[0001] The invention relates to a ceramic layer system which has an outer ceramic thermal
barrier coating with vertical cracks and an underlying high porous ceramic sublayer.
[0002] Components for the use at high temperatures are coated with metallic coatings in
order to protect them against oxidation and corrosion.
[0003] The protection against the heat is performed by ceramic coatings, which are based
mostly on zirconia.
[0004] Field feedback has shown that the current thermal barrier coatings (TBC) suffer from
low erosion resistance. Turbine blades of stage 1 with high porosity coatings containing
a large number of unmolten or semimolten particles have shown low erosion resistance.
At certain gas turbine types and in specific turbine parts locations, such as the
sections surrounding the leading edge, bond coat has evidently been exposed in early
intervals due to the severe erosion rate of the TBC.
[0005] The development during the last years has pushed thermal spray coatings porosity
upwards. However, that has caused the shrinkage of the sprayability window that allows
coatings to receive both high porosity and good cohesion. In the continuous effort
to increase porosity, coating's cohesion can be neglected and as a result, erosion
has started manifesting itself as a major issue for coatings in specific parts and
engines.
[0006] Nevertheless, due to the constantly increasing temperatures these turbine parts are
exposed to, it is of imperative importance that the ceramic layer must demonstrate
increased erosion resistance.
[0007] It is therefore the aim of the invention to reveal a ceramic layer system which overcomes
the problems given above.
[0008] The problem is solved by a ceramic layer system according to claim 1.
[0009] The problems are preferably addressed by adopting a denser ceramic outer coating.
Preferably this coating will be deposited as a segmented TBC to demonstrate compliance
and strain tolerance. Additionally segmented TBCs have shown significantly lower erosion
rates compared to their porous counterparts. That means for the same chemistry a porous
coating will show more than 3x the erosion rate compared to the segmented's one.
[0010] In the subclaims further advantages are listed, which can be arbitrary combined with
each other to yield further advantages.
[0011] The figure shows an example of the invention.
[0012] The description and the figure show only examples of the invention.
[0013] The novelty lies on the usage of DVC microstructure on top of a porous coating. The
system comprises of a porous, especially partially stabilized zirconia as the low
conductivity lower, especially thicker layer and a high toughness DVC upper, especially
thin layer of especially partially stabilized zirconia (especially 8YSZ) to provide
the high temperature capability.
[0014] The thickness of the upper DVC layer is preferably between 50µm - 250µm.
[0015] Unlike other possible bilayer coating approaches, the same chemistry between the
two coatings can enhance their bonding. Appropriate preheating of the already deposited
porous PSZ will prepare its surface to receive the fully molten particles for the
DVC and due to the high local temperatures attained during spraying will allow better
diffusion between the two similar materials. To reduce the cost ideally the two coatings
can be obtained by using the same high power torch and by appropriate tailoring of
the powder particle size and spraying parameters.
[0016] The advantages that arise are:
1) The erosion resistance of the coating system will be improved significantly. The
dense upper coating is expected to drastically reduce the amount of material loss
due to erosion and help preserve the porous ceramic sublayer 10.
[0017] The new coating system comprises segmented partially stabilized zirconia on porous
partially stabilized zirconia (PSZ). The segmented coating is thinner than the porous.
The porous can be HHP or coating of other similar or higher porosity for increased
thermal protection. The bond coat can be a thermally sprayed typical MNiCoCrAlY.
[0018] The figure shows a metallic substrate 4 which is especially made of a nickel- or
cobalt based superalloy.
[0019] On the surface of the substrate 4 there is a metallic bond coat 7, which is preferably
made of a NiCoCrAlY alloy.
[0020] On this metallic bond coat 7, there is a thermal grown oxide layer (TGO), which is
build up during further application of a ceramic layer or by oxidation or during use
of the component.
[0021] The thermal grown oxide (TGO) is not further shown.
[0022] The ceramic layer is especially a bilayer and comprises a underlying porous ceramic
sublayer 10.
[0023] The porous ceramic sublayer 10 has a high porosity and is thicker, that means at
least 20% thicker than the outer ceramic layer 13.
[0024] The porosity of the porous ceramic sublayer 10 is mostly caused by pores. The porosity
of the porous ceramic sublayer is between 8% - 20%.
[0025] The porous ceramic sublayer preferably has a thickness from 50µm to 500µm.
[0026] The porous ceramic sublayer 10 has a much higher porosity than the outermost ceramic
sublayer 13, especially higher than 50% (relative), very especially higher than 70%
(relative) of the outer ceramic outermost layer and shows vertical cracks 16.
[0027] The porosity of the outer ceramic layer 13 is especially lower than 6%, especially
lower than 5%, wherein the outer ceramic layer is especially the outermost layer.
[0028] The vertical cracks 16 in the outermost ceramic layer (13) are mostly and especially
at least 90% only in the outermost layer 13.
[0029] The outermost layer 13 has a thickness of 5µm to 250µm.
[0030] The ceramic for the porous ceramic sublayer 10 and the outer layer 13 is preferably
zirconia (ZrO
2), which are both preferably stabilized by Yttria (Y
2O
3).
1. Ceramic layer system (1),
at least comprising:
a metallic substrate (4),
especially made of a nickel- or cobalt based superalloy,
a metallic bond coat (7),
especially made of an NiCoCrAlY alloy,
wherein a porous ceramic sublayer (10) is present on the metallic bond coat (7) and
an outer ceramic layer (13),
especially outermost ceramic layer (13),
on the porous ceramic sublayer (10),
wherein the outermost ceramic layer (13) has vertical cracks (16).
2. Layer system according to claim 1,
wherein the porous ceramic sublayer (10) is at least 20% thicker than the outermost
ceramic layer (13).
3. Layer system according to one of the claims 1 or 2,
wherein the porosity of the porous ceramic sublayer (10) is at least 50%, especially
at least 70% higher than the porosity of the outer ceramic layer (13).
4. Layer system according to any of the claims 1, 2 or 3,
wherein the material of the porous ceramic sublayer (10) and the outer layer (13)
is made of zirconia,
especially stabilized by yttria (Y2O3),
especially partially stabilized zirconia (ZrO2).
5. Layer system according to any of the claims 1, 2, 3 or 4,
wherein the outer ceramic layer (13) has a thickness of 50µm to 250µm.
6. Layer system according to any of the claims 1, 2, 3, 4 or 5,
wherein the porosity of the porous ceramic sublayer (10) is mostly caused by pores.
7. Layer system according to any of the claims 1, 2, 3, 4, 5 or 6,
wherein the porosity of the porous ceramic sublayer (10) is between 8% and 20%,
especially 10% to 20%.
8. Layer system according to any of the claims 1, 2, 3, 4, 5, 6 or 7,
wherein the outer ceramic (13) layer has a porosity lower than 6%,
especially lower than 5%.
9. Layer system according to any of the claims 1, 2, 3, 4, 5, 6, 7 or 8,
wherein the ceramic of the layer system (1) consists of an oxide layer of the metallic
bond coat (7), the porous ceramic sublayer (10) and the outer layer (13).
10. Layer system according to any of the claims 1, 2, 3, 4, 5, 6, 7, 8 or 9,
wherein the thickness of the porous ceramic sublayer (10) is at least 100µm, especially
at least 300µm.