The Technology of TBC Deposition by EB-PVD Method

Paweł Pędrak; Andrzej Nowotnik; Marek Goral; Krzysztof Kubiak; Marcin Drajewicz; Jan Sieniawski

doi:10.4028/www.scientific.net/SSP.227.377

Paper Titles

The Oxidation Resistance of Nonmodified and Zr-Modified Aluminide Coatings Deposited by the CVD Method
p.361

The Influence of the Chemical Composition of Superalloys on the Oxidation Resistance of Aluminide Coating
p.365

Influence of Deposition Parameters on Structure of TDCs Deposited by PS-PVD Method
p.369

Microstructure of TBC Coatings Deposited by HVAF and PS-PVD Methods
p.373

The Technology of TBC Deposition by EB-PVD Method
p.377

Analysis of Crystallite Size Changes in an Oxide Layer Formed on Steel during Long-Term Operation at an Elevated Temperature
p.381

Influence of Surface Condition on Oxides Layer Morphology on NiCrAlY Coating during Oxidation at Temperature 1000°C and 1100°C
p.385

Studies on the Adhesion of Oxide Layer Formed on Steel Long-Term Operated at an Elevated Temperature
p.389

Comparison of High-Temperature Oxidation Onset Behavior of Sanicro 28 Steel with KCl, NaCl and K₂CO₃
p.393

HomeSolid State PhenomenaSolid State Phenomena Vol. 227The Technology of TBC Deposition by EB-PVD Method

The Technology of TBC Deposition by EB-PVD Method

Abstract:

The role of thermal barrier coatings is to ensure heat resistance of elements in the hot section of turbofan aircraft engines in high temperatures. Stages of the production process are made up of preparing the base material, forming the aluminide interlayer by chemical vapour deposition method and depositing of the ceramic coating. The paper presents results of tests into microstructure of ZrO₂ and Y₂O₃ ceramic coatings formed by EB-PVD method. The microstructure was assessed in several spots of the turbine blade of a high pressure turbofan engine by means of determining the coating thickness as well as height and width of ceramic columns, depending on the forming conditions.

You might also be interested in these eBooks

View Preview

Info:

Periodical:

Solid State Phenomena (Volume 227)

Pages:

377-380

DOI:

https://doi.org/10.4028/www.scientific.net/SSP.227.377

Citation:

Cite this paper

Online since:

January 2015

Authors:

Paweł Pędrak*, Andrzej Nowotnik, Marek Goral, Krzysztof Kubiak, Marcin Drajewicz, Jan Sieniawski

Keywords:

EB-PVD, Microstructure, TBC, Turbine Blades

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

* - Corresponding Author

References

[1] J. Singh et al., Electron beam-physical vapor deposition technology–present and future applications. Publication of Applied Research Laboratory, Pennsylvania State University, University Park, (2000).

Google Scholar

[2] J.A. Haynes, et al. Characterization of commercial EB-PVD TBC systems with CVD (Ni, Pt) Al bond coatings, Surf. Coat. Tech. 146 (2001) 140-146.

DOI: 10.1016/s0257-8972(01)01483-9

Google Scholar

[3] A. Weisenburger, et al., Pulsed electron beam treatment of MCrAlY bondcoats for EB-PVD TBC systems part 1 of 2: Coating production, Surf. Coat. Technol. 202(4) (2007) 704-708.

DOI: 10.1016/j.surfcoat.2007.07.022

Google Scholar

[4] J.E. Schilbe, Substrate alloy element diffusion in thermal barrier coatings. Surf. Coat. Tech. 133 (2000) 35-39.

DOI: 10.1016/s0257-8972(00)00870-7

Google Scholar

[5] H.U. Minghui, et al. TEM study on microstructure of thermally grown oxide in EB-PVD thermal barrier coatings, Surf. Coat. Tech. 200(20) (2006) 6130-6136.

DOI: 10.1016/j.surfcoat.2005.09.037

Google Scholar

[6] M. Góral, et al., Microstructure of Thermal Barrier Coatings (TBC's) Obtained by Using Plasma Spraying and VPA Methods, Mater. Sci. Forum (2012) 2412-2417.

DOI: 10.4028/www.scientific.net/msf.706-709.2412

Google Scholar

[7] M. Góral, et al., PS-PVD deposition of thermal barrier coatings, Surf. Coat. Tech. 237 (2013) 51-55.

Google Scholar