首页> 外文会议>ASME Internal Combustion Engine Division technical conference >REAL-TIME MONITORING OF COMBUSTION INSTABILITY IN A HOMOGENEOUS CHARGE COMPRESSION IGNITION (HCCI) ENGINE USING CYCLE-BY-CYCLE EXHAUST TEMPERATURE MEASUREMENTS
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REAL-TIME MONITORING OF COMBUSTION INSTABILITY IN A HOMOGENEOUS CHARGE COMPRESSION IGNITION (HCCI) ENGINE USING CYCLE-BY-CYCLE EXHAUST TEMPERATURE MEASUREMENTS

机译:使用循环逐循环排气温度测量,实时监测均匀电荷压缩点火(HCCI)发动机的燃烧不稳定性

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This paper describes an experimental study concerning the feasibility of monitoring the combustion instability levels of an HCCI engine based upon cycle-by-cycle exhaust temperature measurements. The test engine was a single cylinder, four-stroke, variable compression ratio Cooperative Fuel Research (CFR) engine coupled to an eddy current dynamometer. A rugged exhaust temperature sensor equipped with special signal processing circuitry was installed near the engine exhaust port. Reference measurements were provided by a laboratory grade, water-cooled cylinder pressure transducer. The cylinder pressure measurements were used to calculate the Coefficient of Variation of Indicated Mean Effective Pressure (COV of IMEP) for each operating condition tested. Experiments with the HCCI engine confirmed that cycle-by-cycle variations in exhaust temperature were present, and were of sufficient magnitude to be captured for processing as high fidelity signal waveforms. There was a good correlation between the variability of the exhaust temperature signal and the COV of IMEP throughout the operating range that was evaluated. The correlation was particularly strong at the low levels of COV of IMEP (2-3%), where production engines would typically operate. A real-time combustion instability signal was obtained from cycle-by-cycle exhaust temperature measurements, and used to provide feedback to the fuel injection control system. Closed loop operation of the HCCI engine was achieved in which the engine was operated as lean as possible while maintaining the COV level at or near 2.5%.
机译:本文介绍了关于基于循环循环排气温度测量监测HCCI发动机的燃烧不稳定水平的可行性的实验研究。测试引擎是单个气缸,四冲程,可变压缩比协同燃料研究(CFR)引擎,耦合到涡流测功机。在发动机排气口附近安装配备有特殊信号处理电路的坚固的排气温度传感器。通过实验室等级,水冷筒压力传感器提供参考测量。用于计算测试的每个操作条件的显示平均有效压力(IMEP的COV)的变化系数。 HCCI发动机的实验证实,存在排气温度的逐循环变化,并且才能捕获足够的幅度以作为高保真信号波形处理。在评估的整个操作范围内,排气温度信号的可变性与IMEP的COV之间存在良好的相关性。在IMEP的低水平(2-3%)的低水平的COV中的相关性特别强烈,其中生产发动机通常运行。从循环逐循环的排气温度测量获得实时燃烧不稳定信号,并用于向燃料喷射控制系统提供反馈。实现了HCCI发动机的闭环操作,其中发动机尽可能稀薄,同时保持COV水平或接近2.5%。

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