蒸汽减温阀用离心喷嘴雾化特性研究

IF 3.9 3区 工程技术 Q2 ENGINEERING, CHEMICAL
Tao Yu , Jian Zhang , Bai-qi Liu , Shen-bin Luo , Ji-yun Du , Wei Yu , Xin-jun Yang , Dong-xiang Wang , Fang-yang Yuan
{"title":"蒸汽减温阀用离心喷嘴雾化特性研究","authors":"Tao Yu ,&nbsp;Jian Zhang ,&nbsp;Bai-qi Liu ,&nbsp;Shen-bin Luo ,&nbsp;Ji-yun Du ,&nbsp;Wei Yu ,&nbsp;Xin-jun Yang ,&nbsp;Dong-xiang Wang ,&nbsp;Fang-yang Yuan","doi":"10.1016/j.cherd.2025.08.011","DOIUrl":null,"url":null,"abstract":"<div><div>The atomization characteristics of the centrifugal nozzle were studied numerically and experimentally. A multi-scale coupling model was established based on ANSYS Fluent. The effects of structural parameters and operating conditions on spray cone angle and droplet size distribution were analyzed. The experimental photography of nozzle atomization with a high-speed camera verified the reliability of the numerical model. Results indicate that the spray cone angle is positively correlated with inlet pressure and swirl chamber angle, but negatively correlated with swirl hole angle, nozzle stem angle, and air velocity. The nozzle stem angle exhibits the most significant influence on the spray cone angle, while the swirl chamber angle has the least effect. Higher inlet pressure enhances liquid film instability and reduces droplet size. A swirl hole angle of 90° disrupts the swirling flow and causes a sharp increase in SMD. A smaller nozzle stem angle (30°) improves droplet size uniformity. High-speed airflow (&gt; 60 m/s) increases droplet coverage and suppresses accumulation at the axial rear. In the spray near-field, a smaller spray cone angle increases gas–liquid shear stress and reduces SMD. In the far-field, a smaller spray cone angle increases SMD due to higher droplet number density, which elevates the probability of droplet collision and coalescence.</div></div>","PeriodicalId":10019,"journal":{"name":"Chemical Engineering Research & Design","volume":"221 ","pages":"Pages 225-239"},"PeriodicalIF":3.9000,"publicationDate":"2025-08-07","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Atomization characteristics of centrifugal nozzle for steam desuperheating valve\",\"authors\":\"Tao Yu ,&nbsp;Jian Zhang ,&nbsp;Bai-qi Liu ,&nbsp;Shen-bin Luo ,&nbsp;Ji-yun Du ,&nbsp;Wei Yu ,&nbsp;Xin-jun Yang ,&nbsp;Dong-xiang Wang ,&nbsp;Fang-yang Yuan\",\"doi\":\"10.1016/j.cherd.2025.08.011\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><div>The atomization characteristics of the centrifugal nozzle were studied numerically and experimentally. A multi-scale coupling model was established based on ANSYS Fluent. The effects of structural parameters and operating conditions on spray cone angle and droplet size distribution were analyzed. The experimental photography of nozzle atomization with a high-speed camera verified the reliability of the numerical model. Results indicate that the spray cone angle is positively correlated with inlet pressure and swirl chamber angle, but negatively correlated with swirl hole angle, nozzle stem angle, and air velocity. The nozzle stem angle exhibits the most significant influence on the spray cone angle, while the swirl chamber angle has the least effect. Higher inlet pressure enhances liquid film instability and reduces droplet size. A swirl hole angle of 90° disrupts the swirling flow and causes a sharp increase in SMD. A smaller nozzle stem angle (30°) improves droplet size uniformity. High-speed airflow (&gt; 60 m/s) increases droplet coverage and suppresses accumulation at the axial rear. In the spray near-field, a smaller spray cone angle increases gas–liquid shear stress and reduces SMD. In the far-field, a smaller spray cone angle increases SMD due to higher droplet number density, which elevates the probability of droplet collision and coalescence.</div></div>\",\"PeriodicalId\":10019,\"journal\":{\"name\":\"Chemical Engineering Research & Design\",\"volume\":\"221 \",\"pages\":\"Pages 225-239\"},\"PeriodicalIF\":3.9000,\"publicationDate\":\"2025-08-07\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Chemical Engineering Research & Design\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://www.sciencedirect.com/science/article/pii/S0263876225004290\",\"RegionNum\":3,\"RegionCategory\":\"工程技术\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q2\",\"JCRName\":\"ENGINEERING, CHEMICAL\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Chemical Engineering Research & Design","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S0263876225004290","RegionNum":3,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q2","JCRName":"ENGINEERING, CHEMICAL","Score":null,"Total":0}
引用次数: 0

