| CPC C09D 175/06 (2013.01) [C08G 18/4238 (2013.01); C08G 18/6225 (2013.01); C08G 18/78 (2013.01); C08G 18/7893 (2013.01); C09D 7/20 (2018.01); C09D 7/62 (2018.01)] | 12 Claims |
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1. A method for coating a substrate selected from rotor blades of wind turbines, rotor blades of helicopters, ship screws and aircraft, the method comprising:
applying a two-component solvent-based coating composition to the substrate; and
allowing the applied coating composition to cure,
wherein the two-component, solvent-based coating composition comprises
i) a base component comprising
(A) one or more polyester diols having a hydroxyl value in the range of from 150 to 500 mg KOH/g polyester diol;
(B) optionally one or more hydroxyl-functional acrylate resins having a hydroxyl value in the range of from 75 to 500 mg KOH/g resin; and
(C) one or more organosilane-modified inorganic fillers; and
ii) a curing component comprising
(D) one or more polyisocyanates,
in such amounts that the coating composition comprises:
5 to 50 wt % of the one or more polyester diols (A);
0 to 25 wt % of the one or more hydroxyl-functional acrylate resins (B);
10 to 70 wt % of the one or more organosilane-modified inorganic fillers (C);
5 to 40 wt % of the one or more polyisocyanates (D);
wherein the base component comprises no resins other than the one or more polyester diols (A) and any hydroxyl-functional acrylate resins (B);
the one or more polyisocyanates (D) are selected from trimers of di-isocyanates;
the coating composition comprises one or more organic solvents in an amount in the range of from 5 to 35 wt %; and
the coating composition has a viscosity in the range of from 50 to 2,000 mPa·s as measured by means of a rotary viscometer at a shear rate of 1000 s−1 and a temperature of 23° C., 30 seconds after combining and mixing the base component and the curing component.
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