MENKE CHRISTIAN (DE)
| US8317473B1 | 2012-11-27 | |||
| US6074706A | 2000-06-13 | |||
| US20090017260A1 | 2009-01-15 | |||
| US20140174092A1 | 2014-06-26 | |||
| EP1245787A2 | 2002-10-02 |
| Patent claims 1. Component ( 1 ) , which comprises: a substrate (22) a ceramic thermal barrier coating (25) on the substrate (22) , at least one row (7) of cooling holes (10', 10'', ...) along a direction (14) in the substrate (4) and in the thermal barrier coating (25) , wherein the thermal barrier coating (25) has at least one engraving, characterized by that, that the at least one engraving is a long continuous engraving (16, 19, 116, 20, 216, 31) along the direction (14) before and/or after of the at least one row (7) . 2. Component according to claim 1, wherein the engraving (16, 19, 20) is straight. 3. Component according to one or both of the claims 1 or 2, wherein the engraving (116, 216, 31) is multiple curved. 4. Component according to one or any of the preceding claims , wherein the engraving (16, 19, 20, 116, 216, 31) is long and continuous and which is not connecting with each other or endless. 5. Component according to one or any of the preceding claims, wherein several engravings (16, 19, 20, 116, 216, 31) are arranged in the thermal barrier coating (25) . 6. Component according to one or any of the claims 1, 2, 3 4 or 5, wherein the engraving (16, 19, 116, 20, 216, 31) is only arranged before and after one row (7) . 7. Component according to one or any of the claims 1, 2, 3, 4, 5 or 6, wherein the substrate (22) has a metallic overlay coating. 8. Component according claim 7, wherein the engraving (16, 19, 20, 116, 216, 31) has a depth that reaches the outer surface of a metallic coating on the substrate (4) . 9. Component according to one or any of the preceding claims , wherein the engraving (16, 19, 20, 116, 216, 31) is only arranged in the thermal barrier coating and does not reach the substrate (4) or a metallic coating. 10. Component to one or any of the preceding claims, wherein the engraving (16, 19, 116, 216, 31) starts at the beginning and ends at the end of a row (7) . 11. Component to one or any of the preceding claims, wherein both engravings (16, 19, 116, 216, 31) have a distance to each other along an overflow direction (13) of 1mm to 2mm. 12. Component to one or any of the preceding claims 3 to 11, wherein the distance of a curved engraving (116, 20; 216, 31) to a straight engraving (20) or to a curved engraving (31) is smaller between two cooling holes (10", 10"") of these two engravings. 13. Component according to one or any of the preceding cl aims , wherein the substrate (22) is a nickel- or cobalt-based super alloy. |
This invention relates to a ceramic surface structure, wherein a long engraving is present along a row of cooling holes.
The highly loaded turbine blades and vanes require the application of different protection technologies in order to be able to withstand the high thermal loading. The front stages of the turbine blades and vanes require a ceramic coating and the film cooling technology as well as the internal cooling.
The application of such technologies is helpful as long as the combination works during operation and no spallation occurs or nor cooling holes blockage is noticed.
The manufacturing of the film cooling holes could be one of the reasons for the ceramic coating spallation.
Parameters of the laser drilling causes cracks within the ceramic coating, which later spalls down and restricts the operation of the component.
On the other hand it is not possible to reduce the laser drilling energy to a very low level due to the fact that no drilling will take place with low energy.
It is therefore the aim of the invention to improve the lifetime of a ceramic coating and preventing the overall spallation of a TBC . This problem is solved by a ceramic surface structure according to claim 1.
In the dependent claims further developments are disclosed which can be arbitrarily combined which each other to yield further new advantages.
Figures 1, 3, 4 show a view on top of the surface of a
TBC and a row of cooling holes, Figure 2 shows a cross-section area of Figure 1.
By an implementation of a polymer masking it is possible to introduce the suggested design in figures 1 - 4. The polymer masking will provide a ceramic free region along the cooling holes .
This manufacturing procedure has following advantage: · The engraving will not reduce the bond coat thickness as during a laser engraving
• This step can be carried out during the coating
• In case of casting and coating deviations, the polymer masking will not affect the bond coat thickness.
The width of such a ceramic free region could vary between 1 and 2mm.
The positive effect of the engraving is the spallation behavior. In case of spallation the spalled region will not be extended on wide regions.
Another positive effect of the engraving is the vortices introduced due to the no-APS regions, which forces the hot gas flow to stick to the wall as by the dimples on a golf ball. During operation the step within the ceramic coating will be smoothened as well as the APS smoothening procedure will help breaking the edges.
The following positive effects are related to the engraving:
• Retrofitable with current designs
• In case of spallation, only restricted region will be affected
• Lower operation risk
· Reduced rework after laser drilling
• Applicable to all spallation threatened cooling holes rows
• Applicable to vanes and blades. Figure 1 shows a view on the top of a ceramic coating 25 (Figure 2) .
The thermal barrier coating 25 (TBC) is part of a component 1 which has a substrate 22 (Figure 2) wherein on top of the substrate 22 the thermal barrier coating 25 is applied.
This component 1 has at least one row 7 of cooling holes 10', 10'',..., which are during use of the component 1 overflowed by hot gas according the arrow 13, especially almost
perpendicular to the direction 14 of the row 7. The direction 14 is straight or has only one or two times a break of slope of maximum 25°.
Along the direction 14 of the row 7 of the cooling holes 10', 10'', ... there is especially only before the row 7 an
engraving 16 and/or after the row 7 a second engraving 19.
These engravings 16, 19 are continuous, especially straight engravings in the TBC 25.
The engravings 16, 19, 20, 116, 216, 31 (Fig. 3, 4) are not endless, e. g. not a circle or not a square or not closed looped. The engravings 16, 19, 20, 116, 216, 31 start especially at the beginning and end at the end of a row 7.
The distance between two engravings 16, 19, 20, 116, 216, 31 before and after the one row 7 next to each other is
especially 1mm to 2mm.
Furthermore the engravings can also arranged only in the TBC 25. In Figure 2 it can be seen that the engravings 16, 19 have a depth until the substrate 22. But nevertheless the surface of the substrate 22 can
coated with a metallic bond coat like a NiCoCrAl plus optional additives (Y, Re, Si, Ta, ...) .
Figures 3, 4 show a curved form of the engravings 20, 116, 216, 31, wherein the distance of opposite curved engraving 116, 20; 216, 31 is smaller between two cooling holes 10', 10'' and which are not straight (Fig. 4), but multiple curved or a combination of it (Fig. 3) .
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