Airbus Operations Gmbh

Airbus Deutschland Gmbh

Georg Muehlthaler

Rainer Mueller

Sebastian Roering

Jan Dittmar

Cherif Terzi

Christoph Mevenkamp

Sebastian Capistran Zambrano

Anja Erdle

Jean Blenner

A heat exchanger with at least one cooling segment having a first, a second, and a third portion. A first heat carrier flow path, through which a first heat carrier medium flows, extends through the first portion. A second heat carrier flow path, through which a second heat carrier medium flows, extends through the second portion. A first coolant flow path, through which a first coolant medium flows, extends through the third portion. The heat exchanger comprises at least one cooling body, a second coolant medium flowing through a second coolant flow path extending through the cooling body. The first and the second heat carrier flow paths are thermally coupled, respectively, to the first and the second coolant flow path, to discharge heat energy of at least one of the first and the second heat carrier medium to at least one of the first and the second coolant medium.

Heat exchanger, cooling system and method for operating a heat exchanger and a cooling system

An insulation arrangement for thermally and acoustically insulating an aircraft fuselage, which comprises at least one insulation packet arranged on an exterior skin of the aircraft. The insulation packet includes dimensionally rigid foam, and comprises a shape corresponding at least with a structural component on the exterior skin, as the result of which the insulation packet is retained on the structural component even without any additional attachment elements. As a result, ventilation openings need not be provided, thereby reducing condensation water accumulating in aircraft insulation.

Condensation water-free insulation system for passenger aircraft

The invention relates to an aircraft side fairing, with a component () in the form of individual hollow chambers () which are arranged essentially in a preferably curved plane and are arranged between two cover layers (), wherein a gastight film which completely encases the component () with the hollow chambers () is provided and, after application of a vacuum to evacuate the hollow chambers (), surrounds the component () with the hollow chambers in a gastight manner.

Aircraft side fairing

Growing community of inventors

Hamburg, Germany

Georg Muehlthaler