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Reduced Convective Combustion Chamber Wall Heat Transfer Losses of Hydrogen-Fueled Engines by Vortex-Stratified Combustion - Part 1: Background and Optical Engine Observations

机译:通过涡旋分层燃烧减少氢气燃料发动机的对流燃烧室壁传热损耗 - 第1部分:背景和光学发动机观察

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A vortex-stratified combustion process for hydrogen-fueled reciprocating internal combustion engines is introduced to increase the thermal efficiency by reducing the convective heat transfer losses to the surrounding walls during combustion. The process imposes a highly ordered rotational field upon the charge in a separate, transverse, cylindrically shaped combustion chamber by means of channels that connect with the main chamber enclosed by the engine cylinder and piston. Gaseous hydrogen is injected directly during the compression stroke, while air enters into the combustion chamber tangentially and preferentially along the circumference due to the Coand effect. The two streams entrain one another and develop into a vigorous vortex by virtue of the chamber and channel geometries. As mixing proceeds, the fuel is confined radially from the combination of finite-time diffusion being outpaced by the replenishment of pure air at the periphery, and the centripetal field formed by the rotating flow acting on the different density gas mixture. Combustion takes place with a flame propagation that initially follows the rotation of the bulk flow, and then curls radially inward toward the center. This work investigates the process in a fired, optically accessible 2-stroke hydrogen-fueled direct-injected engine tested at up to 5000 RPM. This paper, the first of two parts, explains the theoretical background; presents the schlieren observations; results of zero-dimensional cylinder pressure indication; and apparent heat release measurements comparing two combustion chamber designs - one that actualizes a homogeneous mixture without specific charge motion directionality, and another with the here-introduced vortex-stratified approach.
机译:引入了用于氢气燃料往复式内燃机的涡流分层燃烧过程,以通过将对流传热损耗降低到燃烧期间的周围壁而增加热效率。该过程通过与由发动机气缸和活塞包围的主腔室连接的通道在单独的横向的圆柱形燃烧室中施加高度有序的旋转场。在压缩冲程期间直接注入气态氢,而由于芯片效果,空气沿着圆周切向并优先于燃烧室进入燃烧室。两条溪流彼此纳入并凭借腔室和通道几何形状发展成剧烈的漩涡。当混合前进时,燃料由有限时间扩散的组合径向限制在周边处的纯空气的补充,以及由作用在不同密度气体混合物上的旋转流动形成的向心磁场。燃烧发生,火焰传播最初遵循散装流的旋转,然后沿向内径向向内卷曲。这项工作调查了在烧制的光学可接近的2行中风燃料的直喷发动机中的过程测试,最高可达5000rpm。本文是两部分中的第一个解释了理论背景;呈现Schlieren观察;零旋气压力指示的结果;表观热释放测量比较了两个燃烧室设计 - 一种在没有特定电荷运动方向性的情况下实现均匀混合物的释放测量,并且通过这里引入的涡旋分层方法另外。

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