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

Ucan, Hakan and Scheller, Scheller and Nguyen, Duy Chinh and Nieberl, Dorothea and Beumler, Thomas and Haschenburger, Anja and Meister, Sebastian and Kappel, Erik and Prussak, Robert and Deden, Dominik and Mayer, Monika and Pantelelis, Nikos and Zapp, Philipp and Hauschild, Bernd and Menke, Niklas (2019) Automated, Quality Assured and High Volume Oriented Production of Fiber Metal Laminates (FML) for the Next Generation of Passenger Aircraft Fuselage Shells. The Fourth International Symposium on Automated Composites Manufacturing, 25.-26. Apr. 2019, Montreal, Kanada.

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The use of fiber-metal laminates (FML) allows for substantial advantages over a fuselage skin made of monolithic aluminum materials. The combination of glass-fiberreinforced plastic and aluminum is characterized by low fatigue, high load tolerance and the resistance to residual stress. For this reason, FML, and GLARE in particular, have been identified as superior materials for aerospace applications. It has already been used extensively in the wide body aircraft of the Airbus Group A380, specifically on the upper fuselage shells. 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), 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 based on fiber-metal-laminates as a material is aimed at allowing a scaling-up to 60 aircrafts 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.

Item URL in elib:https://elib.dlr.de/127353/
Document Type:Conference or Workshop Item (Speech)
Title:Automated, Quality Assured and High Volume Oriented Production of Fiber Metal Laminates (FML) for the Next Generation of Passenger Aircraft Fuselage Shells
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Ucan, HakanHakan.Ucan (at) dlr.dehttps://orcid.org/0000-0002-5568-4564
Scheller, SchellerJoachim.Scheller (at) ifam.fraunhofer.deUNSPECIFIED
Nguyen, Duy ChinhChinh.Nguyen (at) dlr.deUNSPECIFIED
Nieberl, DorotheaDorothea.Nieberl (at) dlr.deUNSPECIFIED
Beumler, ThomasThomas.Beumler (at) airbus.comUNSPECIFIED
Haschenburger, AnjaAnja.Haschenburger (at) dlr.dehttps://orcid.org/0000-0001-9342-0220
Meister, SebastianSebastian.Meister (at) dlr.dehttps://orcid.org/0000-0002-8193-1143
Kappel, ErikErik.Kappel (at) dlr.dehttps://orcid.org/0000-0002-8760-8451
Prussak, RobertRobert.Prussak (at) dlr.deUNSPECIFIED
Deden, DominikDominik.deden (at) dlr.dehttps://orcid.org/0000-0001-8959-8720
Mayer, MonikaMonika.Mayer (at) dlr.deUNSPECIFIED
Pantelelis, Nikosnp (at) synthesites.comUNSPECIFIED
Zapp, PhilippPhilipp.Zapp (at) dlr.deUNSPECIFIED
Hauschild, BerndBernd.Hauschild (at) ifam.fraunhofer.deUNSPECIFIED
Menke, NiklasNiklas.Menke (at) dlr.deUNSPECIFIED
Date:26 April 2019
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In ISI Web of Science:No
Keywords:FML, fuselage sections automated Composite manufacturing, lay-up technologies ATL AFP, multi head pick and place technologies, inline quality assurance, one shot bonding
Event Title:The Fourth International Symposium on Automated Composites Manufacturing
Event Location:Montreal, Kanada
Event Type:international Conference
Event Dates:25.-26. Apr. 2019
Organizer:Concordia University / Montreal
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Structures and Materials (old)
Location: Stade
Institutes and Institutions:Institute of Composite Structures and Adaptive Systems
Institute of Composite Structures and Adaptive Systems > Composite Process Technology
Deposited By: Ucan, Dipl.-ing. Hakan
Deposited On:10 May 2019 14:05
Last Modified:09 Dec 2019 09:35

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