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Sulfidation behavior of a non harmful water based Al and AlSi slurry ti CM247 ll coating on CM247 superalloy X. Montero, M.C. Galetz, M. Schütze email: [email protected] Funded by: EU Period: 01.10.200801.10.2012 The overall objective of the PARTICOAT project is to develop a novel, nonconventional and cost efficient multipurpose high temperature coating system with the potential to serve as Introduction Spherical Al particles and AlSi alloy particles were deposited by air brush on CM 247 alloy and heat treated in air at 1000°C during 2 hours. These coatings were exposed to air and to synthetic air + 1.5 % SO 2 at 1000°C . Oxide formation and the microstructure of the coating were studied using thermo gravimetric analysis, Xray diffraction, light microscopy, scanning electron microscopy (SEM) combined with energy dispersive Xray spectroscopy and electron probe micro analysis (EPMA). A statistical evaluation of the corrosion data was performed to determine the cumulative distribution of corrosion depth and the remaining undamaged coating. The cumulative distribution was obtained by determining the thermal barrier produced in one manufacturing step. Aluminium does not form metastable oxides in a particle size window of 2 to 20 μm, but hollow spheres consisting of Al 2 O 3 . These observations led to the idea of depositing such Al particles on an alloy substrate using a non harmful water based slurry and convert them into a coating by heat treatment. The result is a coating structure consisting of a ceramic quasifoam top coat comprising spherical hollow alumina particles and an Al rich intermetallic diffusion layer below, which has the potential to serve as a bond coat and to form a protective alumina scale. The presented case is oriented to evaluate the oxidation and sulfidation resistance of a nickel base superalloy coated by Al or AlSi particles containing slurries. Experimental procedure performed to determine the cumulative distribution of corrosion depth and the remaining un damaged coating. The cumulative distribution was obtained by determining the number of spots with values above a given corrosion depth. The weight gain evolution is shown in fig. 1. The highest weight gains are observed for the exposure in SO 2 containing atmosphere. The Al slurry based coating showed slightly lower weight gains than the AlSi slurry based on data after 1000 hours of exposure in both atmospheres. Results AlSi slurry Al slurry Synthetic air + SO 2 The coating damage diagram, which represents the relative diffusion layer which has been affected by sulfidation, is shown in fig. 4. After 500 hours of exposure under SO 2 containing atmosphere the damaged coating diffusion zone is slightly higher (around 25%) for the Al than for the AlSi slurry coating. After 1000 hours of exposure these values increased for both coatings (ranging around 45%), but interestingly the damage values are inverted, the AlSi slurry based coating being more prone to attack. A similar inversion has also been observed in the initial stages of weight gain evolution (see fig. 1). Fig. 1: Mass gain evolution of the coated alloys at 1000 C in air and synthetic air + 1.5% SO 2 Air The cross section of Al Si slurry coated CM 247 after 500 hours of exposure in air at The SEM crosssection of the Al slurry coated CM 247 after 500 hours in SO 2 containing atmosphere (fig. 3b) reveals a typical type I hot corrosion attack related to Fig. 2: SEM crosssection AlSi slurry coated CM247 after 500h exposure at 1000 C in air Si O NiAl Al Ni The crosssection of AlSi slurry coated CM 247 after 500 hours of exposure in air at 1000ºC (fig.2) shows that Si is mainly localized in the diffusion layer close to the top coat interface. Fig. 4: Quantification of the damaged diffusion layer after image analysis of SEM crosssections of CM 247 slurry coated samples exposed at 1000 C in SO 2 containing synthetic air. The corrosion depth is higher after 500 hours for the Al slurry coated sample as for the AlSi coated one (fig. 5); however, the damage seems to be more homogeneous for the Al slurry coated sample. This information confirms the beneficial effect of a silicon rich diffusion layer at least during the first 500 hours of exposure. After 1000 hours of exposure, the corrosion depth increases for both coatings, showing higher depths for the case of the Al Si slurry coating which demonstrates a time limitation for the sulfidation/oxidation in the diffusion layer (indicated by arrow). The element mapping for the sulfidizing atmosphere (fig. 3c) reveals accelerated oxide formation and sulfur presence. the case of the AlSi slurry coating, which demonstrates a time limitation for the improvement by silicon in the modified aluminide coating. In other words, silicon in the diffusion layer has been beneficial until its entire transformation into corrosion product. a c Wh d t lfidi i / idi i t h th tifi ti f th d d ti h th t Si difi d ti bh b tt th th i l l i id l Summary and perspective Fig 3: SEM crosssection of Al slurry coated CM 247 exposed at 1000 C in air (a) and SO 2 containing atmosphere (b) and EPMA mapping of the later (c). Fig. 5: Cumulative probability graphs of CM 247 slurry coated samples exposed at 1000 C in SO 2 containing synthetic air. b The authors would like to thank G. Schmidt for the EPMA analysis, D. Hasenpflug, S. Gansler and E. BerghofHasselbächer for helping with the metallographic preparation. This work is supported by the European 7th Framework Program (project CPIP 2113292). When exposed to sulfidizing/oxidizing atmosphere, the quantification of the damaged coating shows that Si modified coatings behave better than thesimplealuminideslurry coatings as long as the silicon is maintained in the coating (the first 500 hours). Exposure of the coatings has demonstrated the possibility of forming an oxidation and sulfidation resistant thermal barrier coating system produced in air in a single step by the slurry route which offers unique advantages that can be very favourable especially as a repairing technique . Acknowledgements

