COMPUTATIONAL AND EXPERIMENTAL DETERMINATION OF ENERGY LOSS OF THE OPERATING FLUID IN THE INTAKE SYSTEM OF THE AUTOMOBILE PISTON PNEUMATIC ENGINE USING THE EXERGY METHOD

O. Voronkov, Anatolij Ivanovych Charchenko, Igor Nikitchenko, Y. B. Novikova, E. Teslenko, A. Nazarov
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Abstract

The application exergy method of the thermodynamic analysis for determining the energy loss of the operating fluid in the intake system of the automobile piston pneumatic engine using experimental data of its engine test rigs has been considered. The analysis of the performed exergy calculational and experimental research on the evaluation of energy loss in the intake system of the engine for current modes of its operation has been presented. The sample of a piston pneumatic engine for a combined automobile power unit created at the ICE Department of KhNAHU requires further improving and developing especially such components and systems as those connected to the burn process. A compressed air intake system is one of them. Compressed air is not only some working fluid for a pneumatic engine but the energy source for its intake system. The energy loss factor like reliability and durability is referred to the performance and efficiency factors. The object of the study is a pneumatic engine created by converting a gasoline four-cylinder four-stroke ICE at the ICE Department of KhNAHU. The experimental research was carried out by laboratory engine test rigs of the pneumatic engine with speed characterization provided that two thermodynamic parameters of compressed air at the intake were kept constant for each characteristic: pressure p s = idem and temperature Т s = 293 K. In each test mode all external parameters of the pneumatic engine were recorded and indicator diagrams of the first cylinder were taken. Each speed characteristic consisted of 6–8 modes p s = idem and Т s = 293 К = idem with changing the rotational rate of the crankshaft n, rpm, from minimally stable (about n=200 rpm) to maximum possible n = 1000 ± 50 rpm It should be noted that there is an operating fluid pressure drop in the intake system chamber due to available inconvertibilities: throttling in the test port, hydraulic loss along the intake port as a result of fluid friction, swirls and other gas-dynamic phenomena. The exergy loss of the operating fluid enthalpy in the intake system D вп =Е вп -Е нап with the intake pressure р s = 0.5 MPais 13.3 kW, with the intake pressure р s = 0.7 MPa is 15.0 kW, with the intake pressure р s = 0.9 MPa is 16.9 kW, with the intake pressure р s = 1.1 MPa is 19.7 kW.
用火用法计算和实验确定了汽车活塞式气动发动机进气系统中工作流体的能量损失
考虑了利用汽车活塞式气动发动机试验台的实验数据,应用热力学分析的火用法确定发动机进气系统工作流体的能量损失。对发动机进气系统在当前运行模式下的能量损失评估进行了火用计算和实验研究分析。KhNAHU ICE部门创建的用于组合汽车动力单元的活塞气动发动机样品需要进一步改进和开发,特别是与燃烧过程相关的组件和系统。压缩空气进气系统就是其中之一。压缩空气不仅是气动发动机的工作流体,而且是其进气系统的能量来源。像可靠性和耐久性这样的能量损失因素是指性能和效率因素。该研究的对象是由KhNAHU ICE部门的汽油四缸四冲程ICE改装而成的气动发动机。在速度表征气动发动机的实验室发动机试验台上进行了实验研究,每个特性都保持进气处压缩空气的两个热力学参数恒定:压力p s = idem,温度Т s = 293 K。在每个试验模式下,记录气动发动机的所有外部参数,并拍摄第一缸的示功图。每个速度特性由6 - 8 p s =同上的模式和Тs = 293К=同上的改变曲轴的转动速度n, rpm,从最小稳定(n = 200 rpm),最大可能n = 1000±50 rpm应该注意的是,有一个操作流体压降的进气系统室由于可用不能兑换:节流在测试端口,水力损失在进气口由于流体摩擦,漩涡和其他气动现象。进气系统中工作液焓的火用损失D вп =Е вп -Е нап在进气压力为0.5 MPa时为13.3 kW,在进气压力为0.7 MPa时为15.0 kW,在进气压力为0.9 MPa时为16.9 kW,在进气压力为1.1 MPa时为19.7 kW。
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