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Experiment investigation on the performance and regulation rule of two-stage turbocharged diesel engine for various altitudes operation

机译:两级涡轮增压柴油机在不同高度运行的性能和调节规律的实验研究

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摘要

To satisfy intake demand under high-altitude condition, two-stage turbocharging system is matched for diesel engine. However, it is necessary to regulate turbocharging system at low altitude due to decline of overall system efficiency. Moreover, regulation rule of turbocharging system, in terms of regulation ability and overall efficiency, which is critical to engine performance and unclear for various altitudes operation so that regulation strategy of turbocharging system depends on numerous calibration. In this paper, regulation rules at various altitudes are investigated by experiments. Test result indicates regulation ability increases as altitudes rises up and provides less excess air coefficient with constant regulation area. Whereas, overall efficiency presents disparate tends at different altitude. Output torque and fuel consumption continue to deteriorate as the bypass valve opens at high altitude condition, while can be improved below 2000 m with reasonable regulation area due to greater overall efficiency. The effect of altitude on regulation area boundary and scope are acquired. Finally, optimal regulation strategy at various altitudes is proposed. Experiment results manifest the maximal increment of overall system efficiency achieves 7.3% and leads to fuel consumption reduction of 13.9 g/kW h under 2200r/min and 0 m condition, compared to fixed turbocharging system.
机译:为了满足高海拔条件下的进气需求,柴油发动机配套了两级涡轮增压系统。但是,由于整体系统效率的下降,有必要在低空调节涡轮增压系统。此外,涡轮增压系统的调节规则,就调节能力和整体效率而言,对发动机性能至关重要,并且对于各种高度的运行情况尚不清楚,因此,涡轮增压系统的调节策略取决于大量的校准。本文通过实验研究了不同高度的调节规则。测试结果表明,调节能力随海拔的升高而增加,并且在恒定调节面积的情况下提供的空气系数较小。而在不同的高度,总体效率呈现出不同的趋势。当旁通阀在高海拔条件下打开时,输出扭矩和燃油消耗继续恶化,而由于整体效率更高,可以在合理的调节面积下将其提高到2000 m以下。获得了海拔高度对管制区边界和范围的影响。最后,提出了不同海拔高度的最优调节策略。实验结果表明,与固定式涡轮增压系统相比,在2200r / min和0 m的条件下,系统总效率的最大增量达到7.3%,并降低了13.9 g / kW h的油耗。

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