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  4. Automated, Quality Assured and High Volume Oriented Production of Fiber Metal Laminates (FML) for the Next Generation of Passenger Aircraft Fuselage Shells
 
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2019
Journal Article
Title

Automated, Quality Assured and High Volume Oriented Production of Fiber Metal Laminates (FML) for the Next Generation of Passenger Aircraft Fuselage Shells

Abstract
The use of fiber-metal laminates (FML) allows for substantial advantages over a fuselage skin made of monolithic aluminum materials. Glass fiber prepreg reinforced aluminium is characterized by high damage tolerance capabilities, supporting the structural strength capability in case of any kind of damage. For this reason, FML, and GLARE in particular, have been identified as superior materials for aerospace applications. More than 400m2 FML is applied on each A380, as skin panels and as D-noses for both, vertical and horizontal stabilizer. FML possess the potential to become the baseline material for next-generation single-aisle aircrafts. The development of a new production chain that will allow automated fuselage production for future short-haul aircrafts is the focus of the studies that make up the joint project AUTOGLARE. As part of the fifth call-up for the German Aeronautical Research Programme (LuFo), the German Aerospace Center (DLR) is working with its project partners Airbus Operations, Premium Aerotech (PAG) and the Fraunhofer Gesellschaft (FhG). The development of a production chain for stiffened fuselage panels made of Fiber metal Laminates should support a production rate of 60 aircraft per month. This study contains the research work of the DLR and FhG regarding the automated and quality assured process for chain stiffened FML fuselages. In addition to a detailed explanation of the systems that were set up, this paper covers the planned tests, the completed demonstration models and the findings derived from them.
Author(s)
Ucan, Hakan
German Aerospace Centre, Institute for Composite Structures and Adaptive Systems, Braunschweig, Germany
Scheller, Joachim  
Fraunhofer-Institut für Fertigungstechnik und Angewandte Materialforschung IFAM  
Nguyen, Chinh
German Aerospace Centre, Institute for Composite Structures and Adaptive Systems, Braunschweig, Germany
Nieberl, Dorothea
German Aerospace Centre, Institute of Structures and Design, Augsburg, Germany
Beumler, Thomas
Airbus Operations GmbH, Hamburg, Germany
Haschenburger, Anja
German Aerospace Centre, Institute for Composite Structures and Adaptive Systems, Braunschweig, Germany
Meister, Sebastian
German Aerospace Centre, Institute for Composite Structures and Adaptive Systems, Braunschweig, Germany
Kappel, Erik
German Aerospace Centre, Institute for Composite Structures and Adaptive Systems, Braunschweig, Germany
Prussak, Robert
German Aerospace Centre, Institute for Composite Structures and Adaptive Systems, Braunschweig, Germany
Deden, Dominik
German Aerospace Centre, Institute of Structures and Design, Augsburg, Germany
Mayer, Monika
German Aerospace Centre, Institute of Structures and Design, Augsburg, Germany
Zapp, Phlilipp
German Aerospace Centre, Institute for Composite Structures and Adaptive Systems, Braunschweig, Germany
Pantelelis, Nikos
Synthesites SNC, Uccle, Belgium
Hauschild, Bernd  
Fraunhofer-Institut für Fertigungstechnik und Angewandte Materialforschung IFAM  
Menke, Niklas
German Aerospace Centre, Institute for Composite Structures and Adaptive Systems, Braunschweig, Germany
Journal
Science and engineering of composite materials  
Open Access
DOI
10.1515/secm-2019-0031
Additional link
Full text
Language
English
Fraunhofer-Institut für Fertigungstechnik und Angewandte Materialforschung IFAM  
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