@inproceedings{BerndtLindnerSchreineretal., author = {Berndt, Dominik and Lindner, Matthias and Schreiner, Rupert and Pipa, Andrei V. and Hink, R{\"u}diger and Brandenburg, Ronny and Foest, R{\"u}diger and Geils, Judith and Sander, Aljoscha and Hoffmann, Florian and Matz, Daniel and Baars, Albert and Kesel, Antonia and Max, Alexander and Caspari, Ralf}, title = {Realization of Multifunctional Surfaces Containing MEMS-based DBD Plasma Actuators and Biomimetic Structures for Flow Manipulation}, series = {AIAA Aviation 2019 Forum, 2019, Dallas}, booktitle = {AIAA Aviation 2019 Forum, 2019, Dallas}, publisher = {American Institute of Aeronautics and Astronautics, Inc}, doi = {10.2514/6.2019-2999}, language = {en} } @inproceedings{LindnerBerndtPrommesbergeretal., author = {Lindner, Matthias and Berndt, Dominik and Prommesberger, Christian and Langer, Christoph and Schreiner, Rupert}, title = {Field emission assisted micro plasma discharges at vacuum and atmospheric pressures}, series = {31st International Vacuum Nanoelectronics Conference (IVNC), 2018, Kyoto, Japan}, booktitle = {31st International Vacuum Nanoelectronics Conference (IVNC), 2018, Kyoto, Japan}, doi = {10.1109/IVNC.2018.8520181}, pages = {2}, abstract = {Spatially confined non-equilibrium plasmas at vacuum and atmospheric pressure in the dimensions from a few microns to one millimeter are a promising approach to the generation and maintenance of stable glow discharges. The realization of these micro-discharges or micro-plasmas enable more accurate investigations in the field of micro plasma research. We report on field emission assisted micro plasmas excited by an alternating current with frequencies up to 1 kHz. Due to the field enhancement caused by an array of Si nano-tip structures the ignition voltage of stable plasma discharges can be reduced by 30\%.}, language = {en} } @inproceedings{BerndtLindnerTschurtschenthaleretal., author = {Berndt, Dominik and Lindner, Matthias and Tschurtschenthaler, Karl and Langer, Christoph and Schreiner, Rupert}, title = {Miniaturized Plasma Actuator Flow Measurements by MEMS-Based Thermal Conductivity Sensors}, series = {MDPI Proceedings of Eurosensors 2018, 9-12 September, Graz}, volume = {Vol.13}, booktitle = {MDPI Proceedings of Eurosensors 2018, 9-12 September, Graz}, number = {2}, doi = {10.3390/proceedings2130939}, abstract = {The gasflow created by a minaturized dielectric barrier discharge (DBD) plasma actuator is measured by a MEMS-based thermal conductivity gas sensor giving an indication of flow velocity and flow direction. The possiblity of several sensors in a small area gives a far better accuracy of local flow phenomena compared to conventional sensors. This is important for a better understanding of plasma- induced flow characteristics.}, language = {en} } @article{BerndtMuggliWittweretal., author = {Berndt, Dominik and Muggli, Josef and Wittwer, Franz and Langer, Christoph and Heinrich, Stephan and Knittel, Thorsten and Schreiner, Rupert}, title = {MEMS-based thermal conductivity sensor for hydrogen gas detection in automotive applications}, series = {Sensors and Actuators A: Physical}, volume = {305}, journal = {Sensors and Actuators A: Physical}, number = {April}, publisher = {Elsevier}, doi = {10.1016/j.sna.2019.111670}, abstract = {Accurate detection of hydrogen gas in vehicle interiors is very important for the future of a fuel cell car. Since this type of gas is highly volatile and flammable, the measurement methods have to be very reliable and precise due to safety reasons. In this paper a thermal conductivity sensor for hydrogen gas detection is presented, exhibiting a lower detection