Im Rahmen der vorliegenden Arbeit werden dynamische Modelle eines IGCC-Kraftwerkes mit CO2-Abtrennung unter Verwendung des Modellierungstools Modelica/Dymola entwickelt. Dabei liegt der Schwerpunkt auf dem Gaspfad der Gasreinigung. Es ist vorteilhaft, für verschiedene Aufgaben, Modelle mit unterschiedlicher Tiefe zu verwenden. Mit den detaillierten Modellen werden Simulationen der Teilprozesse durchgeführt. Für den Aufbau eines Gesamtsystems werden vereinfachte Modelle verwendet. Anhand des Gesamtsystems werden drei Regelkonzepte (Gleitdruckregelung, Leistungsregelung der Gasturbine, Leistungsregelung des Vergasers) untersucht und bewertet. Des Weiteren werden drei Störfallszenarien (Ausfall des Sättigers im Brennstoffsystem, Betriebsstörung in der Vergaserinsel, Unterbrechung der Stickstoffzumischung im Brennstoffsystem) getestet.

Modeling of heat transfer using Dymola. In this report a evaporator, economizer and superheater where modeled. The report describes how the models where modeled and what input was most suitable for a accurate model.

This diploma thesis deals with processes of electrical circuits calculations in the last years' worldwide standards like Dymola, MATLAB, Maple or SPICE applications. Circuits calculations are linked with methods for solving linear differential equations, used in this work also by verification of functionality of designed models for CMOS inverter, CMOS NAND, CMOS NOR. Numerical integration method in combination with Taylor series is a suitable method also for parallel calculations of CMOS VLSI circuits. CMOS circuits simulation was implemented with this method in applications in MATLAB language, solving circuits, represented by differential equations. Functionality of the applications was verified by some real examples. Significant acceleration of calculations using Taylor series compared to other methods is an important factor in choosing methods used in circuit simulations.

<p dir="ltr">Energy consciousness initiatives have seen a recent uptick to curb the ever growing concerns of global warming. Heat Pumps are a crucial piece of technology for these efforts, as they consume lower energy than the requirement they satisfy and are typically used for refrigeration and HVAC systems. Hybrid Heat Pump Water Heater (HPWH) technologies have seen increased adoption, and the improvement of these technologies could pay dividends in the long run. </p><p dir="ltr">This project explores the optimal design space of HPWHs within the context of the Department of Energy Guidelines for their performance rating and compares several up and coming refrigerants with lower GWP than the current market dominant refrigerant, R-134a, to provide consistent performance with improvements on the environmental front along with potential cost improvements on the manufacturing front. For this purpose, Dymola, a simulation software that employs the Modelica language for modeling complex dynamic systems, is employed to study the transient behavior of a market example Heat Pump Water Heater. </p><p dir="ltr">The results of these simulations were validated using experimental data gathered in the laboratory using relevant instrumentation on the physical device and manufacture specified performance ratings to compare the validity of the simulation results. The results of the study indicated the presence of a multi-dimensional design space with a defined set of possible combinations for device implementation. Within that feasible region, there exist multiple trajectories of iso-preference which alter the overall device performance, and the careful study of these parameters and their implications on the device performance can lead to a more robust design pathway for future improvements of the device. The work also contextualizes these improvements by quantifying the relative importance of different parameters upon the final performance of the device, showing how to identify which parameters to focus on when embarking upon an improvement journey. Additionally, preliminarily ideal specifications for the device operation under different refrigerants studied were also identified to provide similar or better performance to the current device. </p><p dir="ltr">The study showed that when matching mass flux rates, R-152a, R-290, and R-600a outperform R-134a in terms of expected COP. Of the 3, only R-290 uses a smaller compressor size than the baseline R-134a cycle for achieving the required heating capacity. The other refrigerants studied do not improve upon the COP of the cycle, but do have benefits over R-134a in terms of their respective GWPs. </p><p dir="ltr">The results suggest that with the considered alterations, R-290 systems within the current charge restrictions (<150g) can be developed and achieve the same heating performance with slight improvements on COP and therefore potentially UEF values. </p><p dir="ltr">The study also shows that all refrigerants considered could achieve the required heating capacity with a considerably downsized condenser and appropriately reduced subcooling. It highlighted the trends being consistent across refrigerants and implemented a final alternative refrigerant through the identified optimization steps to arrive at a new configuration without revalidating the trends, showing that newer optimal configurations could be identified with minimal time spent in the simulation environment. </p><p dir="ltr">Finally, the study explored alternative control possibilities by way of overheating the water beyond its required setpoint and enabling a control based mixing at the outlet to reduce the energized time of the device and leveraging the exceptional insulation capabilities for thermal storage.</p>

