非对称双涡管涡轮增压重型柴油发动机排气脉冲特性研究

IF 1.1 Q3 TRANSPORTATION SCIENCE & TECHNOLOGY SAE International Journal of Engines Pub Date : 2024-07-24 DOI:10.4271/03-17-06-0048
Liangqin Wu, Jianjiao Jin, Jie Wang, Chenyun Zhang
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引用次数: 0

摘要

非对称双涡管涡轮增压发动机排气脉冲的形状和能量分布特性对非对称双涡管涡轮与发动机的匹配以及非对称双涡管与涡轮的匹配有重要影响。本文研究了非对称双涡管涡轮增压发动机的排气脉冲特性。实验在涡轮试验台和发动机性能台上进行,以确定排气脉冲强度、涡轮流量参数、涡轮等熵能和涡轮效率的运行规律。结果表明,随着发动机转速的增加,小涡轮和大涡轮进气口的排气脉冲强度持续下降。根据排气压力脉冲 "次峰 "两侧波谷极值点的压力偏差,大小涡轮入口处的流量参数随膨胀比的变化分别呈现出 "环形 "或 "蝶形"。此外,涡轮等熵功率的分布趋势与大小涡旋入口处排气压力脉冲的趋势一致。此外,当打开平衡阀时,在涡轮等熵功率脉冲的 "主峰 "和 "次峰 "附近分别出现了 "凹 "和 "凸 "的特征。最后,随着发动机转速的增加,涡轮瞬时效率的波动逐渐减小。在计算涡轮瞬时效率时,需要考虑转子转动惯量的影响,否则可能会出现效率超过 100%的错误现象。
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An Investigation on Exhaust Pulse Characteristics of Asymmetric Twin-Scroll Turbocharged Heavy-Duty Diesel Engine
The shape and energy distribution characteristics of exhaust pulse of an asymmetric twin-scroll turbocharged engine have a significant impact on the matching between asymmetric twin-scroll turbines and engines, as well as the matching between asymmetric twin scrolls and turbine wheels. In this article, the exhaust pulse characteristics of an asymmetric twin-scroll turbocharged engine was studied. Experiments were conducted on a turbine test rig and an engine performance stand to determine the operation rules of exhaust pulse strength, turbine flow parameters, turbine isentropic energy, and turbine efficiency. The results showed that the exhaust pulse strength at the inlets of both the small and large scrolls continuously decreased with the increase of engine speed. And the flow parameters at the inlets of the small and large scrolls exhibited a “ring” or “butterfly” shape with the change of expansion ratio depending on the pressure deviation of the extreme points at the troughs on both sides of the “secondary peak” of the exhaust pressure pulse, respectively. Besides, the distribution trend of turbine isentropic power was consistent with the trend of exhaust pressure pulse at the inlets of the small and large scrolls. Furthermore, when opening the balance valve, it caused the appearance of “concave” and “convex” features near the “main peak” and “secondary peak” of the turbine isentropic power pulses, respectively. Finally, as the engine speed increased, the fluctuation of turbine instantaneous efficiency gradually decreased. When calculating the instantaneous efficiency of the turbine, the influence of the rotor’s rotational inertia needs to be considered, otherwise, there may be a false phenomenon of exceeding 100% efficiency.
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来源期刊
SAE International Journal of Engines
SAE International Journal of Engines TRANSPORTATION SCIENCE & TECHNOLOGY-
CiteScore
2.70
自引率
8.30%
发文量
38
期刊最新文献
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