4.6 Article

A Wind Tunnel Test of the Anti-Icing Properties of MoS2/ZnO Hydrophobic Nano-Coatings for Wind Turbine Blades

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COATINGS
卷 13, 期 4, 页码 -

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MDPI
DOI: 10.3390/coatings13040686

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anti-icing; hydrophobic coating; MoS2; ZnO; wind turbine blade; wind tunnel test

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Wind turbines operating in cold regions often face the problem of blade icing, which can have a negative impact on their aerodynamic characteristics and safety performance. In this study, MoS2/ZnO/PDMS superhydrophobic nano-anti-icing coatings were developed to address this issue. The coatings exhibited a thin sheet-like morphology and a hilly nano-rough structure, resulting in high contact angles and low sliding angles. The results of wind tunnel tests showed that the MoS2/ZnO coatings reduced the level of icing on the blade airfoil surface compared to uncoated blades, highlighting the potential of these coatings for anti-icing applications.
Wind turbines operating in cold regions are prone to blade icing, which seriously affects their aerodynamic characteristics and safety performance. Coatings are one of the effective solutions to the icing problem on wind turbine blades. In this study, MoS2/ZnO/PDMS superhydrophobic nano-anti-icing coatings were prepared using the hydrothermal method and the liquid phase method. SEM revealed that the MoS2/ZnO coating was a typical superhydrophobic nanostructure with an ultra-thin sheet-like morphology of clusters and a hilly nano-rough structure, with contact angles (CA) of 152.1 degrees and 4.7 degrees with water droplets and the sliding angle (SA), respectively. The MoS2/ZnO/PDMS coating had an adhesion strength to ice of 78 kPa, which was 60.2% lower than an uncoated surface. The icing effects of the NACA0018 airfoil blade model with or without MoS2/ZnO coatings were studied at different ambient temperatures and wind speeds using the icing wind tunnel test. The results showed that, compared to uncoated blades, the level of icing was lower on the blade airfoil surface that was coated with MoS2/ZnO. At 10 m/s and -10 degrees C, the icing thickness and icing area of the leading edge of the blade airfoil were 13.7% and 28.3% lower, respectively. This study provides a valuable reference for the development of anti-icing coatings for wind turbine blades.

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