion of the second rail component, and the second rail component is cohesively connected to the first profile rail. Furthermore, the hybrid component has a first profile rail made of a carbon-fiber reinforced plastic material and a second rail component made of a titanium material.

Method for producing a rail-shaped hybrid component, and such a hybrid component

A pressure bulkhead of an aircraft with a fuselage shell and a pressure bulkhead disposed therein preferably in the rear region for forming a fuselage-internal pressure region, which pressure bulkhead is attached on the edge in the interior of the fuselage shell, wherein the pressure bulkhead has a lenticular cross-section and a sandwich construction that comprises a foam core sandwiched between two opposing exterior shells.

Pressure fuselage of an aircraft with a fuselage shell and a pressure bulkhead disposed therein

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Hamburg, Germany

Carsten Rowedder