Inflow boundary condition for one-dimensional gas dynamics simulation code of internal combustion engine manifolds

Author(s):  
D Chalet ◽  
P Chesse ◽  
J-F Hetet ◽  
X Tauzia
2021 ◽  
Author(s):  
Thiago Ebel ◽  
Mark Anderson ◽  
Parth Pandya ◽  
Mat Perchanok ◽  
Nick Tiney ◽  
...  

Abstract When developing a turbocharged internal combustion engine, the choice of turbocharger is usually based on designer experience and existing hardware. However, proper turbocharger design relies on matching the compressor and turbine performance to the engine requirements so that parameters such as boost and back pressure, compressor pressure ratio, and turbine inlet temperatures meet the needs of the engine without exceeding its allowable operating envelope. Therefore, the ultimate measure of a successful turbocharger design is how well it is matched to an engine across various operating conditions. This, in turn, determines whether a new turbocharger is required, or an existing solution can be used. When existing turbocharger solutions are not viable, the engine designer is at a loss on how to define a new turbocharger that meets the desired performance requirements. A common approach in industry has been to scale the performance of an existing turbocharger (compressor and turbine maps) and take these requirements for Original Equipment Manufacturers to possibly match it with a real machine. However, the assumptions made in a basic scaling process are quite simplistic and generally not satisfactory in this situation. A better approach would be to use a validated meanline model for a compressor and turbine instead, allowing to perform an actual preliminary design of such components. Such approach allows to link the engine performance requirements in a very early stage of te component design project and it guides the designer for the design decisions, such as rotor size, variable geometry nozzles, diameter, or shroud trims and others. Therefore, a feasible solution is more likely with design less iterations. This paper describes a methodology for an integrated approach to design and analyze a turbocharged internal combustion engine using commercially available state-of-the-art 1D gas dynamics simulation tool linked to two powerful turbomachinery meanline programs. The outputs of this analysis are detailed performance data of the engine and turbocharger at different engine operating conditions. Two case studies are then presented for a 10-liter diesel truck engine. The first study demonstrates how the programs are used to evaluate an existing engine and reverse engineer an existing turbocharger based only on the available performance maps. Then a second study is done using a similar approach but redesigning a new turbocharger (based on the reverse engineered one) for an increased torque output of the same engine.


2020 ◽  
Vol 142 (2) ◽  
Author(s):  
Jiajia Waters ◽  
David B. Carrington

Abstract The Los Alamos turbulent reactive flow researchers, our modelers, and simulation code developers have succeeded in providing the engine research and development community an encompassing, robust, accurate, and easy-to-use software for engine modeling or simulations. This software is now known as the fearce Toolkit. In this paper, we discuss the physics present in the engine by discussing the methods we have employed to solve the model equations within the toolkit. Provided is background on what has been developed recently at LANL for internal combustion engine modeling.


2021 ◽  

The article presents a study and modification of the cooling system of a KAMAZ R6 in-line diesel engine using a heat exchanger of the combustion products recirculation system in the Simcenter AMESim one-dimensional simulation software. In the course of the research, the problems of engine overheating when using a heat exchanger of the combustion products recirculation system were identified, and possible solutions were proposed and investigated to optimize the temperature level of the coolant in the engine cooling system. Keywords one-dimensional modeling, 1D modeling, ICE, internal combustion engine, heat exchange, cooling system, CO, heat exchanger, heat exchanger, TA


2015 ◽  
Author(s):  
Fábio de Castro Radicchi ◽  
João Marcos Gomes Vieira ◽  
Leonardo Fonseca ◽  
José Eduardo Mautone Barros ◽  
Ramón Molina Valle

Author(s):  
David B. Carrington ◽  
Jiajia Waters

The Los Alamos turbulent reactive flow researchers, our modelers and simulation code developers have succeeded in providing the engine research and development community an encompassing, robust, accurate and easy to use software for engine modeling or simulations. This software is now known as the FEARCE Toolkit. In this paper we discuss the physics present in the engine by discussion the methods we’ve employed to solve the model equations within the toolkit. Provided are background on what has been developed recently at LANL for internal combustion engine modeling.


