Investigation of ice shedding properties of superhydrophobic coatings on helicopter blades

被引:103
作者
Tarquini, Stefania [1 ]
Antonini, Carlo [1 ,2 ]
Amirfazli, Alidad [3 ]
Marengo, Marco [1 ]
Palacios, Jose [4 ]
机构
[1] Univ Bergamo, Dept Engn, Dalmine, BG, Italy
[2] ETH, Mech & Proc Engn Dept, Lab Thermodynam Emerging Technol, CH-8092 Zurich, Switzerland
[3] York Univ, Dept Mech Engn, Toronto, ON M3J13P, Canada
[4] Penn State Univ, Dept Aerosp Engn, University Pk, PA 16802 USA
关键词
Helicopter icing; Blade de-icing; Superhydrophobic surfaces; Icephobic surfaces; Ice adhesion strength; Ice regimes; WATER; ADHESION; STRENGTH; SURFACES; IMPACT;
D O I
10.1016/j.coldregions.2013.12.009
中图分类号
X [环境科学、安全科学];
学科分类号
08 ; 0830 ;
摘要
The state-of-the-art of icing protection systems for helicopter rotor blades is based on active thermal de-icing systems that require large amounts of power. This work focused on assessing the potential icephobicity of superhydrophobic coatings as an alternative passive strategy. Ice shedding tests were conducted in a helicopter blade icing chamber, to simulate atmospheric icing conditions. Ice accretion and shedding were tested on four different materials, including two common metals and two superhydrophobic materials, with the objective of evaluating icephobic potential for anti-icing purposes. Coating test results showed a strong influence of temperature and surface roughness on the ice adhesion: the strength increased when temperature decreased and roughness increased. Ice regime was independent of the type of surface used, but superhydrophobic surfaces resulted in a thinner ice shape in comparison with common metals, which resulted in a shorter shedding time, especially in rime ice conditions. The relationship between ice regime and adhesion load showed that ice adhesion load substantially increases in rime ice conditions, demonstrating that ice regime is an important parameter in the ice adhesion process. Additional results showed that superhydrophobic surfaces were associated with a decrease in the adhesion load with respect to the baseline materials ranging from the 16% to the 70% in the best case; but this reduction may not be revealing for practical applications as ice reduction mechanisms need to be first understood. (C) 2014 Elsevier B.V. All rights reserved.
引用
收藏
页码:50 / 58
页数:9
相关论文
共 48 条
[1]   Dynamics of Ice Nucleation on Water Repellent Surfaces [J].
Alizadeh, Azar ;
Yamada, Masako ;
Li, Ri ;
Shang, Wen ;
Otta, Shourya ;
Zhong, Sheng ;
Ge, Liehui ;
Dhinojwala, Ali ;
Conway, Ken R. ;
Bahadur, Vaibhav ;
Vinciquerra, A. Joseph ;
Stephens, Brian ;
Blohm, Margaret L. .
LANGMUIR, 2012, 28 (06) :3180-3186
[2]  
Anderson D., 1997, AER SCI M EXH 35 REN
[3]  
Anderson DN, 2004, NASA CR
[4]  
[Anonymous], 2006, 2073A FAA
[5]   Drop Rebound after Impact: The Role of the Receding Contact Angle [J].
Antonini, C. ;
Villa, F. ;
Bernagozzi, I. ;
Amirfazli, A. ;
Marengo, M. .
LANGMUIR, 2013, 29 (52) :16045-16050
[6]   Understanding the effect of superhydrophobic coatings on energy reduction in anti-icing systems [J].
Antonini, C. ;
Innocenti, M. ;
Horn, T. ;
Marengo, M. ;
Amirfazli, A. .
COLD REGIONS SCIENCE AND TECHNOLOGY, 2011, 67 (1-2) :58-67
[7]   Dynamic Defrosting on Nanostructured Superhydrophobic Surfaces [J].
Boreyko, Jonathan B. ;
Srijanto, Bernadeta R. ;
Trung Dac Nguyen ;
Vega, Carlos ;
Fuentes-Cabrera, Miguel ;
Collier, C. Patrick .
LANGMUIR, 2013, 29 (30) :9516-9524
[8]   Delayed Frost Growth on Jumping-Drop Superhydrophobic Surfaces [J].
Boreyko, Jonathan B. ;
Collier, C. Patrick .
ACS NANO, 2013, 7 (02) :1618-1627
[9]  
Brouwers E.W., 2011, P 67 AM HELICOPTER S, P3011
[10]   Anti-Icing Superhydrophobic Coatings [J].
Cao, Liangliang ;
Jones, Andrew K. ;
Sikka, Vinod K. ;
Wu, Jianzhong ;
Gao, Di .
LANGMUIR, 2009, 25 (21) :12444-12448