초록 ▼

A thermal barrier coating (TBC) system (450) capable of self-healing has a substrate (420), a metal-based advanced bond coat (435) overlying the substrate and a ceramic top coat (440) overlying the bond coat. The bond coat (435) comprises ceramic oxide precursor materials capable of forming a non-al

A thermal barrier coating (TBC) system (450) capable of self-healing has a substrate (420), a metal-based advanced bond coat (435) overlying the substrate and a ceramic top coat (440) overlying the bond coat. The bond coat (435) comprises ceramic oxide precursor materials capable of forming a non-alumina ceramic oxide composition when exposed to a thermally conditioning oxidizing environment. Embodiments of such bond coat (435) comprise rare earth elements in a range of 1-20 weight percent, and Hf in a range of about 5 to 30 weight percent or Zr in a range of about 2 to 20 weight percent. Examples of self-healing TBC systems (400, 402, 404) are provided using such bond coat (435) or its advanced bond coat chemistries in combination with conventional bond coats (433, 437) or conventional bond coat chemistries.

대표청구항 ▼

The invention claimed is: 1. A thermal barrier coating (TBC) system comprising: a substrate; a metal-based bond coat overlying the substrate; and a ceramic top coat overlying the metal-based bond coat; wherein the metal-based bond coat comprises ceramic oxide precursor materials that, after heating

The invention claimed is: 1. A thermal barrier coating (TBC) system comprising: a substrate; a metal-based bond coat overlying the substrate; and a ceramic top coat overlying the metal-based bond coat; wherein the metal-based bond coat comprises ceramic oxide precursor materials that, after heating the metal-based bond coat to over 900 degrees Celsius in an oxidizing atmosphere, form a non-alumina ceramic oxide layer toward a surface directly associated with the ceramic top coat, the non-alumina ceramic oxide layer comprising a thermal conductivity coefficient between 0.2 and 1.2 W/m�� K. 2. The TBC system of claim 1, wherein the thermal conductivity coefficient of the non-alumina ceramic oxide layer is between 0.4 and 0.8 W/m�� K. 3. The TBC system of claim 1, wherein the metal-based bond coat comprises between about 5 and about 30 weight percent hafnium, or between about 2 and about 30 weight percent zirconium as the ceramic oxide precursor materials. 4. The TBC system of claim 3, wherein the ceramic oxide precursor materials additionally comprise one or more rare earth elements selected from the group consisting of cerium, dysprosium, erbium, europium, gadolinium, holmium, lanthanum, lutetium, neodymium, praseodymium, samarium, terbium, thulium ytterbium, and yttrium, the one or more rare earth elements capable of forming the non-alumina ceramic oxide layer with the hafnium or the zirconium. 5. The TBC system of claim 4 wherein the total weight percent in the metal-based bond coat of the one or more rare earth elements is between about one and about twenty percent. 6. The TBC system of claim 4 wherein the total weight percent in the metal-based bond coat of the one or more rare earth elements is greater than three to about twenty percent. 7. The TBC system of claim 1, wherein the metal-based bond coat comprises between about 5 and about 30 weight percent hafnium, or between about 2 and about 20 weight percent zirconium; and one or more rare earth elements selected from the group consisting of cerium, dysprosium, erbium, europium, gadolinium, holmium, lanthanum, lutetium, neodymium, praseodymium, samarium, terbium, thulium, ytterbium, and yttrium; wherein the one or more rare earth elements is/are capable of forming the ceramic oxide layer that comprises oxides of zirconium or hafnium. 8. The TBC system of claim 1, wherein the metal-based bond coat comprises yttrium at a concentration between 1 and 20 weight percent of a NiCrAlY, a CoCrAlY or a CoNiCrAlY composition that comprises the metal-based bond coat. 9. The TBC system of claim 1, wherein the non-alumina ceramic oxide layer has a Coefficient of Thermal Expansion (CTE) greater than 8 μm/m�� C. 10. A thermal barrier coating (TBC) system comprising: a substrate; a metal-based bond coat overlying the substrate; and a ceramic top coat; the metal-based bond coat comprising ceramic oxide precursor materials that, after heating the metal-based bond coat to over 900 degrees Celsius in an oxidizing atmosphere, form a non-alumina ceramic oxide layer toward a surface directly associated with the ceramic top coat and, the metal-based bond coat comprising: Co, 24-38 weight percent; Ni, 20-32 weight percent; Cr, 11-20 weight percent; Al, 5-7 weight percent; one or more rare earth elements totaling 2.99-20 weight percent; and at least one of Hf, at 9-30 weight percent, and Zr, at 2-20 weight percent, wherein the non-alumina ceramic oxide layer comprises Hf or Zr. 11. The TBC system of claim 10, wherein the thermal conductivity coefficient of the non-alumina ceramic oxide layer is between 0.2 and 1.2 W/m�� K. 12. The TBC system of claim 10, wherein the thermal conductivity coefficient of the non-alumina ceramic oxide layer is between 0.4 and 0.8 W/m�� K. 13. The TBC system of claim 10, wherein the non-alumina ceramic oxide layer has a Coefficient of Thermal Expansion (CTE) greater than about 8 μm/m�� C. 14. A thermal barrier coating (TBC) system comprising: a substrate; a first advanced bond coat overlying the substrate; and a ceramic top coat overlying the first advanced bond coat; wherein the first advanced bond coat comprises ceramic oxide precursor materials capable of forming a non-alumina ceramic oxide layer when exposed to an oxidizing atmosphere at over 900 degrees Celsius, effective to self-heal the TBC system upon a loss of a region of the overlying ceramic top coat. 15. The TBC system of claim 14, wherein the first advanced bond coat comprises the elements: Co, 24-38 weight percent; Ni, 20-32 weight percent; Cr, 11-20 weight percent; Al, 5-7 weight percent; one or more rare earth elements totaling 2.99-20 weight percent; and at least one of Hf, at 9-30 weight percent, and Zr, at 2-20 weight percent. 16. The TBC system of claim 14, wherein a transitioning bond coat comprises a gradient transitioning from a bond coat region that forms alumina or chromia and that overlies the substrate to the first advanced bond coat directly adjacent the ceramic top coat. 17. The TBC system of claim 14, comprising a first bond coat layer that forms alumina or chromia and that overlies the substrate, and the first advanced bond coat overlying the first bond coat layer. 18. The TBC system of claim 17, wherein the first bond coat layer comprises a composition adapted to form an alumina or a chromia layer when exposed to over 900 degrees Celsius. 19. The TBC system of claim 14, wherein a multi-layer bond coat comprises: a first bond coat layer overlying the substrate, comprising a composition adapted to form an alumina or a chromia layer when exposed to over 900 degrees Celsius; the first advanced bond coat overlying the first bond coat layer; and a second bond coat layer overlying the first advanced bond coat, comprising a composition adapted to form an alumina or a chromia layer when exposed to over 900 degrees Celsius. 20. The TBC system of claim 15, wherein the elements of the first advanced bond coat are provided over the substrate from a powder prepared by gas atomization.