Superhydrophobic Compositions And Coating Process For The Internal Surface Of Tubular Structures
US-2015337170-A1 · Nov 26, 2015 · US
US9879657B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9879657-B2 |
| Application number | US-201314440188-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 15, 2013 |
| Priority date | Dec 20, 2012 |
| Publication date | Jan 30, 2018 |
| Grant date | Jan 30, 2018 |
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The present invention relates to rotor blades of devices, particularly of wind turbines, having an anti-ice coating, as well as to methods for their production and their use.
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The invention claimed is: 1. A method of coating a rotor blade to lower a freezing point of water on the rotor blade, the method comprising: lowering the freezing point of water on the rotor blade by coating at least one surface of the rotor blade with a coating selected from a group consisting of a first coating containing 15 to 75 atom-% fluorine and 25 to 85 atom-% further components (each determined according to XPS analysis) and a second coating containing 25 to 29 atom-% silicon, 22 to 45 atom-% oxygen, and 26 to 49 atom-% carbon (each determined according to XPS analysis), the coating having a structuring in a form of a dot pattern or a line pattern. 2. The method according to claim 1 , wherein the structuring in a form of a dot pattern or a line pattern has structuring in the micrometer range having dimensions of 1 to 1000 μm, and the coating further has a structuring in the nanometer range having dimensions of 0.02 to 40 nm. 3. The method according to claim 1 , wherein the coating has a thickness of 10 nm to 500 nm. 4. A rotor blade having a lowered freezing point comprising: a main body; and a coating lowering a freezing point of water on the main body of the rotor blade, the coating selected from a group consisting of a first coating containing 15 to 75 atom-% fluorine and 25 to 85 atom-% further components (each determined according to XPS analysis) and a second coating containing 25 to 29 atom-% silicon, 22 to 45 atom-% oxygen, and 26 to 49 atom-% carbon (each determined according to XPS analysis), wherein the coating is provided on at least one surface of the rotor blade and has a structuring in a form of a dot pattern or a line pattern. 5. The rotor blade according to claim 4 , wherein the structuring in a form of a dot pattern or a line pattern has structuring in the micrometer range having dimensions of 1 to 1000 μm, and the coating further has a structuring in the nanometer range having dimensions of 0.02 to 40 nm. 6. The rotor blade according to claim 4 , wherein the coating has a thickness of 10 nm to 500 nm. 7. A method of coating a rotor blade to lower a freezing point of water on the rotor blade, the method comprising: lowering the freezing point of water on the rotor blade by coating at least one surface of the rotor blade with a coating selected from a group consisting of a first coating containing 15 to 75 atom-% fluorine and 25 to 85 atom-% further components (each determined according to XPS analysis) and a second coating containing 25 to 29 atom-% silicon, 22 to 45 atom-% oxygen, and 26 to 49 atom-% carbon (each determined according to XPS analysis), the coating having a thickness of 10 nm to 500 nm, a first structuring in a form of a dot pattern or a line pattern having first structuring in the micrometer range having dimensions of 1 to 1000 μm, and a second structuring in the nanometer range having dimensions of 0.02 to 40 nm.
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