FULLY STABILIZED ZIRCONIA IN A SEAL SYSTEM

Abstract

A seal system for gas turbine that includes a stator and a blade with a blade tip facing the stator. The blade has a protective ceramic coating having an inner ceramic layer being made of a partially stabilized zirconia and having at least a partially segmented microstructure in form of vertical cracks. The ceramic coating further includes an outer ceramic layer made of fully stabilized zirconia and having a segmented microstructure. Advantageously, the entire airfoil surface is provided with the protective ceramic coating. With the fully stabilized zirconia coating on the tip of a blade which faces a casing with a ceramic coating, a result is a better sealing system. The stator includes an abradable coating having at least an outer ceramic coating being made of fully stabilized or ytterbium stabilized zirconia.

Claims

1. A seal system, comprising: a stator or a casing, and a blade, wherein the stator has a first ceramic coating, which faces a tip of the blade, wherein the first ceramic coating comprises: a first inner ceramic coating made of Partially Stabilized Zirconia (PSZ); and a first outer ceramic coating made of Fully Stabilized Zirconia (FSZ) or Ytterbia stabilized Zirconia (YBZO), wherein the blade, which faces the stator or the casing or the first ceramic coating of the casing, has on the tip of the blade a second ceramic coating comprising: a second inner ceramic coating with a partially segmented microstructure and a minimum thickness of 125 μm made of PSZ, and a second outer ceramic coating with a segmented microstructure made of FSZ.

2. The seal system according to claim 1, wherein a ceramic airfoil coating is present on an airfoil of the blade, which comprises an inner ceramic airfoil coating made of PSZ and an outer ceramic airfoil coating made of FSZ is on the airfoil on the blade.

3. The seal system according to claim 1, wherein the second ceramic coating consists of a segmented microstructure.

4. The seal system according to claim 2, wherein the ceramic airfoil coating consists of a segmented microstructure.

5. The seal system according to claim 1, wherein the first inner ceramic coating does not consist of a segmented microstructure.

6. The seal system according to claim 1, wherein the first inner ceramic coating made of PSZ has a porosity of at least 15% and maximum 35%.

7. The seal system according to claim 1, wherein the first outer ceramic coating made of FSZ or YBZO has a porosity of 25% to 40%.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0013] The figure shows an arrangement of a seal system 1.

DETAILED DESCRIPTION OF INVENTION

[0014] The figure and the description show only one or several examples of the invention.

[0015] The seal system 1 comprises a casing 4 or a stator 4.

[0016] The stator 4 or the casing 4 has advantageously a substrate 10, which is especially metallic, on which advantageously first inner ceramic coating 16 is applied on. Preferably this first inner ceramic coating 16 is a porous PSZ (partially stabilized zirconia) coating with preferable a porosity of at least 15% and maximum 35%.

[0017] On top of the first inner ceramic coating 16 a first outer ceramic coating 17 is applied, which can be YBZO (Yb.sub.2O.sub.3 stabilized Zirconia) or a fully stabilized Zirconia (FSZ), both having a porosity advantageously between 25%-40%.

[0018] Both form the first ceramic coating 15.

[0019] 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 microstructure and is advantageously at least 125 μm thick.

[0020] On top of this PSZ coating 19, a second outer ceramic coating 20 is applied, which is segmented and similarly of the segmented microstructure and of Fully Stabilized Zirconia (FSZ) chemistry.

[0021] Both form the second ceramic coating 21.

[0022] 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.

[0023] 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 especially metallic coat (NiCoCrAlY, . . . ) between the substrates 10, 13 and the ceramic coatings 16, 19, 22 which are not shown here.

[0024] The blade 3 has on its airfoil 14 also a ceramic airfoil coating 24.

[0025] 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 outer ceramic airfoil coating 23.

[0026] But it can also be different in the microstructure but advantageously not in the composition.