Diehl Aerospace Gmbh

Diehl Aircabin Gmbh

Airbus Operations Gmbh

Markus Klingseis

Frank Schmid

Marc Renz

Wolf-Dieter Kuhnla

Norbert Knopp

Dietmar Völkle

Jürgen Grabmann

Dirk-Achim Schevardo

Christian Wesselink

Dietmar Voelkle

Ralph Pätzold

Martin Geldien

Peter Younes

Tobias Gauggel

Juergen Grabmann

The description covers cabin components for aircraft, which can be produced with a sandwich structure and may have the componentsfor signal and/or power transmission. The cabin components in this case have at least two prepreg layersand, for example, a honeycomb layer, which can be connected to one another by pressing and heating. Furthermore, electrical and/or optical signal paths are shown on cabin components, which can be produced by positioning them there or printing. In addition, according to the description, signal and/or power transmission can take place beyond the boundary of cabin components, by means of a transmitter/receiver path.

Elements for signal and/or power transmission into or to cabin components

An internal device arrangement for a passenger cabin, for example of an aircraft, is provided. The device has an internal device element which is selected from a group including wall paneling, window panel, side panel, ceiling paneling and luggage compartment. The device has an electrical apparatus fitted in or on the internal device element; and at least one line for supplying power to the electrical apparatus. Furthermore, a heat dissipation device in the form of an integral component part of the internal device element, the electrical apparatus and/or the at least one line is provided. Such a heat dissipation device makes it possible to dispense with an additional heat sink for temperature management and thus save installation space and weight.

Internal device arrangement for a passenger cabin

Corresponding to reducing the number of components that need to be separately installed, in addition to a weight reduction and a reduction in the cable loom volume, improved system reliability is obtained if the loads relating to a seating space in a passenger cabin (), in particular in an aircraft, are combined on an overhead panel () which is connected, via line connections which are now only short, to a spatially associated supply module (), which is operated in cutouts () in a stub frame (), in order to anchor a hat rack () in the fuselage structure () of the cabin ().

Device for supplying loads in the overhead area of a passenger cabin, in particular in commercial aircraft

According to an exemplary embodiment of the invention, a combined habitation module for the crew of an aircraft is provided, which habitation module comprises two monument units that are separated from each other by a gap such that acoustic decoupling of the two monument units from each other is provided. In this way noise propagation within the habitation module may be prevented to a large extent.

Integrated acoustic decoupling in a habitation module

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Biberach, Germany

Markus Klingseis