Monazite-based thermal barrier coatings
View Patent ↗Monazites and xenotimes are rare-earth phosphates showing a combination of properties expected to be suitable for thermal barrier coatings. For example, lanthanum phosphate (La-monazite) can be used to form thermal barrier coatings to protect superalloy and ceramic parts exposed to high temperature and damage by sulfur, vanadium, phosphorus and other contaminants. The monazite or xenotime coatings can be applied using any of the common application methods including EB-PVD, laser ablation and plasma spraying. The stoichiometry of the coatings can be modulated according to the stoichiometry of specially prepared starting target (source) material. The most effective coatings appear to be largely crystalline and show a columnar structure with feather-like microstructure. For La-monazite, effective coatings between 10 and 500 micrometers in thickness can be deposited on substrates having temperatures between about 750° C. and about 950° C.
1. A thermal barrier coating comprising a layer of rare-earth element phosphate said layer having a thickness greater than about 20 micrometers, a thermal conductivity less than about 2 W/mK and disposed on an exterior surface of one of a ceramic substrate and a metallic substrate selected from the group consisting of a nickel-based superalloy, an iron-based superalloy and a cobalt-based superalloy so as to thermally protect the substrate, and further comprising a layer of aluminum phosphate disposed between the layer of rare-earth element phosphate and the substrate.
2. The thermal barrier coating according to claim 1 further comprising a monazite or xenotime crystal structure.
3. The thermal barrier coating according to claim 1 , wherein the ratio between rare-earth element and phosphate is about 1:1.
4. The thermal barrier coating according to claim 1 , wherein the layer has a thickness between about 20 and 500 micrometers.
5. The thermal barrier coating according to claim 1 deposited on a substrate having a temperature between 600° C. and 1100° C.
6. The thermal barrier coating according to claim 5 deposited on a substrate having a temperature between 750° C. and 950° C.
7. The thermal barrier coating according to claim 1 formed by a process selected from the group consisting of chemical vapor deposition, physical vapor deposition, electron beam evaporation, pulsed electron beam evaporation, laser ablation, and plasma spraying.
8. The thermal barrier coating according to claim 7 using single or multiple sources of materials selected from the group consisting of rare-earth phosphates and mixtures of rare-earth precursors with phosphorous precursors.
9. The thermal barrier coating according to claim 1 formed with a columnar microstructure.
10. The thermal barrier coating according to claim 1 formed with a porous microstructure.
11. The thermal barrier coating according to claim 1 , wherein the phosphate is lanthanum phosphate.
12. The thermal barrier coating according to claim 1 further comprising a layer of alumina between the metallic substrate and said rare-earth element phosphate.
13. The thermal barrier coating according to claim 12 further comprising a region of rare-earth aluminate between the alumina and said rare-earth element phosphate.
14. A thermal barrier coating comprising a layer of comprising a mixture of lanthanum phosphate, cerium phosphate and neodymium phosphate rare-earth element phosphate said layer having a thickness greater than about 20 micrometers, a thermal conductivity less than about 2 W/mK and disposed on an exterior surface of a substrate so as to thermally protect the substrate.
15. A thermal barrier coating comprising a layer of lanthanum phosphate said layer having a thickness greater than about 20 micrometer and disposed on an exterior surface of one of a ceramic substrate and a metallic substrate selected from the group consisting of a nickel-based superalloy, an iron-based superalloy and a cobalt-based superalloy so as to thermally protect the substrate, and further comprising a layer of aluminum phosphate disposed between the layer of lanthanum phosphate and the substrate.
16. The thermal barrier coating according to claim 15 further comprising a monazite crystal structure.
17. The thermal barrier coating according to claim 15 , wherein the ratio between lanthanum and phosphate is about 1:1.
18. The thermal barrier coating according to claim 15 , wherein the layer has a thickness between about 20 and 500 micrometers.
19. The thermal barrier coating according to claim 15 deposited on a substrate having a temperature between 600° C. and 1100° C.
20. The thermal barrier coating according to claim 19 deposited on a substrate having a temperature between 750° C. and 950° C.
21. The thermal barrier coating according to claim 15 formed by a process selected from the group consisting of chemical vapor deposition, physical vapor deposition, electron beam evaporation, pulsed electron beam evaporation, laser ablation, and plasma spraying.
22. The thermal barrier coating according to claim 21 using single or multiple sources of materials selected from the group consisting of rare-earth phosphates and mixtures of rare-earth precursors with phosphorous precursors.
23. The thermal barrier coating according to claim 15 formed with a columnar microstructure.
24. The thermal barrier coating according to claim 15 formed with a porous microstructure.
25. The thermal barrier coating according to claim 15 further comprising a layer of alumina between the metallic substrate and the lanthanum phosphate.
26. The thermal barrier coating according to claim 25 further comprising a region of lanthanum aluminate between the alumina and the lanthanum phosphate.
27. A thermal barrier coating comprising a layer of a mixture of lanthanum phosphate, cerium phosphate and neodymium phosphate lanthanum phosphate said layer having a thickness greater than about 20 micrometer and disposed on an exterior surface of a substrate so as to thermally protect the substrate.
28. A thermal barrier coating comprising a layer of a mixture of rare-earth element phosphates and refractory oxides said layer having a thickness greater than about 20 micrometers, a thermal conductivity less than about 2 W/mK and disposed on an exterior surface of one of a ceramic substrate and a metallic substrate selected from the group consisting of a nickel-based superalloy, an iron-based superalloy and a cobalt-based superalloy so as to thermally protect the substrate, and further comprising a layer of aluminum phosphate disposed between the mixture and the substrate.
29. The thermal barrier coating according to claim 28 , wherein the layer has a thickness between about 20 and 500 micrometers.
30. The thermal barrier coating according to claim 28 deposited on a substrate having a temperature between 600° C. and 1100° C.
31. The thermal barrier coating according to claim 28 formed by a process selected from the group consisting of chemical vapor deposition, physical vapor deposition, electron beam evaporation, pulsed electron beam evaporation, laser ablation, and plasma spraying.
32. The thermal barrier coating according to claim 28 formed with a columnar microstructure.
33. The thermal barrier coating according to claim 28 formed with a porous microstructure.
34. A thermal barrier coating comprising a layer of a mixture of rare-earth element phosphates and refractory oxides said layer having a thickness greater than about 20 micrometers, a thermal conductivity less than about 2 W/mK and disposed on an exterior surface of a substrate so as to thermally protect the substrate further comprising a layer of alumina between the substrate and the mixture.
35. The thermal barrier coating according to claim 34 further comprising a region of rare-earth aluminate between the alumina and said rare-earth element phosphates.