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Waste heat recovery using a novel high performance low pressure turbine for electric turbocompounding in downsized gasoline engines: experimental and computational analysis

机译:使用新型高性能低压涡轮机进行废热回收,用于小型汽油发动机的电动涡轮复合:实验和计算分析

摘要

The development of a high performance LPT (Low Pressure Turbine) for turbocompounding applications in downsized gasoline engine is presented in this paper. The LPT was designed to fill the existing technology gap where no commercially available turbines can operate effectively at low-pressure ratios (1.05-1.3) to drive an electric generator with 1.0 kW power output. The newly designed LPT geometry was tested at Imperial College under steady-state conditions; a maximum total-to-static efficiency, ?t-s 75.8% at pressure ratio, PR ˜ 1.08 was found.The LPT performance maps were then used for a validated 1-D engine model in order to assess the effect of turbocompounding on BSFC (Brake Specific Fuel Consumption). Then a prototype of the LPT was tested in the post catalyst position on a 1.0 L gasoline engine for different operating conditions. The test results showed that reduction in BSFC of 2.6% could be achieved.With the post-catalyst position selected, a KP (key-point) engine speed/load analysis was performed in order to project an overall NEDC (New European Drive Cycle) fuel consumption benefit for the LPT in a mechanical turbocompounding configuration, as well as an overall power benefit calculation. Finally, a sensitivity study indicated what the power could be off-cycle.
机译:本文介绍了用于小型汽油机涡轮复合应用的高性能LPT(低压涡轮)的开发。 LPT旨在填补现有技术空白,在该空白中,没有任何商用涡轮机可以在低压比(1.05-1.3)下有效运行,以驱动功率输出为1.0 kW的发电机。新设计的LPT几何在帝国大学的稳态条件下进行了测试;发现最大总静态效率在压力比为PR时为75.8%,PR约为1.08。然后将LPT性能图用于经过验证的一维发动机模型,以评估涡轮增压对BSFC的影响(制动特定燃油消耗)。然后在不同的工况下,在1.0升汽油发动机上的催化剂后位置测试LPT的原型。测试结果表明,BSFC降低了2.6%。选择了催化剂后位置后,进行了KP(关键点)发动机转速/负载分析,以预测整个NEDC(新欧洲行驶周期)机械涡轮复合配置中LPT的燃油消耗效益,以及总的功率效益计算。最后,一项敏感性研究表明电源可能会关闭。

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