Airbus Operations Gmbh

Deutsches Zentrum Fuer Luft-und Raumfahrt E.v

Diehl Aircabin Gmbh

Diehl Aviation Laupheim Gmbh

Florian Hesselbach

Uwe Schneider

Andreas Baatz

Rainer Müller

Christian Thomas

Ralph Sturm

Norbert Staudigel

Dietmar Voelkle

Stephan Hötzeldt

Wilfried Michaelis

Tobias Lechner

Benjamin Joemann

Mathias Gruen

Benedict Michelis

Sven Utikal

Felix Werner

Tobias Dehne

Johannes Bosbach

Arno Berger

Daniela Büttner

A cladding element having a heating layer in a sandwich construction. In the case of a cladding element in a sandwich construction for an interior space of an aircraft, the cladding element includes a core layer and a first cover layer. The first cover layer forms a visible side of the cladding element. An electrically heating layer extends at least across a sub-face of the first cover layer and serves for generating heat for emission through the first cover layer is disposed between the core layer and the first cover layer.

Cladding element having a heating layer in a sandwich construction

The invention relates to a cabin air inlet module (). The cabin air inlet module () comprises a streaming channel body (). The streaming channel body () comprises at least one wall which limits a streaming channel wherein incoming air () is supplied to a zone () of a cabin (). The cabin air inlet module () comprises an electric heating element () which is used for heating the incoming air (). According to the invention it is proposed that the electric heating element () is embodied as a two-dimensional heating element (in particular as a heating paper, a heating web, a heating foil or a heating varnish). The two-dimensional heating element extends along a wall of the streaming channel body (). The inventive cabin air inlet module () is arranged upstream with a small distance () from an inlet opening () into the zone () of the cabin (). The inventive cabin air inlet module () is used for a tempering zones () of a cabin () of an airplane according to the needs.

Cabin air inlet module and cabin air system

A coating method wherein in order to simplify the coating method and increase the flexibility thereof with respect to respective desired coatings, provision is made that a powder lacquer layer () is applied to a surface () of the component (), and an imprint () is applied to the powder lacquer layer (), preferably by an inkjet method.

Component having coating and coating method

Growing community of inventors

Blaustein, Germany

Florian Hesselbach