Airbus Operations Gmbh

Mankiewicz Gebr. & Co. Gmbh & Co Kg

Fraunhofer-gesellschaft Zur Foerderung Der Angewandten Forschung E.v.

Airbus Deutschland Gmbh

Ottmar Schramm

Martin Kaune

Memis Tiryaki

Dominik Raps

Volkmar Stenzel

Nicole Jordan

Isabell Gradert

Wolfgang Papendick

Yvonne Wilke

Jan Kuever

Bernd Sasse

Tanja Pietzker

Carmen Gerlach

Matthias Geistbeck

Andreas Rabenstein

Diana Becker

Sven Schroeder

Hubertus Lohner

Sven Schröder

Gerlach Carmen,

Gerlach Carmen

Jan KÜVER

A hybrid support rail for receiving fixtures in a cabin of a vehicle includes a support rail base, first attachment elements, second attachment elements formed so as to be complementary to the first attachment elements, and a support rail upper part. The support rail base has a lower side and an upper side. The upper side has a receiving housing extending along a main extension direction of the support rail base for sliding in first attachment elements and, on a side facing away from the lower side, a support surface having at least one recess. The receiving housing is formed so as to prevent the first attachment elements from sliding out towards the support surface. The support rail upper part has a contact surface for placement on the support surface. The contact surface has recesses through which the second attachment elements are guided for insertion in the first attachment elements.

Hybrid support rail for receiving fixtures in a cabin of a vehicle

A method for coating a surface of an aircraft is provided. The method comprises the steps of cutting to size at least one film section from a shrinkable film material in such a manner that the film section relative to a surface section of the aircraft, which surface section is to be coated with the film section, comprises an overmeasure that is determined by the degree of shrinkage of the film material; applying the film section and a functional coating to the surface section so that the functional coating is arranged between the surface section and the film section; and shrinking the film section by heating it to a temperature that corresponds at least to the shrinkage temperature of the film section and at least to the flow temperature of the functional coating until the contours of the film section largely conform to the contours of the surface section.

Method for coating a surface of an aircraft and an aircraft coated through this method

An aircraft landing flap includes a flap member having an abrasion-resistant coating coated on an abrasion region exposed to mechanical rubbing contacts with an aircraft spoiler. The coating comprises a polyurethane matrix based on aliphatic components and fillers embedded in the polyurethane matrix so as to increase resistance to abrasion.

Aircraft landing flap

The present invention relates to a chromate-free composition, to the use thereof for corrosion protection, and to a corrosion protection coating for the inside surfaces of fuel tanks, wherein the composition comprises binding agents, hardening agents, corrosion inhibitors and quaternary ammonium compounds in a quantity of at least 0.1% by weight.

Chromate-free corrosion protection for fuel tanks

Materials and processes for coating substrates having heterogeneous surface properties

Growing community of inventors

Drangstedt, Germany

Ottmar Schramm