RUMPLING PROTECTION · Development of thin ceramic coatings for the protection against temperature and stress induced rumpling of the metal surface of turbine blades
FP6 — Marie Curie Actions (Human Resources and Mobility)
- Duration
- 2005-11-01 → 2007-10-31
- EU contribution
- €196,752
- Participants
- 1
- Scheme
- EIF
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Results in brief
Final Activity Report Summary - RUMPLING PROTECTION (Development of thin ceramic coatings for the protection against temperature and stress induced rumpling of the metal surface of turbine blades)
Surfaces of turbine blades may suffer under rumpling due to the high temperatures and mechanical loads. The objective of the project was to prepare ceramic protective coatings for turbine blades in gas turbines for protection against this surface rumpling. Electrophoretic deposition (EPD) allowed for the fabrication of ceramic coatings at lower cost and higher speed than most other deposition techniques. The processing consisted of powder deposition from a suspension under the influence of an electric field and subsequent consolidation of the coating by sintering. The basis of the powder was zirconia with 5 wt % yttria. Two different types of suspensions with zirconia powder were investigated, namely methyl-ethyl-ketone and ethanol based suspensions. Methyl-ethyl-ketone gave a very stable suspension, but was not environmentally harmless. Ethanol was favoured as suspension, because it was both environmentally friendly and cheaper. The standard sintering temperature was 1 200 degrees Celsius, which could easily damage or change the substrate and also meant high production costs. In order to reduce the sintering temperature, suspensions with the addition of ZrN were investigated. Due to reaction bonding, the heat treatment of coatings from this mixture in air at a remarkable low temperature of 1 000 degrees Celsius resulted in a consolidated coating. Adherent coatings with coating thicknesses up to 0.1 mm with a high porosity were obtained. The ceramic surfaces were smooth and the microstructure was homogeneous. The elastic modulus of the EPD coatings was derived from impulse excitation experiments and the thermal conductivity from laser flash analysis. The elastic modulus was about 22 GPa and the thermal conductivity between 0.4 and 0.6 W/mK at room temperature, both decreasing slightly with temperature. Heat treatment in air at 1 100 degrees Celsius for 100 h significantly increased the thermal conductivity, however compared with commercially available coatings the EPD coatings had much lower thermal conductivities. The exceptionally low thermal conductivity made EPD coatings a promising candidate for thermal barrier coatings. The temperature conditions in turbines were simulated by exposing the specimens to temperature cycles between room temperature and 1 100 degrees Celsius. It was observed that for a limited number of cycles (between 25 and 50, depending on the type of suspension) the ceramic coatings successfully suppressed rumpling. For higher cycle numbers however the rumpling force seemed to be too strong and rumpling related spallation was observed. Within the project, successful EPD ceramic coatings with low elastic modulus, very low thermal conductivity and rumpling protection capabilities were prepared. Nevertheless, for long term applications the adherence should be improved.
Data: CORDIS, © European Union
Project objective
The aim of this project is to improve the performance and lifetime of blades used in gas turbines for aeronautics and energy production. Turbine blades commonly have a metallic oxidation protection coating, which experiences in service severe surface rumpling. Surface rumpling is detrimental, since it decreases the aerodynamic efficiency and the life of turbines. Until now, no solution for rumpling protection is found. A new idea to suppress surface rumpling, for which the proposer is co-applicant of a paten t, is to apply additionally a thin ceramic coating on top.The application of ceramic coatings on metal can be achieved by different methods, which usually are very expensive. An inexpensive method, however, is given by electrophoresis. The host institute KU Leuven has shown this already with success for steel, but not yet for turbine relevant metal systems. Due to the different physical and chemical properties of these metal systems compared with steel, further investigations are necessary to apply this in expensive method for turbine blades.The intention of this project is therefore to utilize electrophoresis for a system, which consists of a substrate and an oxidation protection coating as commonly used for turbine blades. An appropriate ceramic coating and processing procedure has to be developed, which lead to a thin ceramic coating with good adherence. The adherence will be qualified under thermal cycling and the ability of rumpling protection will be tested under multi-axial mechanical and thermal loading.The application of inexpensive and effective rumpling protection coatings will benefit turbine operators greatly. It is estimated, that it has the potential to reduce costs for aeronautics and energy production worldwide by approximately 750 million/per year. Additionally, rumpling prevention will increase the efficiency of turbines, and therefore decrease energy consumption and air pollution significantly.
Original text from CORDIS.
Participants
- KATHOLIEKE UNIVERSITEIT LEUVEN · LEUVENCoordinatorBelgium
Links
Data: CORDIS, © European Union
