介质阻挡放电等离子体防除冰实验研究(空军工程大学等离子体动力学重点实验室，陕西 西安 710038)

Miao TIAN; Huimin SONG; Hua LIANG; Biao WEI; Like XIE; Jie CHEN; Zhi SU

doi:10.11949/0438-1157.20190304

您当前的位置：

首页 >

文章列表页 >

介质阻挡放电等离子体防除冰实验研究(空军工程大学等离子体动力学重点实验室，陕西西安 710038)

流体力学与传递现象 | 更新时间：2020-06-24

- 介质阻挡放电等离子体防除冰实验研究(空军工程大学等离子体动力学重点实验室，陕西西安 710038)
- Experimental study on DBD discharge plasma for anti-icing and de-icing
- 化工学报 2019年70卷第11期页码：4247-4256
- 作者机构：
  
  Key Laboratory of Science and Technology on Plasma Dynamics, Air Force Engineering University, Xi’an 710038, Shaanxi, China
- 作者简介：
- 基金信息：
  
  国家自然科学基金项目(11472306;51407197;51507187)
- DOI：10.11949/0438-1157.20190304
  中图分类号： V 244.15
- 收稿：2019-04-01，
  
  修回：2019-08-09，
  
  纸质出版：2019-11-05
- 稿件说明：
移动端阅览
田苗, 宋慧敏, 梁华, 魏彪, 谢理科, 陈杰, 苏志. 介质阻挡放电等离子体防除冰实验研究[J]. 化工学报, 2019, 70(11): 4247-4256

TIAN Miao, SONG Huimin, LIANG Hua, WEI Biao, XIE Like, CHEN Jie, SU Zhi. Experimental study on DBD discharge plasma for anti-icing and de-icing[J]. CIESC Journal, 2019, 70(11): 4247-4256
田苗, 宋慧敏, 梁华, 魏彪, 谢理科, 陈杰, 苏志. 介质阻挡放电等离子体防除冰实验研究[J]. 化工学报, 2019, 70(11): 4247-4256 DOI： 10.11949/0438-1157.20190304.

TIAN Miao, SONG Huimin, LIANG Hua, WEI Biao, XIE Like, CHEN Jie, SU Zhi. Experimental study on DBD discharge plasma for anti-icing and de-icing[J]. CIESC Journal, 2019, 70(11): 4247-4256 DOI： 10.11949/0438-1157.20190304.

摘要

在无风环境下分别进行了交流介质阻挡放电（AC-DBD）、纳秒脉冲介质阻挡放电（NS-DBD）及射频介质阻挡放电（RF-DBD）等离子体除冰实验研究，采用高速成像技术与红外测温成像技术分别记录除冰过程中介质层表面相变及温度动态变化过程，对比分析了三者的优缺点及传热机理。结果表明，在功率相同的条件下，AC-DBD等离子体激励的温升迅速，加热范围广，除冰实验效果最佳；对于NS-DBD等离子体激励，低压高频的除冰性能明显优于高压低频；RF-DBD等离子体激励放电主要集中在电极条边缘，放电剧烈，但电极间的区域温度较低，导致整体除冰效果不佳。最后，选择除冰效果最好的AC-DBD等离子体激励，在结冰风洞中进行了防冰实验研究。结果表明，AC-DBD等离子体激励整体防冰效果较好，但在防冰过程中，前缘会出现局部结冰，需进一步优化激励器构型及能量，提高AC-DBD等离子体激励防冰效果。

Abstract

In this paper

AC dielectric barrier discharge (AC-DBD)

nanosecond pulse dielectric barrier discharge (NS-DBD) and radio frequency dielectric barrier discharge (RF-DBD) plasma de-icing experiments were carried out in a windless environment. Using high-speed imaging technology and infrared temperature imaging technology to record the dynamic process of the phase transition of the dielectric layer

systematically analyze the advantages and disadvantages of the three and the heat transfer mechanism. The results show that when the power output of the static experiment is the same

the temperature rise of the AC-DBD plasma is rapid

and the de-icing experiment is the best. For the NS-DBD plasma

the low-pressure high-frequency de-icing performance is obviously better than the high-voltage low-frequency; For RF-DBD

the discharge of the plasma is mainly concentrated at the edge of the electrode strip

and the discharge is severe

but the temperature between the electrodes is low

resulting in poor overall deicing effect. Finally

experimental verification of AC-DBD plasma anti-icing was carried out in the icing wind tunnel. In the wind tunnel test

the AC-DBD plasma has a good anti-icing effect in the downstream of the airfoil

but the anti-icing effect is not good at the leading edge position. In the next step

it is necessary to optimize the leading edge actuator configuration and improve the airfoil leading edge anti-icing effect.