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  • Sulfidation behavior of a non harmful water based Al and Al‐Si slurry ti CM247 llcoating on CM247 superalloyX. Montero, M.C. Galetz, M. Schütze

    e‐mail: [email protected] by: EU

    Period: 01.10.2008‐01.10.2012

    The overall objective of the PARTICOAT project is to develop a novel, non‐conventional and cost efficient multipurpose high temperature coating system with the potential to serve asIntroduction

    Spherical Al particles and Al‐Si alloy particles were deposited by air brush on CM 247 alloy and heat treated in air at 1000°C during 2 hours. These coatings were exposed to air andto synthetic air + 1.5 % SO2 at 1000°C . Oxide formation and the microstructure of the coating were studied using thermo gravimetric analysis, X‐ray diffraction, light microscopy,scanning electron microscopy (SEM) combined with energy dispersive X‐ray spectroscopy and electron probe micro analysis (EPMA). A statistical evaluation of the corrosion data wasperformed to determine the cumulative distribution of corrosion depth and the remaining un‐damaged coating. The cumulative distribution was obtained by determining the

    thermal barrier produced in one manufacturing step. Aluminium does not form meta‐stable oxides in a particle size window of 2 to 20 µm, but hollow spheres consisting of ‐Al2O3.These observations led to the idea of depositing such Al particles on an alloy substrate using a non harmful water based slurry and convert them into a coating by heat treatment.The result is a coating structure consisting of a ceramic quasi‐foam top coat comprising spherical hollow alumina particles and an Al rich intermetallic diffusion layer below, which hasthe potential to serve as a bond coat and to form a protective alumina scale. The presented case is oriented to evaluate the oxidation and sulfidation resistance of a nickel basesuperalloy coated by Al or Al‐Si particles containing slurries.

    Experimental procedure

    performed to determine the cumulative distribution of corrosion depth and the remaining un damaged coating. The cumulative distribution was obtained by determining thenumber of spots with values above a given corrosion depth.

    The weight gain evolution is shown in fig. 1. The highest weight gains are observed forthe exposure in SO2 containing atmosphere. The Al slurry based coating showed slightlylower weight gains than the Al‐Si slurry based on data after 1000 hours of exposure inboth atmospheres.

    Results

    Al‐Si  slurry

    Al slurry Synthetic air + SO2

    The coating damage diagram, which represents the relative diffusion layer which hasbeen affected by sulfidation, is shown in fig. 4. After 500 hours of exposure under SO2containing atmosphere the damaged coating diffusion zone is slightly higher (around25%) for the Al than for the Al‐Si slurry coating. After 1000 hours of exposure thesevalues increased for both coatings (ranging around 45%), but interestingly the damagevalues are inverted, the Al‐Si slurry based coating being more prone to attack. A similarinversion has also been observed in the initial stages of weight gain evolution (see fig. 1).

    Fig. 1: Mass gain evolution of the coated alloys at 1000 C in air and synthetic air + 1.5% SO2

    Air

    The cross section of Al Si slurry coated CM 247 after 500 hours of exposure in air at

    The SEM cross‐section of the Al slurry coated CM 247 after 500 hours in SO2 containingatmosphere (fig. 3b) reveals a typical type I hot corrosion attack related to

    Fig. 2: SEM cross‐section Al‐Si slurry coated CM247 after 500h exposure at 1000 C in air

    Si ONiAl Al Ni

    The cross‐section of Al‐Si slurry coated CM 247 after 500 hours of exposure in air at1000ºC (fig.2) shows that Si is mainly localized in the diffusion layer close to the topcoat interface. Fig. 4: Quantification of the damaged diffusion layer after image analysis of SEM cross‐

    sections of CM 247 slurry coated samples exposed at 1000 C in SO2 containing synthetic air.

    The corrosion depth is higher after 500 hours for the Al slurry coated sample as for theAl‐Si coated one (fig. 5); however, the damage seems to be more homogeneous for theAl slurry coated sample. This information confirms the beneficial effect of a silicon richdiffusion layer at least during the first 500 hours of exposure. After 1000 hours ofexposure, the corrosion depth increases for both coatings, showing higher depths forthe case of the Al Si slurry coating which demonstrates a time limitation for thep ( g ) yp yp

    sulfidation/oxidation in the diffusion layer (indicated by arrow). The element mappingfor the sulfidizing atmosphere (fig. 3c) reveals accelerated oxide formation and sulfurpresence.

    the case of the Al‐Si slurry coating, which demonstrates a time limitation for theimprovement by silicon in the modified aluminide coating. In other words, silicon in thediffusion layer has been beneficial until its entire transformation into corrosion product.

    a

    c

    Wh d t lfidi i / idi i t h th tifi ti f th d d ti h th t Si difi d ti b h b tt th th i l l i id l

    Summary and perspective

    Fig 3: SEM cross‐section of Al slurry coated CM 247 exposed at 1000 C in air (a) and SO2containing atmosphere (b) and EPMA mapping of the later (c).

    Fig. 5: Cumulative probability graphs of CM 247 slurry coated samples exposed at 1000 C inSO2 containing synthetic air.

    b

    The authors would like to thank G. Schmidt for the EPMA analysis, D. Hasenpflug, S. Gansler and E. Berghof‐Hasselbächer for helping with the metallographic preparation. This workis supported by the European 7th Framework Program (project CP‐IP 211329‐2).

    When exposed to sulfidizing/oxidizing atmosphere, the quantification of the damaged coating shows that Si modified coatings behave better than the simple aluminide slurrycoatings as long as the silicon is maintained in the coating (the first 500 hours). Exposure of the coatings has demonstrated the possibility of forming an oxidation and sulfidationresistant thermal barrier coating system produced in air in a single step by the slurry route which offers unique advantages that can be very favourable especially as a repairingtechnique .

    Acknowledgements