Saertex Wagener Gmbh & Co. Kg

Deutsches Zentrum Fuer Luft-und Raumfahrt E.v

Arianegroup Gmbh

Airbus Operations Gmbh

Airbus Deutschland Gmbh

Deutsches Zentrum Fur Luft-und Raumfahrt E.v.

Technische Universitat Braunschweig

Aernnova Aerospace

Markus Kleineberg

Axel Siegfried Herrmann

Paul Jörn

Arno Erk Pabsch

Jens Bold

Markus Müller

Christof Sigle

Gert Wagener

Matthias Meyer

Christian Hühne

Klaus Dilger

Lars Herbeck

Matthias Grote

Jens Kleffmann

Carsten Schoeppinger

Jörg Nickel

Christian Wendt

Andreas Kolbe

Daniel Stefaniak

Jan Stüve

Dirk Röstermundt

Markus Quadt

Michael Quatmann

Gerrit Quappen

Tobias Ströhlein

Michael Frauenhofer

Steffen Niemann

Miguel Angel Castillo Acero

Robert Kaps

Denise Düring

Olaf Steffen

Tobias Bach

Christian Ückert

Federico Martin De La Escalera

David Cruz Palacios

Ulrich Herrmann

Dirk Röstermund

Heiko Assing

Thomas Wurl

A tank for the storage of liquid or gaseous substances with a fiber-reinforced plastic sheathing, which limits at least one interior space for holding the materials to be stored. At least one circumferential section of the fiber-reinforced plastic sheathing comprises an evacuable sandwich structure, which completely encloses the circumferential section. As a result, the tank has a low weight with a high thermal insulation capacity. Furthermore, a reliable explosion protection of the tank is provided. Furthermore, a method for manufacturing a tank for the storage of liquid or gaseous substances is provided.

Tank and method

The invention relates to a wing structure () for flying objects, comprising a wing leading edge () and a wing box (), wherein the wing leading edge should be arranged on the wing box in particular in a detachable manner. For this purpose, the wing leading edge is connected to the wing box within a joining segment () and to rib extensions () of the wing box by means of fastening element () near the nose segment () such that a fastening-free segment () extends on the top side () of the wing leading edge in order to compensate thermal deformation during flight.

Wing structure for flying objects

A thread or other element for bonding fibers in a fibrous reinforcement for use in a fiber composite is such that it is at least degraded in the course of the production of said fiber composite.

Fiber-reinforced composites and method for the production thereof

Growing community of inventors

Hemmingen, Germany

Markus Kleineberg