关键词

Keywords

references

Lynch F , Khodadoust A . Erratum to “Effects of ice accretions on aircraft aerodynamics” [J]. Progress in Aerospace Sciences , 2002 , 38 ( 3 ): 273 - 274 .

Bragg M B , Broeren A P , Blumenthal L A . Iced-airfoil aerodynamics [J]. Progress in Aerospace Sciences , 2005 , 41 ( 5 ): 323 - 362 .

AOPA Air Satety Foundation Online Computer Library Center , Inc . Aircraft icing [EB/OL]. [2009-09-04] . http: // www. asf. org www. asf. org .

Thomas S K , Cassoni R P , Macarthur C D . Aircraft anti-icing and de-icing techniques and modeling [J]. Journal of Aircraft , 2012 , 33 ( 5 ): 841 - 854 .

Papadakis M , Wong S H , Yeong H W , et al . Icing tunnel experiments with a hot air anti-icing system [C]// 46th AIAA Aerospace Sciences Meeting and Exhibit . Reno, Nevada, USA : AIAA , 2008 : 444 - 448 .

彭宇泰 , 陆文华 , 李宝磊 . 石墨烯在飞机电热防除冰技术的应用 [J]. 化工设计通讯 , 2018 , ( 4 ): 66 - 67

Peng Y T , Lu W H , Li B L . Graphene application in the electro-thermal anti-icing or deicing technology of aircrafts [J]. Chemical Design Communication , 2018 , ( 4 ): 66 - 67

马辉 , 张大林 , 孟繁鑫 , 等 . 复合材料部件电加热防冰性能试验 [J]. 航空学报 , 2013 , 34 ( 8 ): 1846 - 1853 .

Ma H , Zhang D L , Meng F X , et al . Electric heating and anti-icing performance test of composite parts [J]. Journal of Aviation , 2013 , 34 ( 8 ): 1846 - 1853 .

郭涛 . 机翼电脉冲除冰系统电磁力及其除冰过程仿真研究 [D]. 南京 : 南京航空航天大学 , 2017 .

Guo T . Simulation study on electromagnetic force and deicing process of airfoil electric pulse deicing system [D]. Nanjing : Nanjing Aerospace University , 2017 .

袁赫 . 飞机电排斥除冰系统研究 [D]. 武汉 : 华中科技大学 , 2010 .

Yuan H . Research on aircraft electric rejection deicing system [D]. Wuhan : Huazhong University of Science and Technology , 2010 .

苗波 . 翼型压电振动除冰理论和实验研究 [D]. 南京 : 南京航空航天大学 , 2016 .

Miao B . Theoretical and experimental study on airfoil piezoelectric vibration deicing [D]. Nanjing : Nanjing Aerospace University , 2016 .

Cao L , Jones A K , Sikka V K , et al . Anti-icing super hydrophobic coatings [J]. Langmuir , 2009 , 25 ( 21 ): 12444 - 12448 .

陈凯 , 王强 , 夏祖西 . 飞机超疏水表面的防冰性能研究进展 [J]. 应用化工 , 2016 , 45 ( 10 ): 1969 - 1973 .

Chen K , Wang Q , Xia Z X . Research progress on anti-icing performance of aircraft super-hydrophobic surface [J]. Applied Chemical Industry , 2016 , 45 ( 10 ): 1969 - 1973 .

赵安家 , 孟哲理 . 飞机结冰及预防控制措施研究 [J]. 飞机设计 , 2018 , 38 ( 3 ): 55 - 59+64 .

Zhao A J , Meng Z L . Research on aircraft icing and preventive control measures [J]. Aircraft Design , 2018 , 38 ( 3 ): 55 - 59+64 .

李艳春 . 适于飞机防/除冰的超疏水微结构的制备研究 [D]. 上海 : 上海交通大学 , 2013 .

Li Y C . Preparation of superhydrophobic microstructure suitable for aircraft anti-icing or deicing [D]. Shanghai : Shanghai Jiao Tong University , 2013 .

Joussot R , Leroy A , Weber R , et al . Plasma morphology and induced airflow characterization of a DBD actuator with serrated electrode [J]. Journal of Physics D: Applied Physics , 2013 , 46 ( 12 ): 125204-125216 .

Joussot R , Boucinha V , Weber R , et al . Thermal characterization of a DBD plasma actuator: dielectric temperature measurements using infrared thermography [C]// 40th Fluid Dynamics Conference or Exhibit . Chicago, Illinois, USA : AIAA , 2010 : 389 - 401 .

