燃气活塞发动机工作参数的计算与实验研究

V. Kamaltdinov, V. Markov, S. S. Nikiforov
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引用次数: 1

摘要

介绍了活塞式燃气发动机Perkins 4012 TESI工作过程的研究结果。该发动机作为固定热电联产装置的一部分运行,以1500转/分钟的曲轴转速产生电能和热能。在实验研究过程中,记录了一个没有编码器的往复式发动机在从空转到600千瓦的不同负载下的缸内压力。开发并实现了在实验指示图上确定上死点标记位置的技术,并与理论计算图进行了比较。确定了燃烧过程分为两个阶段。主动放热的主要阶段从曲轴旋转开始持续40-50度。加力阶段也有50-80度的持续时间。采用“双维贝函数”程序进行理论计算和研究。确定了燃烧性质的指标和每一阶段燃烧燃料的量。该程序“双韦贝函数”允许充分模拟燃气活塞发动机的工作过程,当它在均质混合物上运行。计算参数值与实验参数值的差异为:具体指标油耗不大于1%;指标效率不大于0.5%;最大燃烧压力不大于1%。该计算模型可用于往复式燃气发动机的现代化和设计,目的是作为自主动力装置的一部分运行。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Calculation and Experimental Studies of the Working Parameters of the Gas Piston Engine
The results of studies of the working process of a piston gas engine Perkins 4012 TESI are presented. The engine operates as a part of a stationary cogeneration installation and generates electric and thermal energy at a crankshaft rotation speed of 1500 rpm. In the course of experimental studies, the pressure in the cylinder of a reciprocating engine without an encoder was recorded at various loads: from idling to 600 kW. The technique for determining the position of the marking of the top dead point on the experimental indicator diagram was developed and implemented when this diagram is compared with the calculated theoretical one. It is established that the combustion process consists of two phases. The main phase of active heat release has the duration of 40–50 degrees from the crankshaft rotation. The afterburning phase also has the duration of 50–80 degrees. Theoretical calculations and studies were carried out using the “Double-Wiebe function” program. The indicators of the nature of combustion and the amount of combustion fuel in each phase are determined. The program “Double-Wiebe function” allowed to adequately simulate the working process of a gas piston engine when it operates on homogeneous mixtures. Differences in the values of the calculated and experimental parameters were: specific indicator fuel consumption is not more than 1%; indicator efficiency is not more than 0.5%; maximum combustion pressure is not more than 1%. The calculation model can be used in the modernization and design of reciprocating gas engines intended for operation as part of autonomous power installations.
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