Thermal barrier coatings for internal combustion engines
US-2024067829-A1 · Feb 29, 2024 · US
US10400150B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10400150-B2 |
| Application number | US-201715421241-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jan 31, 2017 |
| Priority date | Feb 29, 2012 |
| Publication date | Sep 3, 2019 |
| Grant date | Sep 3, 2019 |
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Titanium dioxide is used as an emissivity enhancer in high emissivity coating compositions. The titanium dioxide increases the emissivity of the high emissivity coating compositions. In certain embodiments, titanium dioxide is recovered from industrial waste sources such as catalyst containing waste streams from olefin polymerization processes or re-based sources. Titanium dioxide emissivity enhancers recovered from industrial waste sources contribute favorably to the cost of manufacturing high emissivity coating compositions containing such enhancers.
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The invention claimed is: 1. A thermal emissivity coating composition comprising: a dry admixture of a set of emissivity agents including titanium dioxide, wherein a weight percentage of the titanium dioxide is less than approximately 20% by weight of the coating composition and at least approximately 10% by weight of the coating composition; and at least one matrix strength enhancer selected from the group consisting of silicon carbide, hafnium diboride, hafnium carbide, hafnium nitride, tantalum diboride, tantalum carbide, tantalum nitride, titanium diboride, titanium carbide, titanium nitride, zirconium diboride, zirconium carbide, and zirconium nitride. 2. The thermal emissivity coating composition of claim 1 , wherein the coating composition includes at least approximately 10% by weight of titanium dioxide and an increased emissivity value at a temperature range of between approximately 400° C. and 1300° C. 3. The thermal emissivity coating composition of claim 1 , wherein the emissivity value of the coating composition at a temperature of approximately 1000° C. increases as the percentage by weight of titanium dioxide in the coating composition increases. 4. The thermal emissivity coating composition of claim 1 , wherein the set of emissivity agents includes in addition to titanium dioxide at least one emissivity agent selected from the group consisting of silicon carbide, chromium oxide, silicon dioxide, iron oxide, boron silicide, boron carbide, silicon tetraboride, molybdenum disilicide, tungsten disilicide, and zirconium diboride. 5. The thermal emissivity coating composition of claim 1 , further comprising at least one filler selected from the group consisting of aluminum oxide, silicon dioxide, magnesium oxide, calcium oxide, and boron oxide. 6. The thermal emissivity coating composition of claim 1 , further comprising about 2.08% to about 85.71% by weight on a dry basis filler selected from aluminum oxide, silicon dioxide, magnesium oxide, calcium oxide and boron oxide. 7. The thermal emissivity coating composition of claim 1 wherein the set of matrix strength enhancers includes SiC in an amount ranging between about 8% to less than 30% on a dry weight basis. 8. The thermal emissivity coating composition of claim 1 , further comprising on a dry basis about 8% to about 20% SiC on a weight basis. 9. A thermal emissivity coating composition comprising: a dry admixture of a set of emissivity agents including titanium dioxide and at least one emissivity agent selected from the group consisting of silicon carbide, chromium oxide, silicon dioxide, iron oxide, boron silicide, boron carbide, silicon tetraboride, molybdenum disilicide, tungsten disilicide, and zirconium diboride, wherein a weight percentage of the titanium dioxide is less than approximately 20% by weight of the coating composition and at least approximately 10% by weight of the coating composition; and a set of matrix strength enhancers selected from at least one matrix strength enhance chosen from ceramic borides, ceramic carbides and ceramic nitrides. 10. The thermal emissivity coating composition of claim 9 , wherein the coating composition includes at least approximately 10% by weight of titanium dioxide and an increased emissivity value at a temperature range of between approximately 400° C. and 1300° C. 11. The thermal emissivity coating composition of claim 9 , wherein the emissivity value of the coating composition at a temperature of approximately 1000° C. increases as the percentage by weight of titanium dioxide in the coating composition increases. 12. The thermal emissivity coating composition of claim 9 , wherein the set of matrix strength enhancers includes at least one matrix strength enhancer selected from the group consisting of silicon carbide, hafnium diboride, hafnium carbide, hafnium nitride, tantalum diboride, tantalum carbide, tantalum nitride, titanium diboride, titanium carbide, titanium nitride, zirconium diboride, zirconium carbide, and zirconium nitride. 13. The thermal emissivity coating composition of claim 9 , further comprising at least one filler selected from the group consisting of aluminum oxide, silicon dioxide, magnesium oxide, calcium oxide, and boron oxide. 14. The thermal emissivity coating composition of claim 9 , further comprising about 2.08% to about 85.71% by weight on a dry basis, filler selected from aluminum oxide, silicon dioxide, magnesium oxide, calcium oxide and boron oxide. 15. The thermal emissivity coating composition of claim 9 wherein the set of matrix strength enhancers includes SiC in an amount ranging between about 8% to less than 30% on a dry weight basis. 16. The thermal emissivity coating composition of claim 15 , comprising on a dry basis about 8% to about 20% SiC on a weight basis.
inorganic · CPC title
Ceramics · CPC title
Binders based on phosphoric acids or phosphates · CPC title
Aluminum oxide or oxide forming salts thereof, e.g. bauxite, alpha-alumina · CPC title
Titanium dioxide · CPC title
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