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Tytuł artykułu

Microstructure of thermal barrier coatings deposited by APS method with application of new type ceramic powders

Autorzy
Wybrane pełne teksty z tego czasopisma
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
Purpose: The paper presents results of structural research into thermal barrier coatings obtained by the APS. For the base the Rene 80 alloy was used, whereas a MeCrAlY-type multicomponent alloy was used for an interlayer. Design/methodology/approach: Throughout the research an optic microscope as well as a scanning electron microscope were employed. Measurements of the formed structure’s porosity were taken. Findings: It has been observed that application of novelty ceramic powders allows for a possibility of forming thermal barrier coatings, which can be used for protecting of the combustion chamber’s surface as well as turbine’s blades in an aircraft engine. Research limitations/implications: Further research into resistance to oxidation of these coatings seems necessary for experimental determination of their actual work temperature. Practical implications: They can be successfully applied in automotive industry for coating of petrol or diesel engine’s components. Originality/value: Investigation into possible applications of two-layer and composite coatings, which may improve the work temperature of thermal barrier coatings, is feasible.
Rocznik
Strony
912--917
Opis fizyczny
Bibliogr. 15 poz., rys., tab.
Twórcy
autor
  • Department of Materials Science, Rzeszow University of Technology, Al. Powstanców Warszawy 12, 35-959 Rzeszów, Poland
autor
  • WSK PZL Rzeszow S.A., ul. Hetmańska 120, 35-078 Rzeszów, Poland
Bibliografia
  • [1] D.S. Rickerby, H.C. Low, in Proc. 4th European Propulsion Forum, Royal Aeronautical Society, London, 12, 1993.
  • [2] Coatings for high temperature structural materials, National Materials Advisory Board, Report, National Academy Press, Washington, DC, 1996.
  • [3] G. Lehnert, H. Meinhardt, Present state and trend of development of surface coating methods against oxidation and corrosion at high temperatures, Electrodeposition and Surface Treatment 1/1 (1972) 71-76.
  • [4] D. Driver, D.W. Hall, G.W. Meetham, The development of the gas turbine engine, Applied Science Publishers, London, 1981.
  • [5] G.W. Goward, D.H. Boone, Mechanisms of formation of diffusion aluminide coatings on nickel-base superalloys, Oxiddation of metals 3 (1971) 475-496.
  • [6] G.W. Goward, Progress in coatings for gas turbine airfoils, Surface and Coatings Technology 108-109 (1998) 73-79.
  • [7] J.R. Nicholls, Designing oxidation-resistant coatings. Journal of the Minerals, Metals and Materials Society 52 (2000) 28-35.
  • [8] F.T. Talboom, R.C. Elam, and L.W. Wilson, evaluation of advanced superalloy Protection Systems, Report CR7813, National Aeronautics and Space Administration, Houston, 1970.
  • [9] D.K. Gupta and D.S. Duvall, Coatings for single crystal superalloys, The Minerals, Metals and Materials Society, Warrendale, 1984
  • [10] http://www.sulzermetco.com/en/desktopdefault.aspx/tabid-1741//3381_read-5289.
  • [11] R. Vaßen, M. O. Jarligo, T. Steinke, D. E. Mack, D. Stover, Overview on advanced thermal barrier coatings Surface and Coatings Technology 205/4 (2010) 938-942.
  • [12] A. Nusair Khan, I.N. Qureshi, Microstructural evaluation of ZrO2-MgO coatings Journal of Materials Processing Technology 209/1 (2009) 488-496.
  • [13] M. Góral, M. Drajewicz M. Pytel S. Kotowski, Characterization of powders used for LPPS thin film plasma spraying of thermal barrier coatings, Journal of Achievements in Materials and Manufacturing Engineering 47/2 (2011) 157-165 .
  • [14] G. Moskal, B. Witala, A. Rozmysłowska, Metallographic preparation of the conventional and new TBC layers, Archives of Materials Science and Engineering 39/1 (2009) 53-60.
  • [15] G. Moskal, The porosity assessment of thermal barrier coatings obtained by APS method, Journal of Achievements in Materials and Manufacturing Engineering 20 (2007) 483-486.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-f2bc4db3-3d4a-41d3-a4b4-10dd45513fa0
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