Airbus Operations Gmbh

Airbus Deutschland Gmbh

Sven Werner

Wolfgang Eilken

Memis Tiryaki

Andre Zybala

Marco Pacchione

Torsten Noebel

Bernd Raeckers

Armin Fangmeier

André Zybala

Bernd Schwing

Christian Kulik

Christian Frank

Daniela Lohwasser

Bernd Räckers

Andreas Behr

Axel Bonde

Manos Troulis

A rail for the fastening of equipment elements, such as, in particular, seats, in aircraft, includes a holding region for connection to an equipment element of an aircraft, and a support region to fasten the rail to a carrier element of the aircraft. The rail has a metallic shell which is, for example, made of titanium and which is filled with a fiber-reinforced thermoplastic filler material which is reinforced by short fibers. To produce the rail, a metallic molded part is used as a casting mold and is filled, for example by injection, with the filler material and, after the rail has been produced, forms the metallic shell for the filler material.

Rail for the fastening of equipment elements in aircraft, in particular seats, and method for production

A seat rail assembly for fastening a seat assembly in a vehicle and a method for making such a seat rail assembly are described. The seat rail assembly includes a seat rail configured to fasten the seat assembly, the seat rail including a metal material. A fastening profile element of the seat rail assembly is configured to receive the seat rail, the fastening profile element being formed of a plastic material. The fastening profile element forms a receiving region, which is configured to receive the seat rail, and the seat rail includes a seat rail crown which is arranged in the receiving region of the fastening profile element such that a wall portion of the fastening profile element at least partly extends around the seat rail crown. The seat rail assembly may be used in an aircraft.

Seat rail assembly for fastening a seat assembly in a vehicle, use of a seat rail assembly of this type in an aircraft, and method for producing a seat rail assembly

A floor system for creating a floor in an interior of a vehicle has base part and a floor panel. The base part having a trough-shaped depression and the floor panel are attached to a floor support structure and together provide a customary installation height and also cavities for accommodating installation objects.

Floor system for a vehicle

A rail system for fixing fittings in a cabin of a vehicle includes a first elongate rail body with a fixing side for fixing to a vehicle structure, an opposite support side with a support surface for receiving fittings, and a rail cross-section extending between the fixing side and the support side, and several fixing inserts which can be fixed along the support surface. The rail cross-section has two mutually opposing legs which are spaced apart from each other and run perpendicularly to the support surface, and the fixing inserts are configured so as not to protrude beyond the support surface.

Rail systems for fixing fittings in a cabin of a vehicle

A method for manufacturing a load bearing structure involves providing a panel; providing a first set of split stiffening elements on a surface of the panel, wherein the split stiffening elements of the first set have bottom surfaces and central portions with open top clearances, respectively, spaced apart from each other; providing a second set of stiffening elements having bottom surfaces and top surfaces and central portions, respectively; inserting the stiffening elements of the second set into respective open top clearances of the split stiffening elements of the first set and providing the second set of stiffening elements on the surface of the panel for forming a grate structure; and attaching top surfaces to the split stiffening elements of the first set for forming complete profiles.

Method for manufacturing a load bearing structure and such a load bearing structure

A fuselage structure comprises a plurality of elements that in longitudinal direction are interconnected by weld joints; a plurality of circumferential ribs that are connected to the plurality of elements and that extend so as to be substantially perpendicular in relation to the longitudinal direction of the elements; and a plurality of clips that are arranged between the elements and the ribs such that said clips do not cover the respective weld joints.

Fuselage structure

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Sven Werner