多股射流撞击雾化机理的实验研究 | |
英文题名 | Experimental Study on Characteristics of multi-jet impingement Atomization |
侯林![]() | |
导师 | 范学军 |
2024-05-18 | |
学位授予单位 | 中国科学院大学 |
学位授予地点 | 北京 |
学位类别 | 博士 |
学位专业 | 流体力学 |
关键词 | 多股射流 雾化机理 偏心撞击 SMD 液滴分布均匀性 |
摘要 | 众所周知,燃烧室整体性能与喷嘴的雾化性能是密不可分的,雾化性能良好
的喷嘴可以使液体燃料或氧化剂形成大量细小而均匀的小液滴,从而增加液滴与
周围环境空气的接触面积,促进换热与蒸发过程,有利于促进混合气的形成,提
高燃烧的稳定性。本课题以水介质的射流撞击雾化形成的喷雾为主要研究对象,
创新设计了多股环状排列射流的正心与偏心撞击雾化喷嘴,定义了表征射流偏心
撞击程度的偏心碰撞参数 B,围绕多股射流撞击雾化液膜结构与破碎机理、射流
撞击形成的液膜形态与尺寸特性,多参数下的喷雾液滴统计学规律展开实验研究。
本课题利用高速背光成像技术对射流撞击雾化喷雾进行可视化测量,结果表
明,与双股射流撞击后形成的叶片状液膜的平面雾化结构不同,三股环状排列的
射流撞击于一点,随后在下游形成由三个半叶状液膜组成的空间结构,在液膜表
面波与周围空气共同作用下,液膜发生破碎形成液丝和大液滴,随后继续破碎成
大量小液滴。随着撞击韦伯数的增大,结构下游尖端边缘从闭合状态转变为开放
状态,分析了液膜上的表面波,测量了表面波波长,并与理论值做了对比,得出
液膜上的表面波为气动波与撞击波的非线性叠加,韦伯数较小时波长较长,而韦
伯数较大时,波长较短,这与粘性耗散与拉伸应力有关。通过对可视化测量获取
的喷雾图像进行处理,计算获取了雾化液膜长度,雾化液膜宽度,雾化液膜厚度
等参数用于表征雾化液膜的尺寸特性,并与理论值做对比,得出液膜的厚度与撞
击韦伯数有关,撞击韦伯数越大,液膜厚度越小,液膜的长度和宽度均与韦伯数
有关,液膜为边缘闭合状态时,液膜长度和最大宽度随韦伯数增大而增大,液膜
为边缘开放状态时,液膜长度随韦伯数增大而减小,液膜最大宽度随韦伯数增大
而增大,这与理论预测相符合。
采用相位多普勒粒子测量技术对雾化液滴粒子数、粒径和速度进行同步测量,
分析获取了雾化场液滴的尺寸分布、空间分布以及速度分布。结果表明,雾化场
内液滴直径的概率密度分布曲线呈近似对称,且在 150μm 至 250μm 范围内出
现峰值,在该分布内,液滴尺寸主要分布在 100μm 至 300μm 范围内,表明该喷
雾雾化效果较好。对雾化场内粒子的归一化尺寸的概率密度分布也进行了分析,
发现其与 Gamma 分布函数有较好的拟合效果。采用径向不均匀指数 RNI 对雾化
场内液滴的空间分布进行表征,结果表明 RNI 随着径向距离的增大而减小,也
就是说,越靠近喷雾边缘,雾化液滴分布越均匀。
射流的偏心撞击对雾化结构的影响体现在两个方面,一是可以使雾化液膜发
生偏转,二是加速液膜下游尖端从闭合状态转为开放状态。对雾化液滴特性的影
响体现在增大撞击偏离程度,会使雾化液滴的平均尺寸减小但是会使得雾化场的
I多股射流撞击雾化机理的实验研究
空间分布均匀性降低。对于雾化场内的液滴尺寸分布,分析表明液滴粒径的概率
密度函数 PDF 的曲线峰值与偏心碰撞参数 B 有关,随着 We 和 B 的增加,测量
平面上液滴直径减小,这将有利于雾化。
最后对射流数量对雾化的影响进行了分析,结果表明,在相同的撞击韦伯数
下,增加射流数量,雾化质量会变差,以五股射流撞击为例,射流撞击后形成窄
小的液膜,液滴沿喷嘴轴向分布,径向的液滴数量减少。虽然增大撞击韦伯数(𝑊)
后,液膜的破碎长度变长,液膜厚度变小。液丝、液滴的数量增多,雾化场内液
滴的索特尔平均直径(SMD)变小,但是对比相同撞击韦伯数下三股和两股射
流撞击雾化喷雾,雾化场内雾化效果仍不理想。使射流偏心撞击后,随着偏心碰
撞参数 B 的增大,雾化锥角增大,雾化液膜的轴向延伸距离增大,液膜下游从闭
合状态转为开放状态。相邻两液膜的相对位置发生改变。在一定范围内,B 的增
大有利于液膜的形成与破碎,超过某一临界值后,随着 B 的增大,雾化场液滴数
目减少,液丝变粗变短。雾化场内液滴的 SMD 变大,不利于液膜破碎成液丝和
液滴。
总的来说,本文以水介质的射流撞击雾化形成的喷雾为主要研究对象,设计
并建造了一套基于 PDPA 和高速相机的可视化测量实验设备,并研发了多股环
状排列射流的正心与偏心撞击雾化喷嘴结构;创新性地定义了适用于多股射流偏
心撞击雾化的偏心参数,量化了多股射流偏心撞击的程度;揭示了多股环状排列
的射流正心和偏心对撞雾化过程和机理,填补了该类型撞击雾化机理实验测试的
部分空白。 |
英文摘要 | As we all know, the overall performance of the combustion chamber is inseparable from the atomization performance of the nozzle, the nozzle with good atomization performance can make the liquid fuel or oxidizer form a large number of small and uniform droplets, thereby increasing the contact area between the droplets and the surrounding ambient air, promoting the heat transfer and evaporation process, which is conducive to promoting the formation of the mixture and improving the stability of combustion. This project took the spray formed by jet impact and atomization of water medium as the main research object, innovatively designed the positive and misaligned impact atomization nozzles of multiple circularly arranged impingment jets, defined the off-center impact factor B that characterized the misaligned impact degree of jets, and focused on the basic morphological characteristics and external macroscopic characteristics of the spray, as well as the morphology and size characteristics of the liquid sheet formed by jet impact. The statistical rule of spray droplets and droplet movement characteristics under multi-parameter were investigated experimentally. In this study, high-speed backlight imaging technology was used to visually measure jet impact atomization spray. The results showed that different from the flat atomization structure of the bladed liquid sheet formed after the impact of two jets, the three ring-arranged jets impact at one point and then form a spatial structure composed of three half bladed liquid sheets downstream. Under the joint action of the surface waves of the liquid sheet and the surrounding air, The liquid sheet breaks to form liquid ligaments and large droplets, which then continue to break into a large number of small droplets. With the