limit of 2000 ppm hydrogen in laboratory air. The sensor element is realized by micro-fabrication techniques on silicon wafers. The heated filament is exposed by a selective wet etching process creating a micro-hotplate on a thin membrane. In order to minimize power consumption, the sensor is operated in pulsed mode. Hydrogen gas detection was carried out using a synthetic gas testbench. Measurements of hydrogen contents ranging from 0\% to 4\% with an increment of 0.5\% were successfully performed for ambient gas temperatures between -15°C and 84°C. Including humidity, high moisture contents have the greatest influence on thermal conductivity. This was predicted in theoretical investigations and confirmed in experiments. For evaluation, both the change in resistance ΔR as well as the time constant τ were taken as sensor output. For both quantities, the previously established theoretical relationship with thermal conductivity could be confirmed.}, language = {en} } @article{BerndtMuggliHeckeletal., author = {Berndt, Dominik and Muggli, Josef and Heckel, Robert and Rahiman, Mohd Fuad and Lindner, Matthias and Heinrich, Stephan and Pl{\"o}chinger, Heinz and Schreiner, Rupert}, title = {A Robust Miniaturized Gas Sensor for H₂ and CO₂ Detection Based on the 3ω Method}, series = {Sensors}, volume = {22}, journal = {Sensors}, number = {2}, publisher = {MDPI}, address = {Basel}, doi = {10.3390/s22020485}, pages = {1 -- 17}, abstract = {Gas concentration monitoring is essential in industrial or life science areas in order to address safety-relevant or process-related questions. Many of the sensors used in this context are based on the principle of thermal conductivity. The 3ω-method is a very accurate method to determine the thermal properties of materials. It has its origin in the thermal characterization of thin solid films. To date, there have been very few scientific investigations using this method to determine the thermal properties of gases and to apply it to gas measurement technology. In this article, we use two exemplary gases (H2 and CO2) for a systematical investigation of this method in the context of gas analysis. To perform our experiments, we use a robust, reliable sensing element that is already well established in vacuum measurement technology. This helix-shaped thin wire of tungsten exhibits high robustness against chemical and mechanical influences. Our setup features a compact measurement environment, where sensor operation and data acquisition are integrated into a single device. The experimental results show a good agreement with a simplified analytical model and FEM simulations. The sensor exhibits a lower detection limit of 0.62\% in the case of CO2, and only 0.062\% in case the of H2 at an excitation frequency of 1 Hz. This is one of the lowest values reported in literature for thermal conductivity H2 sensors.}, language = {en} } @inproceedings{RahimanBerndtSchreiner, author = {Rahiman, Mohd Fuad and Berndt, Dominik and Schreiner, Rupert}, title = {Micro-wire Pirani with temperature-stabilized Environment}, series = {3. Symposium Elektronik und Systemintegration ESI 2022: 06. April 2022, Hochschule Landshut}, booktitle = {3. Symposium Elektronik und Systemintegration ESI 2022: 06. April 2022, Hochschule Landshut}, isbn = {978-3-9818439-7-2}, pages = {52 -- 59}, language = {en} } @article{LangerBerndtSchreiner, author = {Langer, Christoph and Berndt, Dominik and Schreiner, Rupert}, title = {Sensitivity of thermal conductivity vacuum gauges for constant current and constant temperature operation}, series = {Journal of Vacuum Science and Technology B: Nanotechnology and Microelectronics}, volume = {40}, journal = {Journal of Vacuum Science and Technology B: Nanotechnology and Microelectronics}, number = {5}, publisher = {AIP Publishing}, doi = {10.1116/6.0001964}, abstract = {To optimize the measurement range of thermal conductivity vacuum gauges, an expression for the sensitivity is required that takes into account all geometrical, material-specific, and operating parameters. Therefore, equations of the sensor output signal as a function of the pressure for the constant current and the constant temperature mode have been developed analytically. Based on these equations, the sensitivity of the vacuum gauge and its influencing parameters was investigated and discussed. For comparable conditions, the constant temperature operation shows a significantly higher sensitivity for high pressures, while the constant current operation shows higher sensitivity at low pressures. The sensitivity in both the constant current and the constant temperature mode depends on the ratio of the filament surface area and the parasitic thermal conductance. In addition, for the constant current operation, the sensitivity also depends on the current value and the temperature coefficient of the filament resistor. For the constant temperature operation, the sensitivity additionally depends on the distance of the filament and the reference plane. However, to extend the measurement range of a thermal conductivity vacuum gauge toward low pressures, a reduction of the parasitic thermal conductance is mandatory for both the constant current and the constant temperature mode.}, language = {en} } @phdthesis{Berndt, author = {Berndt, Dominik}, title = {Thermische Wasserstoffsensoren f{\"u}r den Automobilbereich}, address = {Regensburg}, abstract = {F{\"u}r den sicheren Betrieb eines Brennstoffzellenfahrzeugs sind Sensoren wichtig, welche die Wasserstoffkonzentration im Fahrzeuginterieur kontinuierlich {\"u}berwachen, um m{\"o}glichen Entz{\"u}ndungen bzw. Explosionen vorzubeugen. Daf{\"u}r wurden von verschiedenen nationalen und internationalen Instanzen bestimmte Kriterien definiert, die Wasserstoffsensoren f{\"u}r einen Einsatz in Brennstoffzellenfahrzeugen erf{\"u}llen m{\"u}ssen. Im Jahr 2020gab es noch keinen einzigen kommerziell erh{\"a}ltlichen Sensor, der alle diese Kriterien bedienen konnte. In der vorliegenden Arbeit wurde f{\"u}r zwei verschiedene Sensoren die Eignung des thermischen Wirkprinzips f{\"u}r die Detektion von Wasserstoff im Kontext dieser Sicherheitskriterien untersucht. Dabei wurden mit einem MEMS-Sensor und einem Mikrodrahtsensor zwei vergleichsweise einfache Geometrien herangezogen, welche den eindimensionalen und zylindersymmetrischen Fall abbilden sollen. F{\"u}r zwei dynamische Operationsmodi (gepulste Str{\"o}me und 3ω-Methode) wurden darauf aufbauend analytische Modelle basierend auf vereinfachten Sensorgeometrien entwickelt, um die Temperaturentwicklung des Sensorelements in Abh{\"a}ngigkeit der Zeit zu charakterisieren. Diese Studien wurden anschließend anhand von detaillierteren Modellen mithilfe von FEM-Simulationen erg{\"a}nzt und spezifiziert. Darin konnte gezeigt werden, dass f{\"u}r den gepulsten Betrieb sowohl die Pulsh{\"o}he als auch die Zeitkonstante des gemessenen Widerstands- bzw. Temperaturpulses als Messgr{\"o}ße herangezogen werden kann. Beim 3ω-Betrieb konnte zudem eine starke Frequenzabh{\"a}ngigkeit dieser Widerstands- bzw. Temperaturcharakteristik beobachtet werden. Die analytischen und numerischen Studien wurden anschließend durch experimentelle Ergebnisse best{\"a}tigt. Im Hinblick auf die zuvor definierten Kriterien stellte sich heraus, dass die Auswertung der Zeitkonstante