An explorative study was performed to demonstrate the feasibility of using a novel hybrid anti-/de-icing strategy for aircraft icing mitigation. The hybrid method was developed by combining the electro-thermal heating mechanism and specialized surfaces/coatings with different wettabilities. While an electrical film heater was utilized to provide thermal energy around the leading edge of a NACA0012 airfoil model, two different coating strategies, (i.e., (a). Superhydrophobic coating covering the entire airfoil surface to increase droplets bounce-off and accelerate surface water runback vs. (b). super-hydrophilic coating at the leading edge to increase evaporation area + superhydrophobic coating in downstream to prevent runback refreezing) were proposed and evaluated aiming at maximizing the anti-/de-icing efficiency of the hybrid method. While a series of experiments were conducted to examine the dynamics of droplet impinging onto the different surfaces (i.e., superhydrophobic vs. super-hydrophilic), a comprehensive experimental study was carried out in the Icing Research Tunnel at Iowa State University (i.e., ISU-IRT) to evaluate the anti-/de-icing performance of the hybrid method with the different coating strategies. It was found that, while both of the coating strategies could promote better anti-/de-icing performance of the hybrid method in comparison to the conventional heating-only method at rime ice condition. For glazed ice condition, the use of superhydrophobic coating over the entire airfoil surface would result in a maximized anti-/de-icing efficiency of the hybrid method (i.e., achieve a complete ice prevention with only 3% chord length covered with the electrical film heater), attributing to the significant droplets bounce-off and accelerated surface water runback behaviors.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    An Explorative Study to Use Super-Hydrophilic/Super-Hydrophobic Hybrid Surfaces for Aircraft Icing Mitigation


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Hu, Haiyang (Autor:in) / Hu, Hui (Autor:in) / Liu, Yang (Autor:in)

    Kongress:

    International Conference on Icing of Aircraft, Engines, and Structures ; 2019



    Erscheinungsdatum :

    2019-06-10




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    An Explorative Study to Use Super-Hydrophilic/Super-Hydrophobic Hybrid Surfaces for Aircraft Icing Mitigation

    Hu, Haiyang / Hu, Hui / Liu, Yang | British Library Conference Proceedings | 2019


    An Explorative Study to Use Graphene-based Materials for Aircraft Icing Mitigation

    Eluchie, Chukwudum / Hu, Haiyang / Johnson, Zachary et al. | AIAA | 2022



    Super-hydrophobic anti-icing aviation aluminum alloy surface and production method

    ZHONG MINLIN / ZHANG HONGJUN / PAN RUI | Europäisches Patentamt | 2020

    Freier Zugriff

    Hydrophobic Coating Study for Anti-icing Aircraft

    Aoki, Akihito / Sakaue, Hirotaka / Morita, Katsuaki et al. | SAE Technical Papers | 2011