Author(s):  
Nicolas-Ivan Hatat ◽  
David Chalet ◽  
François Lormier ◽  
Pascal Chessé

The performance of an internal-combustion engine is directly related to the fuel quantity that can react with the oxygen in the air during the exothermic oxidation step, also called combustion. Thus, the amount of fuel introduced is intrinsically linked to the air volume that can be admitted into the cylinder (air filling of the cylinder). Hence keeping the air in the cylinder is one of the most important concepts to predict in simulations. Nevertheless, the phenomenon of air filling depends on many parameters. Also, the discharge coefficients, and the impact of the piston presence near the valves on the flow, during valve overlap are investigated. For this, a digital flow bench is constructed to reproduce a series of tests carried out on a flow test bench functioning as a result of the reduction in the pressure. In this paper, the engine studied is a 125 cm3 single-cylinder four-stroke atmospheric type with two valves. Thus, the idea of this paper is to treat the case of engines with large valve overlaps as small engines or engines with variable valve timing. First, traditional tests through a single valve are performed. The forward and reverse directions are systematically tested to ensure proper operation of the digital testing, and to determine the differences between tests and simulations in the case of conventional configurations. Then, the flow through the entire cylinder head, i.e. the intake valve–cylinder with piston–exhaust valve system, is tested and studied. The aim is to compare the results obtained by the tests and the simulations during the valve overlap period. Significant differences were highlighted between the rates measured in one-dimensional simulations and in the tests. It was noteworthy that the one-dimensional code overestimated the mass passing through the system during valve overlap by about one fifth of the estimated mass passing through the system from the results obtained with the test rig.


2018 ◽  
Vol 90 (6) ◽  
pp. 906-913 ◽  
Author(s):  
Mohammad Reza Khodaparast ◽  
Mohsen Agha Seyed Mirza Bozorg ◽  
Saeid Kheradmand

Purpose The purpose of this paper is the selection and arrangement of turbochargers set for internal combustion engine which could keep engine power in an altitude of up to 12.2 km above sea level. Design/methodology/approach In the current research, the target engine, a one-dimensional four-stroke 1,600 cc piston engine has been simulated and the manufacturer’ results have been validated. Depending on engine size, three proper types of Garret turbochargers GT30, GT25 and GT20 were selected for this engine. Then, the engine and a combination of two turbochargers have been modeled one-dimensionally. A control system was used for regulation of different pressure ratios between the two turbochargers. Findings The parametric analysis shows that using the combination of GT20, GT30 turbochargers with a properly controlled pressure ratio leads to a constant output power with little changes at different altitudes which enable achieving an altitude of 12.2 km for the target engine. Practical implications Adaptation of the internal combustion engine with a twin turbocharger using one-dimensional modeling. Originality/value The one-dimensional analysis provided an overall picture of the effective performance of turbochargers functioning in different altitudes and loads. It presents a new method for adopting of turbochargers set with internal combustion engines for propulsion medium-altitude aircraft.


2015 ◽  
Vol 798 ◽  
pp. 224-228
Author(s):  
F.C. Radicchi ◽  
J.M.G. Vieira ◽  
Leonardo Fonseca ◽  
Ramon Molina Valle ◽  
José Eduardo Mautone Barros

The work aims to model a spark ignition reciprocating Internal Combustion Engine - ICE. A code was built in Object Pascal to simulate another ICE and now it is being adapted to this research single-cylinder engine using commercial ethanol. The model describes in-cylinder gas by conservation equations, including the momentum conservation, and solves combustion wave equations, such that detonation and deflagration are calculated by the same set of formulas. Adjustments were made to get a proper discharge coefficient for the valves and represent the internal geometry. The mass flow rate calculated by the program differed in only 1% of the experimental value. The maximum pressures from combustion graphs differed in less than 1% too and their curves were similar. Other parameters of interest, also found to be close to the experimental ones, are presented and discussed. The code also showed as a good result the simulation time, which was approximately two minutes.


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