increase of the Weber number, the downstream tip of the structure changes from a closed rim to an open rim. Surface waves on the liquid film were analyzed, and the wavelength of surface waves was measured. By comparing with theoretical values, it was concluded that the surface waves on the liquid sheet were the nonlinear superposition of aerodynamic waves and impact waves. When the We was small, the wavelength was longer, while when the We was large, the wavelength was shorter, which was related to viscous dissipation and tensile stress. By processing the spray images obtained through visual measurement, parameters such as the length, width, and thickness of the atomized liquid sheet were calculated to characterize the size characteristics of the atomized liquid sheet. By comparing with theoretical values, it was found that the thickness of the liquid sheet was related to the impact We. The greater the impact We, the smaller the thickness of the liquid sheet. Both the length and width of the liquid sheet were related to the Wes. When the liquid sheet was in a closed-rim state, both the length and the maximum width of the liquid sheet increased as the We increased. When the liquid sheet was in an open-rim state, the length of the liquid sheet decreased as the We increased, while the maximum width of the liquid sheet increased as the We increased. This was consistent with theoretical predictions. The particle number, particle size and velocity of atomized droplets were measured synchronously by using phase Doppler particle analysis and measurement technology, and the size distribution, spatial distribution and velocity distribution of droplets in atomization spray field were obtained. The results show that the structure of the Probability Density Function (PDF) curve of the droplet diameter in the atomization field is approximately symmetric, and the peak value appears in the range of 150 The influence of the misaligned impingement of the jet on the atomization structure is reflected in two aspects: one is to deflect the atomization liquid sheet, the other is to accelerate the downstream tip of the liquid sheet from the closed rim to the open rim. The influence on the spray droplet characteristics is reflected in the increase of off-center impact factor, B, which will reduce the average size of atomization droplet but reduce the spatial distribution uniformity of atomization spray field. For the droplet size distribution, the analysis results shows that twith the increase of Wes and B, the droplet diameter decreases, which will be conducive to atomization. Finally, the influence of the number of jets on atomization was analyzed. The results showed that under the same impact Weber number (We) , the atomization quality will deteriorate with the increase of the number of jets. Taking the impact of five jets as an example, a narrow liquid sheet is formed after jet impact, and droplets are distributed axially along the nozzle, while the number of radial droplets decreases. With the increase of impact Weber number ( In general, this paper designed and constructed a set of visual measuring experiment equipment based on PDPA and high-speed camera, and developed the structure of the nozzle of multiple circular arranged jets, quantified the extent of the atomization mechanism of multiple jet. |
语种 | 中文 |
文献类型 | 学位论文 |
条目标识符 | http://dspace.imech.ac.cn/handle/311007/95228 |
专题 | 高温气体动力学国家重点实验室 |
通讯作者 | 侯林 |
推荐引用方式 GB/T 7714 | 侯林. 多股射流撞击雾化机理的实验研究[D]. 北京. 中国科学院大学,2024. |
条目包含的文件 | ||||||
文件名称/大小 | 文献类型 | 版本类型 | 开放类型 | 使用许可 | ||
Experimental Study o(9995KB) | 学位论文 | 开放获取 | CC BY-NC-SA | 请求全文 |
个性服务 |
推荐该条目 |
保存到收藏夹 |
查看访问统计 |
导出为Endnote文件 |
Lanfanshu学术 |
Lanfanshu学术中相似的文章 |
[侯林]的文章 |
百度学术 |
百度学术中相似的文章 |
[侯林]的文章 |
必应学术 |
必应学术中相似的文章 |
[侯林]的文章 |
相关权益政策 |
暂无数据 |
收藏/分享 |
除非特别说明,本系统中所有内容都受版权保护,并保留所有权利。
修改评论