Design of a bang-bang pressure regulation system for cold gas and plasma engines

In this thesis the design of a pressure regulation system for space propulsion engines (electric and cold gas) has been performed. The Bang-Bang Control (BBC) method has been implemented through the open/close command on a solenoid valve, and the mass flow rate of the propellant has been fixed with suitable flow restrictors. At the beginning, research for the comparison between mechanical and electronic (for BBC) pressure regulators has been performed, which resulted in enough advantages for the selection of the second valve type. The major advantage is about the possibility to have a variable outlet pressure with a variable inlet pressure through a simple remote command, while in mechanical pressure regulators the ratio between inlet and outlet pressures must be mechanically settled. Different pressure control schemes have been analyzed, changing number of solenoid valves, flow restrictors and plenums. For each scheme the valve’s frequencies were evaluated with simplified mathematical models and with the use of simulators implemented on Python; the results obtained from those two methods matched quiet well. From all the schemes it was possible to observe varying frequency and duty cycle, for changes in different parameters. This results, after experimental checks, can be used to design the control system for a given total number of cycles that a specific solenoid valve can guarantee. Finally, tests were performed and it was possible to verify the goodness of the control system. Moreover from the tests it was possible to deduce some tips in order to optimize the running of the simulator.

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.