This article describes the first development phase of a centrifugal compressor with variable geometry which is designed to match the needs of future heavy-duty engines. Requirements of truck engines are analyzed, and their impact on the properties of the compressor map is evaluated in order to identify the most suitable kind of variable geometry. Our approach utilizes the transformation of engine data into pressure ratio and mass flow coordinates that can be displayed and interpreted using compressor maps. One-dimensional and three-dimensional computational fluid dynamics fluid flow calculations are used to identify loss mechanisms and constraints of fixed geometry compressors. Linking engine goals and aerodynamic objectives yields specific recommendations on the implementation of the variable geometry compressor.

The work was concerned with the design, analysis and basic demonstration of a novel hydraulically assisted fixed geometry turbocharger system intended to help overcome some of the transient issues associated with current automotive boosting technologies. The novel system was based upon use of relatively lightweight parts, where kinetic energy is recovered during vehicle braking, stored in a simple hydraulic accumulator and then used later on to rapidly accelerate the engine's turbocharger. The turbocharger is fitted with a replacement centre housing enclosing a small impulse turbine, rigidly mounted to the turbocharger shaft and powered by a jet of oil. The aim is one of helping the engine to accelerate the vehicle while operating in a region of much higher brake efficiency due to the reduction in exhaust backpressure when compared with competing variable geometry and/or compound boosting technologies. The specific tasks involved concept design and computational analysis, including specification of the turbine type and geometry together with the associated hydraulic parts. A production turbocharger was reverse engineered to confirm the feasibility of packaging the hydraulic turbine system into the centre housing of a typical fixed geometry design. Finally an experimental rig was designed and manufactured to allow basic demonstration of the system, with speeds of up to ~90000 rpm @ 200 bar pressure from the pump via the accumulator achieved in ~0.8 seconds and clear potential for further optimisation. This hydraulic boosting system is capable of attaining 70% efficiency (a product of 0.85 from the oil pump, 0.95 from the hydraulic accumulator and 0.88 of Pelton wheel). The system has higher power density at low cost compared to the main competitor ‘E Boosting - with efficiency in the region of 90%’. The cost of E boosting and need for 48 volt battery makes it less favourable compared to the hydraulic turbine system. The concept has been shown to offer significant potential to assist a turbocharger to spool up via a Novel Hydraulic Kinetic Energy Recovery System approach.

Aim of this diploma thesis is the modification of naturally aspirated engine for Formula Student competition to turbocharged version. Modification which were made are based on the issue knowledge and calculations. The input data were obtained from 3D scanning and measurements, at the school laboratories. All 3D models were created in Pro / Engineer. Input data for the computional analysis was developed in Lotus Engine Simulation. Computational analysis was performed in ANSYS by finite element method. Calculations had to simulate a piston behavior at the critical situations where the engine is under the maxiumum load.

Aim of this diploma thesis is the turbocharger design calculation for single cylinder SI engine for Formula Student. This thesis includes a mathematical model of the engine, which is created in the Lotus Engine Simulation. This model applies for tuning the regulation of turbocharger charging pressure. Lotus uses the turbine waste gate valve for this regulation. The results of the simulation are the charging pressure,lengths of the intake manifold and etc. These parameters ensure the optimal engine qualities. The knowlege and results of the simulations are summarized at the conclusion.

Orientador: Milton Dias Júnior / Dissertação (mestrado) - Universidade Estadual de Campinas, Faculdade de Engenharia Mecânica / Made available in DSpace on 2018-08-25T09:48:12Z (GMT). No. of bitstreams: 1 Nomura_PaulaWatanabe_M.pdf: 4842075 bytes, checksum: fb2b3e20baadde947cb7b9aad16227d8 (MD5) Previous issue date: 2014 / Resumo: As novas legislações de emissões demandam das montadoras de veículos automotores, o desenvolvimento de tecnologias para melhorar o consumo de combustível e emissão de poluentes. Seguindo esta tendência, os sistemas de turbocompressores inovam junto e lançam ao mercado novas arquiteturas de turbos. Uma delas é o turbocompressor regulado de dois estágios, que otimiza a eficiência em um intervalo de rotação mais amplo. Neste sistema, há dois turbocompressores: o estágio de baixa pressão e de alta pressão. O primeiro tem maior influência nas baixas rotações, enquanto o segundo nas altas rotações do motor. Entre os dois estágios, existe uma válvula bypass que controla a passagem do gás de escape para o estágio de baixa pressão, evitando assim, sobrecarregar o estágio de alta pressão. Esta válvula bypass é composta por um eixo rotativo e uma bucha fixa, e exatamente entre estes dois componentes foi detectado desgaste, aumentando as folgas e causando vazamento de gás. Com o objetivo de diminuir este vazamento e resolver o problema, uma investigação sobre este desgaste prematuro foi iniciada dentro da empresa onde a autora da presente dissertação trabalha. Neste trabalho a análise de forças das condições estática e dinâmica que envolve a bucha e o eixo, as forças e momentos para abrir e fechar o prato da válvula, e as equações de movimento são apresentadas. A análise experimental inclui medições feitas em dois motores reais: um deles conectado a um dinamômetro e o outro instalado em um veículo usado na mesma aplicação onde o desgaste excessivo foi observado. Além disso, a análise de desgaste de dez pares bucha-eixo que retornaram de testes de durabilidade é apresentado. A comparação do desgaste entre dois sistemas de bucha e eixo foi realizada. Ambos os sistemas rodaram na mesma condição, exceto pela frequência de operação da válvula de controle, assim a influência desta frequência pôde ser analisada. Ao final, todo este dado foi coletado e usado para o cálculo de taxa de desgaste que avalia a influência de diferentes parâmetros de design sobre a taxa de desgaste / Abstract: The new emission legislations demand, from vehicle manufactures the development of technologies to improve fuel consumption and pollutants emission. Following this trend, the turbocharging systems innovate together and release new turbocharger architectures in the market. One of them is the regulated-two-stages turbocharger, which optimizes the efficiency in a broader engine speed range. In this system, there are two turbochargers, the high and low pressure stages. The former has a bigger influence on the low engine speeds, and the latter in the higher engine speeds. Between both stages there is a bypass valve that controls the gas flow to the low pressure stage, avoiding overpressure in the high pressure stage. This bypass valve is composed by a rotating shaft and a fixed bushing, and exactly between these two components it was detected wear, increasing the clearances and causing gas leakage. In order to reduce this leakage and solve the problem, an investigation about this premature wear has started inside the company where the author of the present dissertation works. In the present work the force analysis of the static and dynamic conditions that involve the shaft and bushing, the forces and momentum to open and close the valve plate, and the equations of motion are presented. The experimental analysis includes measurements made on two real engines: one of them connected to a dynamometer and the other installed on a vehicle used on the same application where the excessive wear was observed. Also, the wear analysis of ten shafts and bushings returned from durability tests is presented. The wear comparison between two shaft-bushing systems was performed. Both systems run in the same condition except for the control valve operational frequency, so the influence of this frequency could be evaluated. In the end, this entire data base collected could be used as input to a wear rate calculation that evaluates the influence of different design parameters on the wear rate / Mestrado / Mecanica dos Sólidos e Projeto Mecanico / Mestra em Engenharia Mecânica

