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首页> 外文期刊>International journal of hydrogen energy >Visualization of hydrogen jet evolution and combustion under simulated direct-injection compression-ignition engine conditions
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Visualization of hydrogen jet evolution and combustion under simulated direct-injection compression-ignition engine conditions

机译:模拟直喷压力点火发动机条件下的氢气进化和燃烧的可视化

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The evolution and combustion of H-2 jets were investigated in an optically-accessible constant-volume chamber under simulated direct-injection (DI) compression-ignition (CI) engine conditions. The parameters varied include injection pressure (84-140 bar) and ambient temperature (1000-1140 K). A detailed characterization of the injector system and the ensuing jet penetration process is reported first. High-speed schlieren imaging, OH* chemiluminescence imaging and pressure trace measurements were subsequently used to investigate the auto-ignition and combustion of the H-2 jets. The results show that the ignition delay of H-2 jets under such conditions is sensitive to ambient temperature variations, but not to injection pressure. Optical imaging reveals that the combustion of H-2 jets mostly initiated from a localized kernel, before spreading to engulf the whole jet volume downstream of ignition location. The imaging also indicates that after ignition, the flame recesses back towards the nozzle and appears to attach to the nozzle to form a diffusion flame structure. (C) 2020 Hydrogen Energy Publications LLC. Published by Elsevier Ltd. All rights reserved.
机译:在模拟直喷(DI)压缩 - 点火(CI)发动机条件下在光学可接近的恒定体积室中研究了H-2喷射的进化和燃烧。参数变化包括注射压力(84-140杆)和环境温度(1000-1140 k)。首先报告喷射器系统和随后的喷射穿透过程的详细表征。高速Schlieren成像,OH *化学发光成像和压力痕量测量随后用于研究H-2喷气机的自动点火和燃烧。结果表明,在这种条件下H-2喷射的点火延迟对环境温度变化敏感,但不是注射压力。光学成像揭示了H-2射流的燃烧主要从局部内核引发,然后在展开点火位置下游的整个喷射体积之前。成像还表明,在点火之后,火焰凹陷朝向喷嘴凹进并似乎连接到喷嘴以形成扩散火焰结构。 (c)2020氢能源出版物LLC。 elsevier有限公司出版。保留所有权利。

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