Development of an altitude simulator and analysis of the performance and emissions of turbocharged diesel engines at different altitudes
- Autores: Javier Gómez Gil
- Directores de la Tesis: José Ramón Serrano Cruz (dir. tes.)
- Lectura: En la Universitat Politècnica de València ( España ) en 2018
- Idioma: español
- Tribunal Calificador de la Tesis: José María Desantes Fernández (presid.), Octavio Armas Vergel (secret.), Colin Douglas Copeland (voc.)
- Programa de doctorado: Programa de Doctorado en Sistemas Propulsivos en Medios de Transporte por la Universitat Politècnica de València
- Materias:
- Enlaces
- Tesis en acceso abierto en: RiuNet
- Resumen
In the last decades, the internal combustion engines research has been focused in the reduction of the fuel consumption and emissions while keeping constant the performance. Besides, in the last years the pressure is increasing even more to the engine manufacturers. The new homologation is a big challenge, mainly because of the introduction of the real driving emissions cycles, which will force to homologate the cars under real driving conditions, more dynamic and with an extended range of ambient conditions. The ambient altitude can reach up to 1300 meters above sea level.
Nowadays, the manufacturers have different ways to test the engines and cars in altitude conditions. Real altitude tests, where the car, engineers and testing systems have to be displaced to an altitude place during long periods of time. The other solution is to test the car in a hypobaric chamber, where the pressure can be controlled. However, these chambers are expensive, difficult to operate and intensive in space and resources.
In the present thesis, an altitude simulator is developed, which will introduce another alternative to test engines in altitude. In this altitude simulator, the engine or car is at room pressure and only its intake and exhaust pipes are at the tested altitude. In the thesis, it is described the altitude simulator operation principle, its different elements and their effect on the altitude simulator performance, as well as the control strategies applied to control the different variables and elements.
In order to proof the potential of the altitude simulator, a turbocharged diesel engine is tested at different altitudes and its performance and emissions results are compared with those obtained in a hypobaric chamber. Also the engine is tested at the different altitudes in dynamic cycles and its performance and emissions are analyzed, showing that the engine control strategy when it is operating in altitude is focused in the protection of the different elements without taking into account the emissions. For these reason, it is important to study different strategies to reduce engine emissions in altitude.
Finally, different parametric studies changing different geometries of the engine valves and exhaust manifold in order to analyze its effect on the aftertreatment inlet temperature and the specific fuel consumption, as a way to reduce the time that it takes to the aftertreatment to reach the target conversion efficiency temperature.