beim gepulsten Betrieb im Hinblick auf Sensitivit{\"a}t und Aufl{\"o}sungsgrenze der Auswertung der Pulsh{\"o}he deutlich unterlegen ist. Beim 3ω-Betrieb k{\"o}nnen durch die hochintegrierte Messumgebung deutlich h{\"o}here Genauigkeiten und Aufl{\"o}sungsgrenzen erzielt werden. F{\"u}r den MEMS-Sensor wurde bei einer Anregungsfrequenz von 1 Hz mit 55 ppm die bislang geringste in der Literatur berichtete Aufl{\"o}sungsgrenze f{\"u}r einen thermischen Wasserstoffsensor erreicht. Der Leistungsverbrauch ist dabei im Vergleich zum Pulsbetrieb entsprechend des jeweiligen Tastgrads leicht bis m{\"a}ßig erh{\"o}ht, die Ansprechzeit wird bei beiden Operationsmodi maßgeblich durch die Sensorgeometrie beeinflusst. Die geometrischen Parameter der jeweiligen Sensoren haben ferner einen starken Einfluss auf die Sensitivit{\"a}t, womit die Divergenz in der Performance von MEMS-Chip und Drahtsensor erkl{\"a}rt werden kann. Es besteht ferner eine starke Temperatur- und Feuchtigkeitsabh{\"a}ngigkeit des Sensorsignals, welches bei beiden Operationsmodi indirekt proportional zur W{\"a}rmeleitf{\"a}higkeit des betrachteten Gasgemischs ist. Die Abh{\"a}ngigkeit vom definierten Umgebungsdruck ist lediglich f{\"u}r die Zeitkonstante relevant, bei der Pulsh{\"o}he besteht keine Druckabh{\"a}ngigkeit. Es konnte eine grunds{\"a}tzliche Eignung des thermischen Messprinzips f{\"u}r den Einsatz eines Wasserstoffsensors im Automobilbereich festgestellt werden. F{\"u}r eine Anwendung m{\"u}ssen allerdings Referenzsensoren f{\"u}r Temperatur, Feuchtigkeit und Druck implementiert werden und eine Kalibrierung in Abh{\"a}ngigkeit dieser Gr{\"o}ßen erfolgen. Der 3ωBetrieb ist aufgrund der h{\"o}heren Genauigkeit zu bevorzugen. W{\"a}hrend der MEMSSensor im Hinblick auf Sensitivit{\"a}t, Ansprechzeit und Leistungsaufnahme gut abschneidet, liegen die Vorteile des Mikrodrahtsensors in seiner Robustheit und der vergleichsweise einfachen Realisierbarkeit}, subject = {Kraftfahrzeugtechnik}, language = {de} } @article{LindnerPipaKarpenetal., author = {Lindner, Matthias and Pipa, Andrei V. and Karpen, Norbert and Hink, R{\"u}diger and Berndt, Dominik and Foest, R{\"u}diger and Bonaccurso, Elmar and Weichwald, Robert and Friedberger, Alois and Caspari, Ralf and Brandenburg, Ronny and Schreiner, Rupert}, title = {Icing Mitigation by MEMS-Fabricated Surface Dielectric Barrier Discharge}, series = {Applied Sciences}, volume = {11}, journal = {Applied Sciences}, number = {23}, publisher = {MDPI}, address = {Basel}, doi = {10.3390/app112311106}, pages = {1 -- 17}, abstract = {Avoiding ice accumulation on aerodynamic components is of enormous importance to flight safety. Novel approaches utilizing surface dielectric barrier discharges (SDBDs) are expected to be more efficient and effective than conventional solutions for preventing ice accretion on aerodynamic components. In this work, the realization of SDBDs based on thin-film substrates by means of micro-electro-mechanical-systems (MEMS) technology is presented. The anti-icing performance of the MEMS SDBDs is presented and compared to SDBDs manufactured by printed circuit board (PCB) technology. It was observed that the 35 mu m thick electrodes of the PCB SDBDs favor surface icing with an initial accumulation of supercooled water droplets at the electrode impact edges. This effect was not observed for 0.3 mu m thick MEMS-fabricated electrodes indicating a clear advantage for MEMS-technology SDBDs for anti-icing applications. Titanium was identified as the most suitable material for MEMS electrodes. In addition, an optimization of the MEMS-SDBDs with respect to the dielectric materials as well as SDBD design is discussed.