The invention relates to a fully stabilized Zirconia based on a tip on a plate which acts as abradable in a seal system.

The currently used abradable coatings in the turbine sections are high porosity ceramics (over 25%) . Specifically, typical abradable coatings used currently in the modern Large Gas Turbines (LGTs) are the YBZO (Ytterbia stabilized Zirconia) coatings. A polyester as a fugitive is sprayed along with the ceramic powder in order to increase the overall porosity of the coating. High porosity is the most important element of an abradable since it can allow good abradability during the rubbing of the blade tip on it. At the new LGTs, the Turbine Inlet Temperature (TIT) is estimated to be over 1873K. At these temperatures the TBC is considered prime reliant. That means that it is an irreplaceable component of the part. If the ceramic coating is lost, then the exposure of the under neath metal in these temperatures will lead to its quick deg radation and the part will have to be exchanged.

In a similar manner, if the blade tips of first row or second row are not coated with TBC, then they will be quickly dete riorated, signifying the importance of a TBC coating on the tip. The TBC coating on the tip should be thick enough in or der to protect the underlying metal and should be tough enough not be rubbed away during its contact with the abrada ble coating on the Ring Segments.

Up to date the typical TBC tip coating used is the YSZ (Yt- tria Stabilized Zirconia) , but this coating lacks the proper ties to survive higher temperatures. New chemistries of TBCs have been developed to address the higher temperatures seen in the latest generations of IGTs. The new chemistries, known as Fully Stabilized Zirconia (FSZ) coatings, combine higher chemical phase stability and better sintering resistance com pared to the standard 8YSZ coating. The adversity of the new chemistries is that however they present also much lower toughness. That means that they can be relatively easily rubbed away against a counterbody such as an abradable coat ing .

It is therefore aim of the invention to overcome the problems mentioned above.

The problem is solved by a seal system according to claim 1.

Further advantages are listed in the dependent claims which can be combined arbitrarily with each other to yield further advantages .

What is suggested is to deposit a FSZ with a microstructure that will maximize its toughness. This microstructure is seg mented. The coating is deposited so dense that vertical cracks are formed in it. It is well documented that the seg mented microstructure combines good thermal strain capability along with significantly improved toughness and erosion re sistance compared to porous coatings of the same chemistry.

It has been shown that the toughness of the segmented micro structure of a FSZ coating is more than 3X higher compared to the toughness of a 15% porous FSZ.

The novelty of the present invention lies on making possible to use a FSZ coating on the tip of the blades as an abrasive coating. The significantly improved toughness of the segment ed FSZ will ensure that the abradable will be rubbed away and not the opposite.

The advantages of the present invention are:

A high temperature stable coating, with an inherited low toughness, can be deposited with a microstructure that can increase significantly its toughness and its rubbing capabil ity.

The figure shows an arrangement of a seal system 1. The figure and the description show only one or several exam ples of the invention.

The seal system 1 comprises a casing 4 or a stator 4.

The stator 4 or the casing 4 has preferably a substrate 10, which is especially metallic, on which preferably first inner ceramic coating 16 is applied on. Preferably this first inner ceramic coating 16 is a porous PSZ (partially stabilized zir- conia) coating with preferable a porosity of at least 15% and maximum 35%.

On top of the first inner ceramic coating 16 a first outer ceramic coating 17 is applied, which can be YBZO (Yb203 sta bilized Zirconia) or a fully stabilized Zirconia (FSZ), both having a porosity preferably between 25% - 40%.

Both form the first ceramic coating 15.

The other part of the seal system 1 is a blade 3, wherein here only the tip 25 is shown. The blade 3 has on the tip 25 second inner ceramic coating 19 which comprises a Partially Stabilized Zirconia (PSZ) coating of a segmented microstruc ture and is preferably at least 125pm thick.

On top of this PSZ coating 19, a second outer ceramic coating 20 is applied, which is segmented and similarly of the seg mented microstructure and of Fully Stabilized Zirconia (FSZ) chemistry .

Both form the second ceramic coating 21.

The blade 3 comprises especially a metallic substrate 13 which is especially a nickel or cobalt based superalloy, but which can also be any CMC or any ceramic material.

For all coatings 15, 21, 24 on the substrate 10, 13 of the casing or on the blade 3 there can be any bond coat especial ly metallic coat (NiCoCrAlY, ...) between the substrates 10, 13 and the ceramic coatings 16, 19, 22 which are not shown here. The blade 3 has on its airfoil 14 also a ceramic airfoil coating 24.

This ceramic airfoil coating 24; 22, 23 on the airfoil 14 can have ideally the same composition and micro structure as the ceramic coating on the tip 25, meaning a segmented FSZ on top of a PSZ with an inner ceramic airfoil coating 22 and an out er ceramic airfoil coating 23.

But it can also be different in the microstructure but pref- erably not in the composition.