TY - CHAP A1 - Afanasev, Anna ED - Mottok, Jürgen ED - Reichenberger, Marcus T1 - Force-oriented 3D printing of continuous fiber-reinforced plastic structures T2 - Applied Research Conference 2019 - ARC 2019, 08 July 2019, Regensburg KW - Faserverbundwerkstoff KW - 3D-Druck Y1 - 2019 SN - 978-3-96409-182-6 SP - 213 EP - 218 PB - Pro Business GmbH CY - Berlin ER - TY - JOUR A1 - Schimmer, Florian A1 - Ladewig, Sven A1 - Motsch, Nicole A1 - Hausmann, Joachim M. A1 - Ehrlich, Ingo T1 - Comparison of Low-Velocity Impact Damage Behavior of Unidirectional Carbon Fiber-Reinforced Thermoset and Thermoplastic Composites JF - Key Engineering Materials N2 - This paper investigates the damage behavior of thermoset and thermoplastic fiber-reinforced composites. The specimens were subjected to low-velocity impacts (LVI) to produce barely visible impact damages (BVID). To compare the dependency of the matrix system and the laminate lay-up on the impact damage, four test series were set up. Therefore, laminates with an epoxy (EP) and a polyether ether ketone (PEEK) matrix in a quasi-isotropic (QI) [+45/0/-45/90]2s and an orthotropic (OT) fiber lay-up [0/90]4s were manufactured. To eliminate the influence of variant fiber systems, the thermoplastic tape and the thermoset prepreg contain similar carbon fibers (CF). After impact testing with three different impact energies, inner damages were investigated by using ultrasonic analyses. To get a deeper understanding of the interior damage mechanisms, cross sections of the damaged areas were examined via reflected light microscopy. By using these destructive and non-destructive test methods, significant differences in the damage behavior of composites with thermoplastic and thermoset matrix systems were identified for both laminate lay-ups. KW - Barely Visible Impact Damage KW - Carbon Fiber Reinforced Plastic KW - Low-velocity-impact KW - Thermoplastics KW - Ultrasonic Analysis Y1 - 2019 U6 - https://doi.org/10.4028/www.scientific.net/KEM.809.9 SN - 1662-9795 VL - 809 SP - 9 EP - 14 PB - Trans Tech Publications ER - TY - CHAP A1 - Seppenhauser, P. ED - Mottok, Jürgen ED - Reichenberger, Marcus T1 - Examinations of the Printer Head Prototype for UV Resins with Continous Fiber-Reinforcement T2 - Applied Research Conference 2019 - ARC 2019, 8 July 2019, Regensburg KW - 3D-Druck KW - Druckkopf KW - Kunstharz KW - Faserverstärkter Kunststoff Y1 - 2019 SN - 978-3-96409-182-6 SP - 241 EP - 248 PB - Pro Business GmbH CY - Berlin ER - TY - JOUR A1 - Romano, Marco A1 - Ehrlich, Ingo A1 - Gebbeken, Norbert T1 - Parametric characterization of a mesomechanic kinematic in plain and twill weave 2/2 reinforced composites by FE-calculations JF - Archives of Materials Science and Engineering (ArchivesMSE) N2 - Purpose: A parametric characterization of a mesomechanic kinematic caused by ondulation in fabric reinforced composites is investigated by numerical investigations. Design/methodology/approach: Due to the definition of plain representative sequences of balanced plain-weave and twill-weave 2/2 fabric reinforced single layers based on sines the variable geometric parameters are the amplitude and the length of the ondulation. Findings: The mesomechanic kinematic can be observed in the FE analyses for both kinds of fabric constructions. Research limitations/implications: The FE analyses consider elasticity and contraction due to Poisson effects, respectively, of the model under selected longitudinal strains. Practical implications: The results are evaluated at relevant positions on the centre-line of the ondulated warp-yarn of the plain representative model. A direct and linear coupling in case of the transversal kinematic behaviour, and thereby a corresponding definite reduction of the evaluated longitudinal strains in terms of the difference of the applied and determined longitudinal strains is identified. Originality/value: Both characteristic purely kinematic reactions due to geometric constraints directly depend on the introduced degree of ondulation. This non-dimensional parameter relates amplitude and length of one complete ondulation, and thus represents the intensity of the ondulation of the respective fabric construction. Y1 - 2019 U6 - https://doi.org/10.5604/01.3001.0013.2869 SN - 1897-2764 VL - 97 IS - 1-2 SP - 20 EP - 38 PB - Index Copernicus ER - TY - RPRT A1 - Schlamp, Matthias A1 - Ehrlich, Ingo ED - Baier, Wolfgang T1 - Analyse des Impact-Verhaltens gekrümmter Strukturbauteile von Luftfahrzeugen zur Entwicklung eines Strukturüberwachungssystems für faserverstärkte Kunststoffe - BIRD T2 - Forschung 2019 / Ostbayerische Technische Hochschule Regensburg N2 - Die in Flugvorausrichtung weisenden Bauteile von Luftfahrzeugen sind oftmals durch Einschläge aufgrund von Vogelschlag, Hagel oder aufgewirbelten Kleinteilen gefährdet. Diese Einschläge, sogenannte Impacts, weisen bei faserverstärkten Kunststoffen ein stark krümmungs- und materialabhängiges Verhalten und Schadensausmaß auf. Impact-Schädigungen führen oftmals zu hohen Reparaturkosten, welche durch eine genauere Kenntnis des Schadens verringert werden können. Zur Klassifizierung dieser Schädigungen steht dabei vor allem das auftretende Frequenz signal des Impacts im Fokus der Untersuchungen. Y1 - 2019 UR - https://doi.org/10.35096/othr/pub-789 SN - 978-3-9818209-6-6 SP - 40 EP - 41 PB - VMK Verlag für Marketing & Kommunikation GmbH & Co. KG ER - TY - RPRT A1 - Siegl, Marco A1 - Ehrlich, Ingo ED - Baier, Wolfgang T1 - Internationale Forschung zum Biege- und Deformationsverhalten von faserverstärkten Kunststoffrohren T2 - Forschung 2019 / OTH Regensburg Y1 - 2019 UR - https://doi.org/10.35096/othr/pub-789 SN - 978-3-9818209-6-6 SP - 42 EP - 43 PB - VMK Verlag für Marketing & Kommunikation ER - TY - CHAP A1 - Lindner, Matthias A1 - Berndt, Dominik A1 - Jungbauer, Bastian A1 - Ehrlich, Ingo A1 - Schreiner, Rupert A1 - Pipa, Andrei V. A1 - Hink, Rüdiger A1 - Foest, Rüdiger A1 - Brandenburg, Ronny A1 - Max, Alexander A1 - Caspari, Ralf T1 - Fabrication, surface integration and testing of miniaturized dielectric barrier discharge plasma actuators for active flow control applications T2 - AIAA Aviation 2019 Forum, 17-21 June 2019, Dallas, Texas Y1 - 2019 U6 - https://doi.org/10.2514/6.2019-2998 ER -