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Robustness Analysis of CFRP structures under thermomechanical loading uncluding manufacturing defects

Liebisch, Martin und Wille, Tobias und Balokas, Georgios und Kriegesmann, Benedikt (2019) Robustness Analysis of CFRP structures under thermomechanical loading uncluding manufacturing defects. 9th EASN International Conference on Innovation in Aviation & Space, 2019-09-03 - 2019-09-06, Athen, Griechenland.

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Kurzfassung

Carbon fibre reinforced plastics (CFRP) show superior weight-specific properties compared to metals. However, the structural behavior is more complex when exposed to thermomechanical load conditions, for instance in engine, turbine or battery environments or in space applications. The properties of CFRP decrease with increasing service temperature due to the temperature-dependency of their plastic matrix system. Yet, within current industrial design processes, temperature limits are defined with high conservatism. Therefore, additional load carrying capabilities at higher temperatures, before complete loss of mechanical performance, are not exploited. This study is presenting an enhanced analysis process for robust composite design by considering temperature-dependent material behavior, effects from manufacturing deviations and uncertainties from thermomechanical loading conditions. A sequential finite element (FE) analysis strategy is utilized to assess the mechanical performance of a structure under thermal load conditions until glass transition temperature. The current investigations use nonlinear temperature-dependent material models to account for the corresponding stiffness and strength reduction. Based on the thermal load conditions and the structural concept, different temperature distribution will occur within the part and therefore, thermal expansion results in varying development of structural deformation and stress. Moreover, the temperature field causes locally decreased material properties. Evaluation of forces, stresses and strains allows assessing the structural performance. Inherent material uncertainties, local property knock-down resulting from fibre-placement defects and deviations of thermal load conditions are introduced to analyze the structural robustness. The work focuses on the analysis strategy and describes the approach of material modelling and applied uncertainties. Finally, results of the presented methodology are shown for a thin-walled stiffened CFRP structure.

elib-URL des Eintrags:https://elib.dlr.de/130913/
Dokumentart:Konferenzbeitrag (Vortrag)
Titel:Robustness Analysis of CFRP structures under thermomechanical loading uncluding manufacturing defects
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Liebisch, MartinMartin.Liebisch (at) dlr.dehttps://orcid.org/0000-0001-5423-7511NICHT SPEZIFIZIERT
Wille, TobiasTobias.Wille (at) dlr.dehttps://orcid.org/0009-0009-5777-2822NICHT SPEZIFIZIERT
Balokas, GeorgiosNICHT SPEZIFIZIERTNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Kriegesmann, BenediktNICHT SPEZIFIZIERTNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Datum:September 2019
Referierte Publikation:Ja
Open Access:Nein
Gold Open Access:Nein
In SCOPUS:Nein
In ISI Web of Science:Nein
Status:veröffentlicht
Stichwörter:Carbon fibre reinforced plastics, thermomechanical loading, material model, probabilistic analysis
Veranstaltungstitel:9th EASN International Conference on Innovation in Aviation & Space
Veranstaltungsort:Athen, Griechenland
Veranstaltungsart:internationale Konferenz
Veranstaltungsbeginn:3 September 2019
Veranstaltungsende:6 September 2019
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 - Simulation und Validierung (alt), L - Strukturen und Werkstoffe (alt)
Standort: Braunschweig
Institute & Einrichtungen:Institut für Faserverbundleichtbau und Adaptronik > Strukturmechanik
Hinterlegt von: Liebisch, Martin
Hinterlegt am:25 Nov 2019 23:52
Letzte Änderung:24 Apr 2024 20:34

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