Preparation of Zirconium Phosphate Bonded Silicon Nitride Ceramic Coatings by Cold Spray and Presureless Sintering

2014 ◽  
Vol 616 ◽  
pp. 47-51
Author(s):  
Fei Chen ◽  
Fei Yu Li ◽  
Qiang Shen ◽  
Lian Meng Zhang

In the present study, a new method for preparing zirconium phosphate bonded silicon nitride (Si3N4) ceramic coatings with low porosity was developed using cold spray and pressureless sintering technique. Zirconium phosphate (ZrP2O7) was used as a binder material instead of the traditional organic materials, in order to prevent the residual carbon which was severe to the dielectric properties of the Si3N4ceramics. Firstly, aqueous Si3N4slurries with 0~40 wt.% solid loading were prepared, using deionized water as the liquid medium. Then the Si3N4slurries were cold sprayed on the Si3N4porous ceramic substrates and finally the samples were presurelessly sintered at 1000oC to achieve the Si3N4ceramic coatings. The rheological properties and viscosity of Si3N4slurries were investigated in detail, as a function of solid loading. The optimum cold spray parameters were spray distance 21 cm and spray time 20 s. The porosity of the obtained Si3N4ceramic coating was ~5 % and the interface between the coating and substrate was well bonded, without microcracks, indicating a good thermal physical match between the coating and substrate.

1999 ◽  
Vol 556 ◽  
Author(s):  
K. R. Wilfinger ◽  
J. C. Farmer ◽  
R. W. Hopper ◽  
T. E. Shell

AbstractCeramic coated carbon steel coupons were corrosion tested in water with dissolved salts to simulate exposure to evaporation concentrated groundwater in an underground nuclear repository. Metallography revealed no corrosion at the ceramic metal interface of dense coatings, even though electrical measurements demonstrated that the coatings were slightly porous. Experimental results and a model to predict corrosion rates influenced by a porous ceramic coating and coating lifetimes are presented.


2014 ◽  
Vol 627 ◽  
pp. 293-296
Author(s):  
Masayuki Arai ◽  
T. Hayashi ◽  
T. Suidzu

A transpiration cooling system for gas turbine applications has significant benefit to reduce the amount of cooling air and to increase cooling efficiency. We had developed a porous ceramic coating deposited by plasma spraying process, which can infiltrate cooling gas, and examined about those mechanical properties. In this study, thermal cycling life of this porous ceramic coating is revealed in order to apply this technology to advanced gas turbine blade in practical use. The thermal cycling test is conducted by using the hand-made device which can heat cyclically up and down around the surface of the porous coating while infiltrating cooling gas. The number of thermal cycles up to reach the coating delamination is related with maximum exposed temperature and pressure of the cooling gas as the test condition, consequently.


2012 ◽  
Vol 508 ◽  
pp. 21-26 ◽  
Author(s):  
Jun Yan Wu ◽  
Fei Chen ◽  
Ming Zhong Li ◽  
Qiang Shen ◽  
Lian Meng Zhang

In this Paper, Five Fundamental Effective Thermal Conductivity Structural Models (Series, Parallel, Two Forms of Maxwell-Eucken and Effective Medium Theory) Were Used to Analyze and Design Silicon Nitride Porous Ceramics. Then α-Si3N4Matrix Porous Ceramics Were Prepared with ZrP2O7as a Binder and Thermal Conductivity of ZrP2O7Bonded Si3N4Porous Ceramic Was Evaluated. ZrP2O7Bonded Si3N4Porous Ceramic Had Open and Interconnected Pore Structure which is either in EMT or in Maxwell-Euken 2. The Thermal Conductivity of ZrP2O7Bonded Si3N4Porous Ceramics Changes from 2.0 to 0.5 W/m•K with Increasing the Porosity from 20% to 51%. The Obtained Results Showed that the External Porosity Material with Maxwell-Euken 2 Structure Had the Lowest Thermal Conductivity in All Porous Materials. The Open and Interconnected Pore Structure of ZrP2O7Bonded Si3N4Porous Ceramics Provided much Lower Thermal Conductivity.


Author(s):  
Ozer Unal

Interest in ceramics as thermal barrier coatings for hot components of turbine engines has increased rapidly over the last decade. The primary reason for this is the significant reduction in heat load and increased chemical inertness against corrosive species with the ceramic coating materials. Among other candidates, partially-stabilized zirconia is the focus of attention mainly because ot its low thermal conductivity and high thermal expansion coefficient.The coatings were made by Garrett Turbine Engine Company. Ni-base super-alloy was used as the substrate and later a bond-coating with high Al activity was formed over it. The ceramic coatings, with a thickness of about 50 μm, were formed by EB-PVD in a high-vacuum chamber by heating the target material (ZrO2-20 w/0 Y2O3) above its evaporation temperaturef >3500 °C) with a high-energy beam and condensing the resulting vapor onto a rotating heated substrate. A heat treatment in an oxidizing environment was performed later on to form a protective oxide layer to improve the adhesion between the ceramic coating and substrate. Bulk samples were studied by utilizing a Scintag diffractometer and a JEOL JXA-840 SEM; examinations of cross-sectional thin-films of the interface region were performed in a Philips CM 30 TEM operating at 300 kV and for chemical analysis a KEVEX X-ray spectrometer (EDS) was used.


Meccanica ◽  
2015 ◽  
Vol 51 (2) ◽  
pp. 415-428 ◽  
Author(s):  
Ruslan Balokhonov ◽  
Aleksandr Zinoviev ◽  
Varvara Romanova ◽  
Olga Zinovieva

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