Analysis and detection of partial discharges in an electric motor of a hybrid supercar.

The objective of this thesis was the development of a new detection method of partial discharge (PD) activity in the stator of an electrical hybrid supercar fed by a silicon carbide converter, for which detection with common methods make it very difficult to separate PD pulses from switching noise. This work focused on the analysis and detection of partial discharges making use of an antenna, a peak detector, and an oscilloscope capable of capturing the electromagnetic pulses emitted during PD activity. Validation of the proposed method was done by comparing the partial discharge inception voltage (PDIV) detected by this system with the one obtained from an optical method of proven accuracy, with different rise times and samples. Further development of this method, if proved successful on a full stator, can help increasing the overall reliability of the car, potentially allowing for real time detection of PD activity and predictive maintenance before failure of the insulation system in a hybrid vehicle.

Regolazione della pompa elettrica del carburante a bassa pressione: Analisi dell'impatto sul consumo specifico di un motore a combustione interna

The trend of CO2 emission limit and fuel saving due to the oil price increase and are important drivers for engines development. The engine auxiliary devices electrification (g.e fuel pump) is a way to reduce the energy consumption, because it becomes possible to control them depending on engine operation point, this kid of management can be applied to the electric low-pressure pump. Usually the fuel delivery is performed at the maximum flow rate and a pressure regulator discharges the exceeding fuel amount inside the rail (gasoline engine) or upstream of the high pressure pump (common rail diesel engine). In this work it has been investigated the fuel saving achievable through a proper control of the electric fuel pump on a small common rail diesel engine, and a control architecture is proposed. The aim was to maximize the fuel economy without any impact on pressure control in the engine transient conditions. L'andamento del limite di emissioni di CO2 e il risparmio di carburante dovuto all'aumento del prezzo del petrolio sono fattori importanti per lo sviluppo dei motori. I dispositivi ausiliari, come la pompa del carburante, sono un modo per ridurre il consumo energetico, in quanto diventa possibile controllarli a seconda del punto di funzionamento del motore, questo tipo di gestione può essere applicato alla pompa elettrica a bassa pressione. Solitamente la portata del combustibile viene eseguita alla portata massima e un regolatore di pressione si scarica la quantità eccedente di carburante all'interno del rail (motore a benzina) o a monte della pompa a alta pressione (common rail motore diesel). In questo lavoro è stato studiato il risparmio di combustibile ottenibile attraverso un adeguato controllo della pompa elettrica del carburante su un piccolo motore diesel common rail e viene proposta una architettura di controllo. Lo scopo è quello di massimizzare il risparmio di carburante, senza alcun impatto sul controllo della pressione nelle condizioni transitorie del motore.

Development of iodine and air chemistry models for the simulation of plasma in Helicon Plasma Thrusters

The aim of this work is to analyse the chemistry models of low pressure Helicon discharges fed with iodine and air. In particular the focus of this research is to understand the plasma dynamics in order to predict propulsive performances of iodine and air-breathing Helicon Plasma Thrusters. The two systems have been simulated and analysed with the use of global models, i.e. a 0 dimensional tool to solve the set of governing equations by assuming that all quantities are volume averaged. Furthermore, some strategies have been implemented to improve the accuracy of this approach. A verification have been accomplished on the global models for both iodine and air, comparing results against simulations taken from literature. Moreover, the iodine global model has been validated against the experimental measurements of REGULUS, an helicon plasma thruster developed by the Italian company T4i, with a good agreement. From the analysis of iodine model, it has been found a significantly higher density for atomic positive ions with respect to molecular ions. Negative ions, instead, have shown to have negligible effect on the propulsive results. Also, the influence of reactions between heavy particles has been analysed with the global model. Results have demonstrated that, in the iodine case, chemistry is almost entirely affected by electronic collisions. For what concerns air-breathing results, it has been investigated the effects of the orbital height on propulsive performances. In particular, the global model has shown that at lower height, the values of thrust and specific impulse are lower due a change in atmosphere concentration. Finally, the iodine chemistry model has been introduced in the fluid code 3D-VIRTUS in order to preliminary assess the plasma properties of a Helicon discharge chamber for electric propulsion.