}, language = {en} } @inproceedings{LindnerBerndtTschurtschenthaletal., author = {Lindner, Matthias and Berndt, Dominik and Tschurtschenthal, Karl and Ehrlich, Ingo and Jungbauer, Bastian and Schreiner, Rupert and Pipa, Andrei V. and Hink, R{\"u}diger and Foest, R{\"u}diger and Brandenburg, Ronny and Neuwirth, Daniel and Karpen, Norbert and Bonaccurso, Elmar and Weichwald, Robert and Max, Alexander and Caspari, Ralf}, title = {Aircraft Icing Mitigation by DBD-based Micro Plasma Actuators}, series = {AIAA AVIATION 2020 FORUM: June 15-19, 2020}, booktitle = {AIAA AVIATION 2020 FORUM: June 15-19, 2020}, doi = {10.2514/6.2020-3243}, abstract = {We present the application of plasma actuators as a technology for ice prevention at airfoils. The miniaturized dielectric barrier discharge (DBD) plasma actuators (PA) were fabricated by means of microelectromechanical systems (MEMS). We elucidate how to make the actuator samples scalable and applicable to any desired shape by the use of flexible inorganic zirconia substrates. For this purpose, we applied our developed embedding method to integrate the micro actuators in modern carbon/glass fiber reinforced polymer (CFRP/GFRP) materials. Next, the embedded actuator samples were mounted on a mechanical air profile-like fixture and placed in the icing wind tunnel iCORE. The samples were tested in rime ice conditions at temperatures of -15 to -20° C and air speeds up to 30 m/s. Unlike other groups we used a thin film zirconia substrate as dielectric for the plasma actuator. Due to the low substrate thickness of just 150 µm, an operating voltage of 2 kVRMS is already sufficient enough for a stable plasma formation. The experiments show that the operated actuator was able to prevent the ice formation and first indications of a De-icing function were also found. Hence, we show that it is feasible to realize an anti-icing system with zirconia-based plasma actuators operated at lower voltages compared to conventional ones.}, language = {en} } @inproceedings{LindnerBerndtJungbaueretal., author = {Lindner, Matthias and Berndt, Dominik and Jungbauer, Bastian and Ehrlich, Ingo and Schreiner, Rupert and Pipa, Andrei V. and Hink, R{\"u}diger and Foest, R{\"u}diger and Brandenburg, Ronny and Max, Alexander and Caspari, Ralf}, title = {Fabrication, surface integration and testing of miniaturized dielectric barrier discharge plasma actuators for active flow control applications}, series = {AIAA Aviation 2019 Forum, 17-21 June 2019, Dallas, Texas}, booktitle = {AIAA Aviation 2019 Forum, 17-21 June 2019, Dallas, Texas}, doi = {10.2514/6.2019-2998}, language = {en} } @inproceedings{EilerBerndtSchreiner, author = {Eiler, Julian and Berndt, Dominik and Schreiner, Rupert}, title = {Miniaturisierter Wasserstoffsensor basierend auf der 3-Omega Methode}, series = {Tagungsband zum 4. Symposium Elektronik und Systemintegration ESI: 17. April 2024, Hochschule Landshut}, booktitle = {Tagungsband zum 4. Symposium Elektronik und Systemintegration ESI: 17. April 2024, Hochschule Landshut}, publisher = {Hochschule f{\"u}r Angewandte Wissenschaften Landshut}, address = {Landshut}, isbn = {978-3-9818439-9-6}, doi = {10.57688/420}, url = {http://nbn-resolving.de/urn:nbn:de:bvb:860-opus4-4205}, pages = {38 -- 45}, abstract = {Die Arbeit stellt einen thermischen Wasserstoffsensor auf Siliziumbasis vor, der mit der 3-Omega Messmethode betrieben wird. Durch das dynamische Messverfahren, die große Sensoroberfl{\"a}che bei gleichzeitig geringer thermischer Masse und der Materialkombination wird eine Aufl{\"o}sungsgrenze von 55 ppm Wasserstoff in Stickstoff erreicht.}, language = {de} }