Durability of superhydrophobic duplex coating systems for aerospace applications

In-flight icing, caused by the collision of supercooled water droplets with exposed aircraft surfaces, is an important safety hazard and a major issue in aviation. Superhydrophobic surfaces (SHS) have been shown to offer improvements to heating-based anti-icing and de-icing systems, reducing energy...

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Veröffentlicht in:Surface & coatings technology 2020-11, Vol.401, p.126249, Article 126249
Hauptverfasser: Brown, Stephen, Lengaigne, Jacques, Sharifi, Navid, Pugh, Martin, Moreau, Christian, Dolatabadi, Ali, Martinu, Ludvik, Klemberg-Sapieha, Jolanta E.
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container_issue
container_start_page 126249
container_title Surface & coatings technology
container_volume 401
creator Brown, Stephen
Lengaigne, Jacques
Sharifi, Navid
Pugh, Martin
Moreau, Christian
Dolatabadi, Ali
Martinu, Ludvik
Klemberg-Sapieha, Jolanta E.
description In-flight icing, caused by the collision of supercooled water droplets with exposed aircraft surfaces, is an important safety hazard and a major issue in aviation. Superhydrophobic surfaces (SHS) have been shown to offer improvements to heating-based anti-icing and de-icing systems, reducing energy requirements for ice prevention and facilitating ice removal. A common SHS fabrication technique is to develop a surface with hierarchical roughness, and to then coat this surface with a hydrophobic topcoat. From this arises an issue: the durability of the entire system is fundamentally limited to the durability of this topcoat. In the present study, we develop a superhydrophobic duplex coating system with an emphasis on the environmental durability of the thin hydrophobic layer. The system consists of a thick TiO2 coating deposited by suspension plasma spraying, and a thin coating stack deposited by plasma enhanced chemical vapor deposition. The thin coating stack is based on DLC:SiOx—diamond-like carbon networked with silicon oxide—which exhibits a water contact angle of up to 95° and a hardness of up to 11 GPa, while the full coating system offers a contact angle of 159° and a contact angle hysteresis of 3.8°. The coating system is exposed to icing/deicing cycling, as well as rain erosion and accelerated aging tests; the results are compared with TiO2 coatings using stearic acid and fluoropolymer hydrophobic layers, as well as a commercially available superhydrophobic spray. The duplex coating system is shown to maintain water droplet mobility after 170 icing/deicing cycles, is resistant to prolonged UV and high-temperature exposure and offers a 300-fold improvement over the stearic acid in rain erosion tests. •A new thin-on-thick coating system is developed, with PECVD coatings applied over suspension plasma sprayed TiO2.•Environmental durability is compared to other thin hydrophobic topcoats on TiO2 and a commercial spray coating.•Developed coating system survived 170 icing/deicing cycles in an icing wind tunnel.•Degradation in icing/deicing cycle tests was found to be primarily chemical.•Developed coating system offers a 300-fold improvement over stearic acid in rain erosion tests.
doi_str_mv 10.1016/j.surfcoat.2020.126249
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subjects Accelerated aging tests
Aircraft accidents
Aircraft hazards
Contact angle
Deicing
Diamond-like carbon films
DLC
Droplets
Durability
Energy requirements
Environmental durability
Exposure
Fluoropolymers
High temperature
Hydrophobic surfaces
Hydrophobicity
Ice prevention
Ice removal
Icing
PECVD
Plasma enhanced chemical vapor deposition
Plasma spray
Plasma spraying
Protective coatings
Rain
Rain erosion
Silicon oxides
Stearic acid
Superhydrophobicity
Titanium dioxide
Water drops
title Durability of superhydrophobic duplex coating systems for aerospace applications
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