Geier, Sebastian und Kintscher, Markus und Wierach, Peter und Monner, Hans Peter und Wiedemann, Martin (2016) Experimental and finite element analyses of multifunctional skins for morphing wing applications. In: Proc. SPIE 9803, Sensors and Smart Structures Technologies for Civil, Mechanical, and Aerospace Systems 2016, 9803. SPIE. Smart Structures NDE, 20.-24. März 2016, Las Vegas, Nevada, USA. doi: 10.1117/12.2219357.
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Kurzfassung
As a consequence of operational efficiency because of rising energy costs, future transport systems need to be mission-adaptive. Especially in aircraft design the limits of lightweight construction, reduced aerodynamic drag and optimized propulsion are pushed further and further. The first two aspects can be addressed by using a morphing leading edge. Great economic advantages can be expected as a result of gapless surfaces which feature longer areas of laminar flow. Instead of focusing on the kinematics, which are already published in a great number of varieties, this paper emphasizes as major challenge, the qualification of a multi-material layup which meets the compromise of needed stiffness, flexibility and essential functions to match the flight worthiness requirements, such as erosion shielding, impact safety, lighting protection and de-icing. It is the aim to develop an gapless leading edge device and to prepare the path for higher technology readiness levels resulting in an airborne application. During several national and European projects the DLR developed a gapless smart droop nose concept, which functionality was successfully demonstrated using a two-dimensional 5 m in span prototype in low speed (up to 50 m/s) wind tunnel tests. The basic structure is made of commercially available and certified glass-fiber reinforced plastics (GFRP, Hexcel Hexply 913). This paper presents 4-point bending tests to characterize the composite with its integrated functions. The integrity and aging/fatigue issues of different material combinations are analyzed by experiments. It can be demonstrated that only by adding functional layers the mentioned requirements such as erosion-shielding or de-icing can be satisfied. The total thickness of the composite skin increases by more than 100 % when required functions are integrated as additional layers. This fact has a tremendous impact on the maximum strain of the outer surface if it features a complete monolithic build-up. Based on experimental results a numerical model can be set up for further structural optimizaton of the multi-functional laminate. © (2016) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
elib-URL des Eintrags: | https://elib.dlr.de/104170/ | ||||||||||||||||||||||||
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Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||||||||||||||||||
Titel: | Experimental and finite element analyses of multifunctional skins for morphing wing applications | ||||||||||||||||||||||||
Autoren: |
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Datum: | 20 April 2016 | ||||||||||||||||||||||||
Erschienen in: | Proc. SPIE 9803, Sensors and Smart Structures Technologies for Civil, Mechanical, and Aerospace Systems 2016 | ||||||||||||||||||||||||
Referierte Publikation: | Nein | ||||||||||||||||||||||||
Open Access: | Ja | ||||||||||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||||||||||
In SCOPUS: | Nein | ||||||||||||||||||||||||
In ISI Web of Science: | Nein | ||||||||||||||||||||||||
Band: | 9803 | ||||||||||||||||||||||||
DOI: | 10.1117/12.2219357 | ||||||||||||||||||||||||
Herausgeber: |
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Verlag: | SPIE | ||||||||||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||||||||||
Stichwörter: | smart droop-nose, morphing structure, morphing wing, morphing leading-edge, NLF, laminar wing concept, electrothermal de-icing; | ||||||||||||||||||||||||
Veranstaltungstitel: | Smart Structures NDE | ||||||||||||||||||||||||
Veranstaltungsort: | Las Vegas, Nevada, USA | ||||||||||||||||||||||||
Veranstaltungsart: | internationale Konferenz | ||||||||||||||||||||||||
Veranstaltungsdatum: | 20.-24. März 2016 | ||||||||||||||||||||||||
Veranstalter : | SPIE society of photo-optical instrumentation engineering | ||||||||||||||||||||||||
HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||||||||||
HGF - Programm: | Luftfahrt | ||||||||||||||||||||||||
HGF - Programmthema: | Flugzeuge | ||||||||||||||||||||||||
DLR - Schwerpunkt: | Luftfahrt | ||||||||||||||||||||||||
DLR - Forschungsgebiet: | L AR - Aircraft Research | ||||||||||||||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | L - Strukturen und Werkstoffe (alt) | ||||||||||||||||||||||||
Standort: | Braunschweig | ||||||||||||||||||||||||
Institute & Einrichtungen: | Institut für Faserverbundleichtbau und Adaptronik > Multifunktionswerkstoffe | ||||||||||||||||||||||||
Hinterlegt von: | Geier, Sebastian | ||||||||||||||||||||||||
Hinterlegt am: | 30 Mai 2016 05:56 | ||||||||||||||||||||||||
Letzte Änderung: | 29 Mär 2023 00:27 |
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