主管部门: 中国航天科技集团有限公司
主办单位: 中国航天空气动力技术研究院
中国宇航学会
中国宇航出版有限责任公司

基于数字全息技术的旋流杯空气雾化燃油喷嘴低温雾化特性

Measurement of Air-Blast Swirl Cup Atomization Field at Low Temperature With Digital Holographic Technique

  • 摘要: 为了研究旋流杯空气雾化喷嘴在低油压、 低油温工况下的近场雾化特性, 采用离轴脉冲激光数字全息测试系统对不同油温及气压组合条件下的喷嘴出口下游雾化形态及液滴颗粒信息进行了测试研究。结果表明, 在0.03 MPa的低油压工况下, 气压和温度变化均对喷嘴出口下游的雾化场有很大影响。当气压较低时, 油雾颗粒较大, 且分布较为稀疏, 雾化锥角轮廓不明显, 雾锥中心区的粒径往往大于边缘处的粒径, 随着气压升高, 油雾颗粒粒径明显降低, 空间分布渐趋均匀, 雾锥轮廓明显; 对于各个工况, 大多数颗粒粒径分布在200 μm或以内, 当气压为0.5 kPa时, 粒径分布峰较宽, 200 μm以上的颗粒数目较多, 随着气压升高, 粒径分布峰越来越窄, 燃油颗粒粒径越来越小; 对于油温-20 ℃, -40 ℃, 油压0.03 MPa, 气压0.5, 1.0 kPa的工况, 雾锥边缘局部出现突增的Sauter平均直径(Sauter mean diameter, SMD)统计结果, 最大达到1 944 μm以上, 表明旋流杯在低油温、 低油压、 低气压工况下雾化性能表现较差; 随着气压升高, x, y方向速率Vx, Vy分布区间范围越广, 粒径在32~66 μm范围细小雾滴的速度分布区间明显更广, 粒径大于500 μm的雾滴统计数目较少, 速度分布也比较集中。试验结果证实了全息技术对低温三维雾化场测量的可行性, 获得的雾化参数可为喷嘴优化设计提供依据。

     

    Abstract: A digital off-axis holography system was applied to measure the atomization characteristics near the exit of a nozzle with an air-blast swirl cup under different combinations of oil temperature and air pressure. It is found that both changes of oil temperature and air pressure have strong effect on the near-nozzle droplet field at oil pressure of 0.03 MPa. The larger droplets with sparse distribution and unconspicuous spray cone have been found at lower air pressure, and the droplet diameter in the spray cone center is larger than that at the edge. As air pressure increases, the droplet diameter decreases significantly, the distribution becomes uniform, and the spray cone is obvious. For all conditions, the droplet diameter is mainly distributed within 200 μm. However, at an air pressure of 0.5 kPa, a large number of droplets are above 200 μm, with a broad particle size distribution. As air pressure increases the diameter distribution range tends to narrow and the droplet diameter becomes smaller. A sharp increase of Sauter mean diameter (SMD), even up to 1 944 μm, appears at the edge of spray cone under conditions of oil temperature of -20 ℃, -40 ℃, oil pressure of 0.03 MPa and air pressure of 1.0 kPa. This result indicates that the atomization quality of air-blast swirl nozzle is poor under low pressure and low temperature conditions. This study also reveals that the values of velocity component in the x and y directions have a wider range of distribution with the increase of air pressure, especially for particle diameters from 32 to 66 μm. However, particles whose diameters are above 500 μm are counted less and have a narrow range of velocity distribution. The experimental results indicate that the digital off-axis holography is a powerful tool for three-dimensional visualization of near-nozzle atomization at low oil temperatures. This work can provide reference data for optimization of the nozzle structure design.

     

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