Airbus Defence and Space Gmbh

Airbus Operations Gmbh

Neotech Amt Gmbh

Nils Ischdonat

Patrick Rollfink

Rolf Bense

Martin Hedges

Benedikt Schmidt-Kortenbusch

Fabian Reimer

Melanie Stoob

Daniel Graef

Thomas Reitberger

Leonardo Wulfhorst

A cabin structural component for a transport vehicle, in particular for an aircraft or spacecraft, has a sandwich structure that has a core and a first cover layer, the first cover layer being provided with a heat conductor that is arranged and designed for heating a cabin wall that can be produced using the cabin structural component.

Cabin structural component, method for producing a cabin structural component, cabin assembly and transport vehicle

A device for fixing and electrical contacting of a facing element of an aircraft on a support structure, which is attached to an aircraft structure including a fixing device for detachable fixation of the facing element on the support structure and a contacting device for providing multiple electrical contacts between facing element leads and connecting leads on the support structure, wherein the fixing device can be placed into positive engagement by a transitory relative movement between the facing element and the support structure, and the contacting device includes at least two first contacts on the facing element and the same number of second contacts on the support structure cooperating therewith, which can be respectively brought into contact with one another electrically during the transitory relative movement, wherein the first contacts are connected with the facing element leads and the second contacts are connected with the connecting leads on the support structure.

Device for fixing and electrical contacting a facing element of an aircraft on a support structure

The invention relates to a device comprising a base plate and a support for adjusting the height of an assembly, in particular of a galley module in an aircraft, without using tools. According to the invention, two opposing wedge bodies are arranged such that they can be displaced horizontally between the base plate and the support, the oppositely directed manual displacement of the two wedge bodies, when the lock levers have been raised, causes in the 'adjusting position' a raising or lowering of the support for the height adjustment. The assembly is connected to the support, for example by a conventional screw connection through the attachment hole in the support. The device according to the invention allows a user to perform a simple and rapid height adjustment of an assembly arranged thereon, thereby greatly reducing the assembly effort required for prefabricated assemblies or modules in aircraft.

Device for adjusting the height of an assembly without the use of tools

Growing community of inventors

Hamburg, Germany

Nils Ischdonat