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基于拉瓦尔效应的超音速喷嘴雾化性能分析与试验

杨超 陈波 姜万录 高殿荣 金光俊

农业工程学报2016,Vol.32Issue(19):57-64,8.
农业工程学报2016,Vol.32Issue(19):57-64,8.DOI:10.11975/j.issn.1002-6819.2016.19.008

基于拉瓦尔效应的超音速喷嘴雾化性能分析与试验

Analysis and experiment on atomizing characteristics of supersonic nozzle based on Laval effect

杨超 1陈波 2姜万录 3高殿荣 1金光俊2

作者信息

  • 1. 燕山大学河北省重型机械流体动力传输与控制重点实验室,秦皇岛 066004
  • 2. 燕山大学先进锻压成形技术与科学教育部重点实验室,秦皇岛 066004
  • 3. 秦皇岛首创思泰意达环保科技有限公司,秦皇岛 066004
  • 折叠

摘要

Abstract

Atomizing nozzle is a crucial part of spray device. And it is widely applied in many fields such as agricultural spraying, plant cooling and dust suppression. Moreover, the atomizing performance of nozzle has a great influence on the size and velocity of droplet, and the flow distribution. In order to improve the atomizing performance of the supersonic atomizing nozzle, atomizing principle of the supersonic atomizing nozzle is analyzed in this paper, and it is found that the velocity difference of air phase and water phase has a great effect on the atomizing performance. The spool structure of the atomizing nozzle is changed according to the supersonic principle of Laval nozzle when it is tapered before. The key size of Laval-style structure is important to its accelerated performance, the air inlet diameter is 4.5 mm, the throat diameter is 1.5 mm, the spool outlet diameter is 3.5 mm, the water inlet diameter is 0.9 mm, the subsonic contraction period length is 3.3 mm, the supersonic expansion period length is 6.2 mm, and the expansion period cone angle is 10°. A three-dimensional (3D) geometry model of Laval-style spool is built, supersonic can be achieved while the air pass through the nozzle, and velocity distributions law of the nozzle flow field is obtained by using computational fluid dynamics software Fluent. Furthermore, a test bench is built for atomization and the atomizing testing is carried out. The atomizing effect of nozzle is analyzed and compared before and after the spool structure being changed, and the atomizing performance influence rule of Laval-style atomizing nozzle is studied under different operational parameters. The numerical simulation results show that the velocity within most parts of the nozzle can reach supersonic and the velocity difference of air phase and water phase is significantly increased. In addition, the results of atomization testing indicate that the change of spool structure and the operational parameters have a great influence on atomizing performance, and the Laval-style atomizing nozzle is better than the tapered atomizing nozzle. Compared to the tapered atomizing nozzle, the droplet sprayed from Laval-style atomizing nozzle is smaller, the spray angle is larger, the droplet is more uniformly distributed in the flow field, and the droplet suspending time in the air is longer. In the test, the operational parameters of Laval-style atomizing nozzle include air pressure, water pressure and air-water pressure ratio. The air pressure is within the range of 0.3-0.6 MPa, the water pressure is within the range of 0.1-0.4 MPa, and the air-water pressure ratio is within the range of 0-6. The testing results reveal that it is beneficial to decrease the droplet size by increasing the air pressure or the air-water pressure ratio, but the effect will be the opposite by increasing the water pressure. The droplet size will increase when the values of air pressure and water pressure are almost the same or the droplet flow filed is split. However, the droplet size will decrease when the shrill crash appears during the spray process. Overall, with the air-water pressure ratio increasing in the range of 0-6, the droplet size shows an obvious trend toward decreasing. When the air-water pressure ratio is within the range of 0-3, the droplet size decreases rapidly by an amplitude that is as high as 90.56%, but when the air-water pressure ratio is within the range of 3-6, the droplet size displays a slow decrease. The Sauter mean diameter of droplet can be as small as 18.52μm when the air-water pressure ratio is 6. The research results of the paper will provide a reference for the further research on the supersonic atomizing nozzle and the design of new atomizing device.

关键词

超音速/喷嘴/计算流体动力学/拉瓦尔效应/雾化/雾滴粒径

Key words

supersonic flow/nozzle/computational fluid dynamics/Laval effect/atomization device/droplet size

分类

农业科技

引用本文复制引用

杨超,陈波,姜万录,高殿荣,金光俊..基于拉瓦尔效应的超音速喷嘴雾化性能分析与试验[J].农业工程学报,2016,32(19):57-64,8.

基金项目

国家自然科学基金资助项目(51375421);国家自然科学基金资助项目(51475405);河北省研究生创新资助项目 ()

农业工程学报

OA北大核心CSCDCSTPCD

1002-6819

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