New icephobic paint has been developed for the purpose of preventing the icing of the airfoils of aircrafts. The basic characteristics of the paint in terms of icing prevention were examined by an optical method and a load test. The water contact angle is so high-150 degrees-that high water repellency can be obtained as expected from the design. The adhesion strength of the ice formed on this coating is decreased to the lowest value as compared to all paints ever developed. The results from the icing wind tunnel test carried out in conditions similar to what aircrafts encounter show that the paint contributes to fuel and weight savings due to the effective use of deicer.
A New Surface Coating for Prevention of Icing on Airfoils
Sae Technical Papers
2007 SAE Aircraft and Engine Icing International Conference ; 2007
2007-09-24
Aufsatz (Konferenz)
Englisch
A New Surface Coating for Prevention of Icing on Airfoils
British Library Conference Proceedings | 2007
|Improved Hybrid System Protects Airfoils Against Icing
Online Contents | 1998
Ice Accretions and Icing Effects for Modern Airfoils
NTRS | 2000
|Icing Numerical Simulation for Single and Multi-Element Airfoils
British Library Conference Proceedings | 2010
|Boundary-Layers Integral Analysis - Heated Airfoils in Icing Conditions
British Library Conference Proceedings | 2008
|