摘要

对离心喷嘴的雾化特性进行了数值和实验研究。基于ANSYS Fluent建立了多尺度耦合模型。分析了结构参数和操作条件对喷雾锥角和液滴粒径分布的影响。用高速相机对喷管雾化进行了实验摄影,验证了数值模型的可靠性。结果表明:喷嘴锥角与进口压力、旋流腔角呈正相关,与旋流孔角、喷嘴杆角、风速呈负相关;喷嘴杆角对喷嘴锥角的影响最大,旋流腔角对喷嘴锥角的影响最小。较高的进口压力增强了液膜的不稳定性,减小了液滴的尺寸。90°的旋流孔角破坏了旋流,导致SMD急剧增加。较小的喷嘴杆角(30°)可改善液滴尺寸均匀性。高速气流(>;60 m/s)增加液滴覆盖范围,抑制轴向尾部积聚。在喷雾近场中,较小的喷雾锥角增大气液剪切应力,减小SMD。在远场,较小的喷射锥角增加了液滴数密度,从而提高了液滴碰撞和聚并的概率。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Atomization characteristics of centrifugal nozzle for steam desuperheating valve
The atomization characteristics of the centrifugal nozzle were studied numerically and experimentally. A multi-scale coupling model was established based on ANSYS Fluent. The effects of structural parameters and operating conditions on spray cone angle and droplet size distribution were analyzed. The experimental photography of nozzle atomization with a high-speed camera verified the reliability of the numerical model. Results indicate that the spray cone angle is positively correlated with inlet pressure and swirl chamber angle, but negatively correlated with swirl hole angle, nozzle stem angle, and air velocity. The nozzle stem angle exhibits the most significant influence on the spray cone angle, while the swirl chamber angle has the least effect. Higher inlet pressure enhances liquid film instability and reduces droplet size. A swirl hole angle of 90° disrupts the swirling flow and causes a sharp increase in SMD. A smaller nozzle stem angle (30°) improves droplet size uniformity. High-speed airflow (> 60 m/s) increases droplet coverage and suppresses accumulation at the axial rear. In the spray near-field, a smaller spray cone angle increases gas–liquid shear stress and reduces SMD. In the far-field, a smaller spray cone angle increases SMD due to higher droplet number density, which elevates the probability of droplet collision and coalescence.
求助全文
通过发布文献求助,成功后即可免费获取论文全文。 去求助
来源期刊
Chemical Engineering Research & Design
Chemical Engineering Research & Design 工程技术-工程:化工
CiteScore
6.10
自引率
7.70%
发文量
623
审稿时长
42 days
期刊介绍: ChERD aims to be the principal international journal for publication of high quality, original papers in chemical engineering. Papers showing how research results can be used in chemical engineering design, and accounts of experimental or theoretical research work bringing new perspectives to established principles, highlighting unsolved problems or indicating directions for future research, are particularly welcome. Contributions that deal with new developments in plant or processes and that can be given quantitative expression are encouraged. The journal is especially interested in papers that extend the boundaries of traditional chemical engineering.
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
联系我们:info@booksci.cn Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。 Copyright © 2023 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:604180095
Book学术官方微信