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Reduced Convective Combustion Chamber Wall Heat Transfer Losses of Hydrogen-Fueled Engines by Vortex-Stratified Combustion - Part 2: Numerical Analyses

机译:通过涡旋分层燃烧减少对流燃烧室壁传热损耗氢燃料发动机 - 第2部分:数值分析

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In this second of two parts, the fundamentals of convective wall heat transfer losses are elucidated in the context of the desired objective toward its reduction in a direct-injected, hydrogen-fueled internal combustion engine. A comparative, transient 2D CFD analysis evaluated at 4500 RPM between a combustion chamber design representing current practice and the here-introduced “vortex-stratified combustion” process finds an approximately 50% reduction in the peak convective flux with the latter. The simulation results show that reduced heat flux of the vortex approach is driven by the combination of two effects: The first is finite-time diffusive mixing getting outpaced by the replenishment of pure air being introduced preferentially along the circumference of the combustion chamber due to the Coand effect; this results in a distinct radial charge stratification during mixture preparation in the compression stroke, with a fuel-concentrated center and essentially pure air at the periphery. The second effect is the forced-segregation of different density reactants during the course of the combustion process caused by large body forces that result from the gravitational acceleration of the rapidly rotating charge, thereby constraining the combustible mixture and the flame to some distance from the walls. Evidence for this is observed by hot, low-density hydrogen being forced to remain near the center and cooler, heavier oxygen being inhibited from migrating from the outer periphery to react with the aforementioned hydrogen, and the distinct curvature of the radial gas temperature profile at a substantially greater distance from the wall than the thermal boundary layer thickness.
机译:在两个部分中的第二个中,在期望的目的的背景下阐明了对流壁传热损失的基础,朝向其直接注入的氢气燃料的内燃机的降低。在代表当前实践的燃烧室设计和这里引入的“涡旋分层燃烧”过程的燃烧室设计之间以4500rpm评估的比较的瞬态2D CFD分析在后者中发现峰值对流助焊剂的减少约50%。仿真结果表明,由于两种效应的组合驱动了涡旋方法的减少的热量:首先是通过沿着燃烧室的圆周优先引入的纯净空气来超出纯空气的有限时间扩散混合。芯片效应;这导致在压缩冲程中的混合物制备期间具有明显的径向电荷分层,其具有燃料浓缩的中心和在周边的基本上纯净空气。第二次效果是在由快速旋转电荷的重力加速度引起的大体力导致的燃烧过程过程中的强制隔离,从而限制可燃混合物和火焰与壁的一定距离。通过热,低密度氢被迫靠近中心和冷却器来观察到这一点的证据,抑制从外周迁移的较重氧气与上述氢气反应,以及径向气体温度曲线的不同曲率。从壁的距离大于壁的距离而不是热边界层厚度。

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