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车载加油油气回收系统中气液两相流动特性的实验和数值模拟
引用本文:刘美丽, 陈家庆, 汤水清, 朱玲, 姬宜朋. 车载加油油气回收系统中气液两相流动特性的实验和数值模拟[J]. 环境工程学报, 2018, 12(2): 388-395. doi: 10.12030/j.cjee.201707122
作者姓名:刘美丽  陈家庆  汤水清  朱玲  姬宜朋
作者单位:1.北京石油化工学院环境工程系, 北京 102617; 2.中国核电工程有限公司, 北京 100840
基金项目:北京市教委科技发展计划重点项目暨北京市自然科学基金重点项目(B类)(KZ201410017019)
摘    要:合理分析车载加油油气回收系统(ORVR)内气液两相的流动特性对油气排放控制技术的实施具有重要意义。以ORVR加油系统为对象,采用高速摄像、粒子动态分析仪(PDA)实验测量和CFD数值模拟相结合的方法,对ORVR车辆加油过程中的气液两相流动特性进行了系统研究,讨论了加油量对加油管内流场和压力场的影响。结果表明,随着加油速度的增大,加油管口的射流卷吸增强,气液两相流动过程中的湍流程度加剧,液流冲击与破碎严重,涡旋现象明显;随着加油速度的增大,气液掺混严重,液体自由表面边界逐渐模糊;加油过程中加油管和燃油箱内气相压力的变化分为2个阶段:开始加油时气相压力迅速增大,在5~8 s内达到峰值;然后气相压力逐渐减小,最终趋于稳定。

关 键 词:加油排放   车载加油油气回收   流动特性   数值模拟

Experiment and numerical simulation of gas-liquid two phase flow in on-board refueling vapor recovery system
LIU Meili, CHEN Jiaqing, TANG Shuiqing, ZHU Ling, JI Yipeng. Experiment and numerical simulation of gas-liquid two phase flow in on-board refueling vapor recovery system[J]. Chinese Journal of Environmental Engineering, 2018, 12(2): 388-395. doi: 10.12030/j.cjee.201707122
Authors:LIU Meili  CHEN Jiaqing  TANG Shuiqing  ZHU Ling  JI Yipeng
Affiliation:1.Department of Environmental Engineering, Beijing Institute of Petrochemical Technology, Beijing 102617, China; 2.China Nuclear Power Engineering Co.Ltd., Beijing 100840, China
Abstract:An analysis of the gas-liquid two-phase flow in on-board refueling vapor recovery (ORVR) system is of great importance to implement the evaporation emissions control technology.The flow characteristic of gas-liquid two phase of ORVR was investigated using the research methods, such as numerical simulation and experimental measurement with particle doppler dynamic analyzer (PDA) and high-speed camera. The results of influence of refueling velocity show that with the increasing of refueling velocity, the jet entrainment near the pipe inlet increases and the flow turbulence is intensified. At the same time, the increased refueling velocity makes serious fluid impingement and breakage, inducing the more obvious vortex phenomenon. In addition, as the refueling velocity increases, the gas-liquid mixing is increased and the free surface of liquid is gradually blurred. The change of vapor pressure comes in two stages in both refueling pipe and fuel tank. At beginning, the gas pressure increases rapidly and reaches peak within 5 to 8 seconds. Then the gas pressure decreases and becomes stable in the end.
Keywords:refueling emission  on-board refueling vapour recovery(ORVR)  flow characteristic  numerical simulation
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