螺旋桨负荷波动对稀燃天然气发动机部分负荷性能和排放的影响

IF 5.4 2区 工程技术 Q1 ENGINEERING, AEROSPACE
S. Tavakoli , J. Schramm , E. Pedersen
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引用次数: 0

摘要

为稀燃天然气发动机提供稳定的燃烧一直是一个巨大的挑战,特别是在低负荷运行时。在瞬态海况下,由于不规则的时变载荷,还存在额外的问题。因此,本研究通过对某型船用火花点火稀燃天然气发动机的整机模拟,对其部分负荷运行进行了研究。发动机的基本部件建模,包括空气歧管,进气阀,燃油系统,控制器,燃烧室,排气阀,排气歧管和涡轮增压器。在稳态下,模拟的排放化合物的结果与25%至100%负载的测量数据进行了比较。在瞬态工况下,在约50 min的采样时间内,从船舶记录数据中选取燃油流量和涡轮增压器输出,并与仿真结果进行比较。该模型在预测发动机的稳态和瞬态响应方面具有很大的潜力。对发动机在部分负荷瞬态工况下的模拟表明,稀燃燃气发动机的未燃烃形成(即甲烷滑脱)多于部分负荷稳态。甲烷漏失的增加是由于低负荷燃烧不稳定和这种瞬态条件下的火焰熄灭。发动机测量数据显示,在25%负荷下,甲烷漏失量是100%负荷下的两倍。然而,在瞬态条件下的模拟输出证实了甲烷滑移比等效稳态负荷增加了四倍以上。此外,由于缸内温度较低,稀燃燃气发动机在稳定状态下部分负荷运行时释放的氮氧化物较少。在瞬态工况下,过量空气比具有显著的不稳定性。由于这种不稳定性,在负载上升期间的瞬时时间步长中存在丰富的混合。因此,它将导致异常高的NOX量,并且是等效稳态输出的两倍以上。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Effects of propeller load fluctuations on performance and emission of a lean-burn natural gas engine at part-load conditions

Providing stable combustion of lean-burn natural gas engines was always a big challenge, particularly during a low load operation. In transient sea conditions, there is an additional concern due to irregular time-varying loads. Therefore, this study aimed at investigating the part-load operation of a marine spark-ignition lean-burn natural gas engine by simulating the entire engine. The engine's essential components are modeled, including air manifold, intake valves, fuel system, controllers, combustion chamber, exhaust valves, exhaust manifold and turbocharger.

In steady-state, the results of emission compounds from modeling have been compared to measured data from 25% to 100% loads. For transient conditions, for the sample time of about 50 min, the fuel flow and turbocharger output are selected from the vessel logged data and compared with the simulation results. The model has shown the great potential of predicting the engine response throughout the steady-state and transient conditions. Simulating the engine at part-load transient condition showed that the unburned hydrocarbon formation, known as methane slip in lean-burn gas engines, is more than the part-load steady-state. This increase of methane slip is due to the combustion instability in lower loads and flame extinguishing in such transient conditions. The engine measured data shows a double amount of methane slip in a 25% load than the 100% load in steady-state. However, the simulation output in the transient conditions confirms an increase in methane slip over four times than equivalent steady-state load. Moreover, the lean-burn gas engine releases less NOX in part-load operation in a steady-state due to lower in-cylinder temperature. In transient conditions, there is remarkable instability in excess air ratio. Due to this instability, there is a rich mixture in instantaneous time steps during loads up. Therefore, it will result in an unusually high amount of NOX, and more than two times in comparison with the equivalent steady-state output.

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来源期刊
CiteScore
7.50
自引率
5.70%
发文量
30
期刊介绍: Propulsion and Power Research is a peer reviewed scientific journal in English established in 2012. The Journals publishes high quality original research articles and general reviews in fundamental research aspects of aeronautics/astronautics propulsion and power engineering, including, but not limited to, system, fluid mechanics, heat transfer, combustion, vibration and acoustics, solid mechanics and dynamics, control and so on. The journal serves as a platform for academic exchange by experts, scholars and researchers in these fields.
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