Cai J , Tian Y , Meng X , et al . An experimental study of icing control using DBD plasma actuator [J]. Experiments in Fluids , 2017 , 58 ( 8 ): 102 .

Tian Y , Zhang Z , Cai J , et al . Experimental study of an anti-icing method over an airfoil based on pulsed dielectric barrier discharge plasma [J]. Chinese Journal of Aeronautics , 2018 , ( 7 ): 1449 - 1460 .

Zhou W , Liu Y , Hu H , et al . Utilization of thermal effect induced by plasma generation for aircraft icing mitigation [J]. AIAA Journal , 2018 , 56 ( 3 ): 1 - 8 .

Kolbakir C , Liu Y , Hu H , et al . An experimental investigation on the thermal effects of NS-DBD and AC-DBD plasma actuators for aircraft icing mitigation [C]// 2018 AIAA Aerospace Sciences Meeting . Kissimmee, Florida, USA : AIAA , 2018 : 345 - 357 .

Liu Y , Kolbakir C , Hu H . A comparison study on the thermal effects in DBD plasma actuation and electrical heating for aircraft icing mitigation [J]. Heat Mass Trans . , 2018 , 124 : 319 – 330 .

Leonov S B , Petrishchev V , Adamovich I V . Dynamics of energy coupling and thermalization in barrier discharges over dielectric and weakly conducting surfaces on μs to ms time scales [J]. Journal of Physics D: Applied Physics , 2014 , 47 ( 47 ): 46 .

贺履平 . 金属材料的热辐射及其测量法 [J]. 激光与红外 , 1982 , 4 : 64 - 67 .

He L P . Thermal radiation of metal materials and its measurement method [J]. Laser and Infrared , 1982 , 4 : 64 - 67 .

王涛 . 具有高红外辐射率的绝缘导热复合材料的制备与性能研究 [D]. 天津 : 河北工业大学 , 2017 .

Wang T . Preparation and properties of insulation and thermal conductive composites with high infrared emissivity [D]. Tianjin : Hebei University of Technology , 2017 .

Shu S B , Li X , Zhang Y Z , et al . Surface temperature measurement of EAST divertor between 20 and 200°C using the emissivity model prior [J]. Infrared Physics and Technology , 2019 , 98 : 1 - 16 .

Chen J , Hua L , Wu Y , et al . Experimental study on anti-icing performance of NS-DBD plasma actuator [J]. Applied Sciences , 2018 , 8 : 1889 - 1904 .

Jia Y , Sang W , Cai Y . Numerical analysis of anti-icing property of NSDBD plasma actuator on airfoil [C]// 9th AIAA Atmospheric and Space Environments Conference . Denver, USA : AIAA , 2017 : 97 - 113 .

赵光银 , 李应红 , 梁华 , 等 . 纳秒脉冲表面介质阻挡等离子体激励唯象学仿真 [J]. 物理学报 , 2015 , 64 ( 1 ): 166 - 176 .

Zhao G Y , Li Y H , Liang H , et al . Nanosecond pulse surface dielectric barrier plasma excitation phenomenological simulation [J]. Journal of Physics , 2015 , 64 ( 1 ): 166 - 176 .

Zhu Y , Wu Y , Cui W , et al . Modelling of plasma aerodynamic actuation driven by nanosecond SDBD discharge [J]. Journal of Physics D: Applied Physics , 2013 , 46 ( 35 ): 355205 .

Civil Aviation Authority . Aircraft Icing Handbook Version 1: FAA FED AC 150/5220-20—1992 [S]. New Zealand : Safety Education and Publishing Unit , 2000 .

邵元培 , 车竞 , 丁娣 . 大飞机机翼结冰对飞行动力学特性影响研究 [J]. 飞行力学 , 2018 , 36 ( 1 ): 12 - 15+19 .

Shao Y P , Che J , Ding D . Study on the influence of aircraft aircraft wings on flight dynamics [J]. Flight Mechanics , 2018 , 36 ( 1 ): 12 - 15+19 .

浏览量

下载量

CSCD

文章被引用时，请邮件提醒。

提交

工具集

关联资源

大液滴撞击结冰传热过程及介质阻挡放电除冰实验研究

基于自驱射流装置的强化池沸腾换热研究

内管移动对卧式管壳相变储热器储放热性能影响的实验研究

石蜡/TPMS结构多孔AlSi10Mg合金复合相变材料蓄热性能实验研究

基于热质传递效应的准稳态结霜模型改进及数值验证