New Coatings Reduce Impact Ice Adhesion Strength

NASA is developing polymer coatings that reduce impact ice adhesion strength. Current coating compositions are based on epoxy resins due to their availability and ease of fabrication. It is anticipated that a successful composition could be used in other polymer classes such as polyurethanes. Initial molecular modeling studies of silanes terminated with various functionalities suggest that chain mobility effects the interface between ice and the surface. To that end, surfaces coated with these compounds were applied to aluminum substrates and the resulting monolayer coating investigated to assess the effect of chemical functionality and chain length under simulated in-flight icing conditions. As shown in the figure below, these molecular coatings demonstrated reduced ice adhesion strength, presumably as a result of the molecular flexibility imbued by the aliphatic chains that has been incorporated into polymers either within the polymer backbone or as pendant groups. Compared to an untreated aluminum alloy surface, a test polymer coating employing in-chain molecular flexibility exhibited a 56% reduction in ice adhesion strength at -16 C. Similarly, another test polymer coating employing pendant group molecular flexibility exhibited a 19% reduction and a 63% reduction in ice adhesion strength at -16 C compared to an aluminum alloy surface and a rigid epoxy control surface, respectively. The reduced ice adhesion strength may lead to decreased energy requirements for active ice mitigation strategies currently used on aircraft when used in conjunction. These anti-icing coatings are a passive approach that are anticipated to be applied to the aircraft surface either as a topcoat or as a constituent of aircraft paint. The coatings need to be optimized for durability, with the goal of achieving a reapplication frequency consistent with routine aircraft maintenance and painting requirements.