任虎虎,徐强仁,王立志,李广超,赵巍,赵庆军.跨音速风扇叶片高低转速下混合相积冰的对比研究[J].装备环境工程,2023,20(7):72-82. REN Hu-hu,XU Qiang-ren,WANG Li-zhi,LI Guang-chao,ZHAO Wei,ZHAO Qing-jun.Comparative Research of Mixed-phase Icing at High and Low Velocities of Transonic Fan Blades[J].Equipment Environmental Engineering,2023,20(7):72-82.
跨音速风扇叶片高低转速下混合相积冰的对比研究
Comparative Research of Mixed-phase Icing at High and Low Velocities of Transonic Fan Blades
投稿时间:2023-03-21  修订日期:2023-05-09
DOI:10.7643/issn.1672-9242.2023.07.010
中文关键词:  混合相  积冰  撞击角度  冰晶温度  高转速  低转速  风扇叶片中图分类号:V231.1 文献标识码:A 文章编号:1672-9242(2023)07-0072-11
英文关键词:mixed-phase  icing  impact angle  ice crystal temperature  high speed  low speed  fan blades
基金项目:国家科技重大专项(J2019-Ⅲ-0010-0054,J2019-Ⅱ-0014-0035)
作者单位
任虎虎 沈阳航空航天大学 航空发动机学院,沈阳 110136;中国科学院工程热物理研究所,北京 100190 
徐强仁 中国科学院工程热物理研究所,北京 100190;中国科学院轻型动力重点实验室,北京 100190 
王立志 中国科学院工程热物理研究所,北京 100190;中国科学院轻型动力重点实验室,北京 100190 
李广超 沈阳航空航天大学 航空发动机学院,沈阳 110136 
赵巍 中国科学院工程热物理研究所,北京 100190;中国科学院轻型动力重点实验室,北京 100190;中国科学院大学 航空宇航学院,北京 100049 
赵庆军 中国科学院工程热物理研究所,北京 100190;中国科学院轻型动力重点实验室,北京 100190;中国科学院大学 航空宇航学院,北京 100049;中国科学院工程热物理研究所 分布式冷热电联供系统北京市重点实验室,北京 100190 
AuthorInstitution
REN Hu-hu School of Aero-engine, Shenyang Aerospace University, Shenyang 110136, China;Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190, China 
XU Qiang-ren Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190, China;Key Laboratory of Light-duty Gas-turbine, Chinese Academy of Sciences, Beijing 100190, China 
WANG Li-zhi Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190, China;Key Laboratory of Light-duty Gas-turbine, Chinese Academy of Sciences, Beijing 100190, China 
LI Guang-chao School of Aero-engine, Shenyang Aerospace University, Shenyang 110136, China 
ZHAO Wei Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190, China;Key Laboratory of Light-duty Gas-turbine, Chinese Academy of Sciences, Beijing 100190, China;School of Aeronautics and Astronautics, University of Chinese Academy of Sciences, Beijing 100049, China 
ZHAO Qing-jun Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190, China;Key Laboratory of Light-duty Gas-turbine, Chinese Academy of Sciences, Beijing 100190, China;School of Aeronautics and Astronautics, University of Chinese Academy of Sciences, Beijing 100049, China;Beijing Key Laboratory of Distributed Combined Cooling Heating and Power System, Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190, China 
摘要点击次数:
全文下载次数:
中文摘要:
      目的 获得跨音速风扇转子叶片高、低转速下混合相积冰的影响规律。方法 使用CFX获取风扇叶片空气流场数据,采用FENSAP-ICE获取积冰冰形,通过过冷水滴与冰晶温度、撞击叶片角度等进行混合相积冰高、低转速冰形分析。结果 风扇叶片高、低转速运转时,过冷水滴与冰晶的运动状态变化相对明显。高转速时,流场内的气流为跨音速流动,过冷水滴与冰晶撞击角度相差较大,撞击角度较大的叶根区域更容易收集过冷水滴与冰晶;低转速时,过冷水滴和冰晶与叶片的撞击角度大部分区域低于10°,使过冷水滴与冰晶碰撞到叶片后的捕获难度提升。风扇叶片高、低转速运转时,叶身的温度差异使过冷水滴在低转速下易直接凝结,未凝结的水膜量极少,而冰晶表面未形成水膜,不易被捕获,使得最终的积冰主要为过冷水滴积冰。结论 风扇叶片混合相积冰在高转速时,流道内温度升高更快,水膜不易凝结,冰晶表面易融化,促进了冰晶积冰。
英文摘要:
      The work aims to obtain the influence of icing on the mixed phase of transonic fan blades at high and low velocities. CFX was used to obtain the airflow field data of fan blades, and FENSAP-ICE was used to obtain ice shapes. The ice shape at high and low velocities of mixed phase icing was analyzed through the temperature of supercooled droplets and ice crystals and the angle of impact on blades. The results showed that when the fan blade worked at high and low velocities, the motion states of supercooled droplets and ice crystals varied significantly. At high velocities, the airflow in the flow field was transonic flow, and the impact angle between supercooled droplets and ice crystals was different. The root area with large impact angle was easier to collect supercooled water droplets and ice crystals; at low velocities, the impact angle of supercooled droplets, ice crystals and blades was less than 10° in most areas, which made it more difficult to capture supercooled droplets and ice crystals after they collided with the blades. The temperature difference of the blade when the fan blade ran at high and low velocities made the supercooled droplets easy to condense directly at low velocities, and the amount of uncondensed water films was very small. However, the ice crystal surface was not easy to be captured because the water film was not formed, so the final ice accretion was mainly the ice accretion formed by the supercooled droplets. When the fan blade mixes phase icing at high velocities, the temperature in the flow passage rises faster, the water film is not easy to condenses, and the ice crystal surface is easy to be molten, which promotes the ice accretion of ice crystals.
查看全文  查看/发表评论  下载PDF阅读器
关闭

关于我们 | 联系我们 | 投诉建议 | 隐私保护 | 用户协议

您是第12777112位访问者    渝ICP备15012534号-5

版权所有:《装备环境工程》编辑部 2014 All Rights Reserved

邮编:400039     电话:023-68792835    Email: zbhjgc@163.com

视频号 公众号