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Analysis of SI and HCCI Combustion in a Two-Stroke Opposed-Piston Free-Piston Engine

机译:两冲程对抗活塞自由活塞发动机中Si和HCCI燃烧分析

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The German Aerospace Center (DLR) is developing a free-piston engine as an innovative internal combustion engine for the generation of electrical power. The arrangement of the Free Piston Linear Generator (FPLG) in opposed-piston design consists of two piston units oscillating freely, thereby alternately compressing the common combustion chamber in the center of the unit and gas springs on either side. Linear alternators convert the kinetic energy of the moving pistons into electric energy. Since the pistons are not mechanically coupled to a crank train, the bottom and top dead centers of the piston movement can be varied during operation e.g. to adjust the compression ratio. Utilizing these degrees of freedom, the present paper deals with the analysis of different combustion processes in a port scavenged opposed-piston combustion chamber prototype. This contains the experimental investigation of spark ignition (SI) as well as the transition to homogeneous charge compression ignition (HCCI). Based on test bench results, a 3D-CFD model, which has been used to develop the first prototype, is calibrated by actual measurements. The simulation results enable a deeper analysis of scavenging and in-cylinder processes exceeding the measurement possibilities on a test bench.
机译:德国航空航天中心(DLR)正在开发自由活塞发动机作为一种创新的内燃机,用于产生电力。自由活塞线性发生器(FPLG)的布置在相对的活塞设计中由两个活塞单元自由振荡,从而将公共燃烧室压制在装置的中心和两侧的气体弹簧中。线性交流发电机将移动活塞的动能转换成电能。由于活塞没有机械地联接到曲柄列车,因此在操作期间可以改变活塞运动的底部和顶部死亡中心。调整压缩比。利用这些自由度,本文涉及在港口清除的相对活塞燃烧室原型中的不同燃烧过程的分析。这包含火花点火(Si)的实验研究以及均匀电荷压缩点火(HCCI)的过渡。基于测试台面结果,通过实际测量校准了用于开发第一个原型的3D-CFD模型。仿真结果能够更深入地分析超出测试台上的测量可能性的清除和缸内过程。

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