LONG, CONTINUOUS ENGRAVING ALONG A ROW OF COOLING HOLES
20170314399 · 2017-11-02
Assignee
Inventors
Cpc classification
F05D2300/175
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2300/20
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
C23C28/00
CHEMISTRY; METALLURGY
F05D2300/611
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D5/288
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2260/202
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D5/186
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
C23C28/3455
CHEMISTRY; METALLURGY
C23C28/30
CHEMISTRY; METALLURGY
F05D2230/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F01D5/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D5/28
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D9/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
By continuously long engravings, the spallation behavior of the thermal barrier coating is reduced and the lifetime of the TBC is prolonged.
Claims
1. A component comprising: a substrate, a ceramic thermal barrier coating on the substrate; at least one row of cooling holes along a direction in the substrate and in the ceramic thermal barrier coating, wherein the ceramic thermal barrier coating has at least one engraving, wherein the at least one engraving is a long continuous engraving along the direction before and/or after of the at least one row.
2. The component according to claim 1, wherein the at least one engraving is straight.
3. The component according to claim 1, wherein the at least one engraving includes multiple curves.
4. The component according to claim 1, wherein the at least one engraving is long and continuous and which is not connecting with each other or endless.
5. The component according to claim 1, wherein the at least one engraving is arranged in the thermal barrier coating.
6. The component according to claim 1, wherein the at least one engraving is only arranged before and after one row.
7. The component according to claim 1, wherein the substrate has a metallic overlay coating.
8. The component according claim 7, wherein the at least one engraving has a depth that reaches an outer surface of a metallic coating on the substrate.
9. The component according to claim 1, wherein the at least one engraving is only arranged in the ceramic thermal barrier coating and does not reach the substrate or a metallic coating.
10. The component to claim 1, wherein the at least one engraving starts at a beginning and an end at an end of a row.
11. The component to claim 1, wherein both engravings have a distance to each other along an overflow direction of 1 mm to 2 mm.
12. The component to claim 11, wherein the distance of a curved engraving to a straight engraving or to a curved engraving is smaller between two cooling holes of these two engravings.
13. The component according to claim 1, wherein the substrate is a nickel- or cobalt-based super alloy.
Description
BRIEF DESCRIPTION
[0009] Some of the embodiments will be described in detail, with reference to the following figures, wherein like designations denote like members, wherein:
[0010]
[0011]
[0012]
[0013]
DETAILED DESCRIPTION
[0014] By an implementation of a polymer masking it is possible to introduce the suggested design in
[0015] This manufacturing procedure has following advantage:
[0016] The engraving will not reduce the bond coat thickness as during a laser engraving
[0017] This step can be carried out during the coating
[0018] In case of casting and coating deviations, the polymer masking will not affect the bond coat thickness.
[0019] The width of such a ceramic free region could vary between 1 and 2 mm.
[0020] The positive effect of the engraving is the spallation behavior. In case of spallation the spalled region will not be extended on wide regions.
[0021] 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.
[0022] The following positive effects are related to the engraving:
[0023] Retrofitable with current designs
[0024] In case of spallation, only restricted region will be affected
[0025] Lower operation risk
[0026] Reduced rework after laser drilling
[0027] Applicable to all spallation threatened cooling holes rows
[0028] Applicable to vanes and blades.
[0029]
[0030] 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.
[0031] These engravings 16, 19 are continuous, especially straight engravings in the TBC 25.
[0032] The engravings 16, 19, 20, 116, 216, 31 (
[0033] The engravings 16, 19, 20, 116, 216, 31 start especially at the beginning and end at the end of a row 7.
[0034] The distance between two engravings 16, 19, 20, 116, 216, 31 before and after the one row 7 next to each other is especially 1 mm to 2 mm.
[0035] Furthermore the engravings can also arranged only in the TBC 25.
[0036] In
[0037] But nevertheless the surface of the substrate 22 can be coated with a metallic bond coat like a NiCoCrAl plus optional additives (Y, Re, Si, Ta, . . . ).
[0038]
[0039] Although the present invention has been disclosed in the form of preferred embodiments and variations thereon, it will be understood that numerous additional modifications and variations could be made thereto without departing from the scope of the invention.
[0040] For the sake of clarity, it is to be understood that the use of “a” or “an” throughout this application does not exclude a plurality, and “comprising” does not exclude other steps or elements.