离子液体氢气压缩机运行参数对振荡流动特性影响机理
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    摘要:

    离子液体氢气压缩机具有冷却效果好、能耗低、易损件少、可靠性高等优点,是未来高压加氢站氢气增压的优选机型。为了厘清离子液体氢气压缩机运行参数对工作腔内部气液两相振荡流动特性的影响机理,本文基于CFD动网格技术和VOF多相流模型,建立了压缩机流-固耦合的离子液体-氢气两相瞬态动力特性分析模型,探究了气液两相在不同活塞运动速度冲击下的振荡流动和形态演变规律。结果表明离子液体在气缸中的运动状态与活塞运动和气阀扰流冲击密切相关。随着液压泵转速的提高,活塞速度和气流速度也随之增加,气液两相振荡运动加剧,湍流作用提高,气液相界面的破碎程度增大,离子液体溢出量也随之快速增加,从120 RPM到600 RPM时,离子液体溢出量增加了4.7倍。在离子液体氢气压缩机设计和应用过程中,可采取较低转速来减弱离子液体-氢气两相振荡运动剧烈程度,同时可减少离子液体溢出量。

    Abstract:

    Ionic liquid hydrogen compressors have the advantages of good cooling effect, low energy consumption, fewer vulnerable parts, and high reliability, making them the preferred model for hydrogen pressurization in future high-pressure hydrogen refueling stations. In order to clarify the influence mechanism of operating parameters of ionic liquid hydrogen compressor on the oscillation flow characteristics of gas-liquid two-phase inside the working chamber, this paper establishes a transient thermal dynamic characteristics analysis model of ionic liquid hydrogen two-phase in compressor fluid solid coupling based on CFD dynamic grid technology and VOF multiphase flow model, and explores the oscillation flow and morphology evolution of gas-liquid two-phase under different piston motion velocities and impacts. The results shows that the motion state of ionic liquids in cylinders is closely related to piston motion and valve turbulence impact. As the speed of the hydraulic pump increases, the piston speed and airflow speed also increase. The oscillation motion of the gas-liquid phase intensifies, the turbulence effect increases, the degree of fragmentation of the gas-liquid interface increases, and the amount of ionic liquid overflow also increases rapidly. From 120 RPM to 600 RPM, the amount of ionic liquid overflow increases by 4.7 times. In the process of ionic liquid hydrogen compressor design and application, lower speed can be taken to weaken the ionic liquid-hydrogen two-phase oscillation movement intensity, while reducing the amount of ionic liquid overflow.

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  • 收稿日期:2024-08-30
  • 最后修改日期:2024-11-20
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