<p>In the process of designing an electric power supply system for an aircraft, parameters like low weight and low losses are important. Reliability, robustness and low cost are other important factors. In the Saab Gripen aircraft, the design of the primary power supply of the electric flight control system was updated by exchanging a switching transistor regulator to a magnetic amplifier (magamp). By introducing a magamp design, weight was saved and a more reliable power supply system at a lower cost was achieved.</p><p> In this particular case, with the power supply of the electric flight control system in the Saab Gripen fighter, advantage could be taken of a specific permanent magnet generator (PM-generator). The frequency of the generator offered the perfect conditions for a magamp controller. A key parameter in designing magnetic amplifiers (magamps) is low losses. New amorphous alloys offer new possibilities of the technique in designing magnetic amplifiers, because of their extremely low losses.</p><p> The core losses are evaluated by studying the equations and diagrams specifying the power losses. The core losses are evaluated and compared with the copper losses in the process of optimizing low weight and low losses. For this an engineering tool is developed and demonstrated.</p><p> Evaluations of the hysteresis characteristics for the magnetic alloys, as well as modeling and simulation of the core losses, are presented in this work. The modeling of the core losses includes hysteresis losses, eddy current losses and excess losses as well as copper losses. The losses are studied dynamically during realistic operational conditions. The model can be used for any generic analysis of hysteresis in magnetic circuits. Applications of magnetic amplifiers in aircrafts have been demonstrated to be a feasible alternative</p>

This master's thesis deals with modeling of linear electrical circuits through the differential algebraical equation systems. It describes methods of numerical solving, discusses the need of algebraical conversions and possibility of minimalization through the use of parasitic components. In addition, it involves the design and implementation of extension of available simulation tool.

In the process of designing an electric power supply system for an aircraft, parameters like low weight and low losses are important. Reliability, robustness and low cost are other important factors. In the Saab Gripen aircraft, the design of the primary power supply of the electric flight control system was updated by exchanging a switching transistor regulator to a magnetic amplifier (magamp). By introducing a magamp design, weight was saved and a more reliable power supply system at a lower cost was achieved. In this particular case, with the power supply of the electric flight control system in the Saab Gripen fighter, advantage could be taken of a specific permanent magnet generator (PM-generator). The frequency of the generator offered the perfect conditions for a magamp controller. A key parameter in designing magnetic amplifiers (magamps) is low losses. New amorphous alloys offer new possibilities of the technique in designing magnetic amplifiers, because of their extremely low losses. The core losses are evaluated by studying the equations and diagrams specifying the power losses. The core losses are evaluated and compared with the copper losses in the process of optimizing low weight and low losses. For this an engineering tool is developed and demonstrated. Evaluations of the hysteresis characteristics for the magnetic alloys, as well as modeling and simulation of the core losses, are presented in this work. The modeling of the core losses includes hysteresis losses, eddy current losses and excess losses as well as copper losses. The losses are studied dynamically during realistic operational conditions. The model can be used for any generic analysis of hysteresis in magnetic circuits. Applications of magnetic amplifiers in aircrafts have been demonstrated to be a feasible alternative / QC 20101103