This article describes the first development phase of a centrifugal compressor with variable geometry which is designed to match the needs of future heavy-duty engines. Requirements of truck engines are analyzed, and their impact on the properties of the compressor map is evaluated in order to identify the most suitable kind of variable geometry. Our approach utilizes the transformation of engine data into pressure ratio and mass flow coordinates that can be displayed and interpreted using compressor maps. One-dimensional and three-dimensional computational fluid dynamics fluid flow calculations are used to identify loss mechanisms and constraints of fixed geometry compressors. Linking engine goals and aerodynamic objectives yields specific recommendations on the implementation of the variable geometry compressor.

Heat transfer plays an important role in affecting an on-engine turbocharger performance. However, it is normally not taken into account for turbocharged engine simulations. Generally, an engine simulation based on one-dimensional gas dynamics uses turbocharger performance maps which are measured without quantifying and qualifying the heat transfer, regardless of the fact that they are measured on the hot-flow or cold-flow gas-stand. Since heat transfer situations vary for on-engine turbochargers, the maps have to be shifted and corrected in the 1-D engine simulation, which mass and efficiency multipliers usually do for both the turbine and the compressor. The multipliers change the maps and are often different for every load point. Particularly, the efficiency multiplier is different for every heat transfer situation on the turbocharger. The heat transfer leads to a deviation from turbocharger performance maps, and increased complexity of the turbocharged engine simulation. Turbochargers operate under different heat transfer situations while they are installed on the engines. The main objectives of this thesis are: heat transfer modeling of a turbocharger to quantify and qualify heat transfer mechanisms, improving turbocharged engine simulation by including heat transfer in the turbocharger, assessing the use of two different turbocharger performance maps concerning the heat transfer situation (cold-measured and hot-measured turbocharger performance maps) in the simulation of a measured turbocharged engine, prediction of turbocharger walls’ temperatures and their effects on the turbocharger performance on different heat transfer situations. Experimental investigation has been performed on a water-oil-cooled turbocharger, which was installed on a 2-liter GDI engine for different load points of the engine and different heat transfer situations on the turbocharger by using insulators, an extra cooling fan, radiation shields and water-cooling settings. In addition, several thermocouples have been used on accessible surfaces of the turbocharger to calculate external heat transfers. Based on the heat transfer analysis of the turbocharger, the internal heat transfer from the bearing housing to the compressor significantly affects the compressor. However, the internal heat transfer from the turbine to the bearing housing and the external heat transfer of the turbine housing mainly influence the turbine. The external heat transfers of the compressor housing and the bearing housing, and the frictional power do not play an important role in the heat transfer analysis of the turbocharger. The effect of the extra cooling fan on the energy balance of the turbocharger is significant. However, the effect of the water is more significant on the external heat transfer of the bearing housing and the internal heat transfer from the bearing housing to the compressor. It seems the radiation shield between the turbine and the compressor has no significant effect on the energy balance of the turbocharger. The present study shows that the heat transfer in the turbocharger is very crucial to take into account in the engine simulations. This improves simulation predictability in terms of getting the compressor efficiency multiplier equal to one and turbine efficiency multiplier closer to one, and achieving turbine outlet temperature close to the measurement. Moreover, the compressor outlet temperature becomes equal to the measurement without correcting the map. The heat transfer situation during the measurement of the turbocharger performance influences the amount of simulated heat flow to the compressor. The heat transfer situation may be defined by the turbine inlet temperature, oil heat flux and water heat flux. However, the heat transfer situation on the turbine makes a difference on the required turbine efficiency multiplier, rather than the amount of turbine heat flow. It seems the turbine heat flow is a stronger function of available energy into the turbine. Of great interest is the fact that different heat situations on the turbocharger do not considerably influence the pressure ratio of the compressor. The turbine and compressor efficiencies are the most important parameters that are affected by that. The component temperatures of the turbocharger influence the working fluid temperatures. Additionally, the turbocharger wall temperatures are predictable from the experiment. This prediction enables increased precision in engine simulations for future works in transient operations. / QC 20120504