Airbus Operations Gmbh

Airbus Defence and Space Gmbh

Airbus Helicopters

Airbus (Sas)

University of Zürich

Airbus Defence and Space S.a.

Elmar Bonaccurso

Peter Linde

Alois Friedberger

Tassilo Witte

Andreas Helwig

Wolfgang Machunze

Christian Thomas

Meinhard Meyer

Nicole Jordan

Christian Herrles

Sonja Nixon

Heiko Fietzek

Silke Grünke

Christian Bartels

Tobias Strobl

Camille Caruhel

Dietrich Jonke

Franz Xaver Hallweger

Oliver Rohr

Martin Englhart

Marie-Paule Guillou

Tobias Hauk

Thomas Bürger

Nikolai Striffler

Norbert Karpen

Jürgen Wehr

Susanne Holtemeyer

Sarah Bagehorn

Sophie Senani

Ricardo Maiko Uehoka Entz

Javier Alejandro Mayén Guillén

Raphael De Andrade Jorge

Stéphane Suel

Fabien Brambilla

Beatriz Rico-Oller

Lothar Mika

Pablo Blazquez Munoz

Miguel Diaz Barja

Fabien Dezitter

Davide Bottone

Stefan Seeger

Simon Schelle

Alexandre Laroche

Vittorio Vercillo

A structural component for an aircraft including at least one heatable component section having a layer structure including an inner base structure, at least one heating layer having carbon allotropes embedded in a matrix material, at least one first group of consecutive layers including at least one anode layer, at least one first insulating layer, and at least one cathode layer having an electroactive coating. The first group of layers are arranged between the inner base structure and the at least one heating layer, and at least one protective layer is arranged outside the heating layer. The first group of layers constitute a structural battery. The at least one anode layer and the at least one cathode layer are electrically connectable with the heating layer.

Structural component for an aircraft with integrated heating layer and structural battery

A system and a method for evaluating performance of a porous skin of an aircraft including the porous skin, and a boundary layer control system. The performance evaluation system includes a first sensor providing data related to the performance of the porous skin. The performance evaluation system is further configured to clean the porous skin based on the performance of the porous skin determined using the data received from the first sensor in order to ensure that the porous skin operates at its maximum capability.

Performance evaluation system of an aircraft component

Growing community of inventors

Taufkirchen, Germany

Elmar Bonaccurso