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Examination of changes in microstructure of turbine vanes with the user of non-destructive methods

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Treść / Zawartość
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Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
The processes associated with operation of traction, marine and avionic turbine engines entail occurrence of various defects affecting turbine components, in particular turbine vanes. The main reasons for defects and deterioration of gas turbine vanes include thermal fatigue and overheating of the vane material. This is why continuous monitoring of technical condition demonstrated by crucial engine components, such as turbine vanes, is a matter of great importance. The monitoring operations involve all the up-to-date diagnostic methods intended to detect and interpret possible hazards. The initial assessment is carried out with the use of visual inspection methods, but the major phase of investigations consists in metallographic examinations, which disables further operation of the vanes. Possible mistakes during the initial assessment of the engine condition result in huge costs due to unnecessary overhaul of the entire engine. Therefore, there is a need to apply non-destructive test methods to the maximum possible extent with the aim to evaluate the overheating status of the gas turbine vanes on a current basis. This paper outlines the non-destructive test methods that are currently in use and that are based on analysis of surface images obtained from the examined parts within the visible bandwidth of electromagnetic waves as well as on surface analysis of examined items with the use of a ring-wedge detector. Particular attention is paid to opportunities that enable unbiased diagnostics of changes in the microscopic structure of vanes by means of the non-destructive thermographic method as well the X-ray computer tomography.
Rocznik
Strony
17--27
Opis fizyczny
Bibliogr. 17 poz., rys., tab.
Twórcy
autor
  • Białystok University of Technology ul. Wiejska 45 C, 15-351 Białystok, Poland tel.:+48 22 6851982, fax: +48 22 6851041, jozef.blachnio@itwl.pl
Bibliografia
  • [1] Dżygadło Z. et al. Rotor units of turbine engines. WKŁ, Warsaw, 1982. (in Polish)
  • [2] Majka H., Sieniawski J.: Investigations on kinetics and coagulation of the γ' phase in the EI-867 nickel superalloy. Archives of Material engineering, vol. 4, 1998, pp. 237-254. (in Polish)
  • [3] Błachnio, J.: The effect of high temperature on the degradation of heat-resistant and high-temperature alloys. Solid State Phenomena, Vols. 147-149, 2009, pp. 744-752.
  • [4] Błachnio J., Bogdan M.: Diagnostics of the technical condition demonstrated by vanes of gas turbines, Diagnostics, No 1 (45), 2008, pp. 91-96.
  • [5] Błachnio J., Bogdan M.: The assessment of the jet gas-turbine blade condition. Archives of Transport. Nr 4, 2008.
  • [6] Kułaszka, A. Szczepankowski A.: Reports on research developments, ITWL, Warsaw 2000 – 2009, unpublished. (in Polish)
  • [7] Kułaszka, A., Chalimoniuk, M.: Reports on research developments, ITWL, Warsaw 2000 – 2010, unpublished. (in Polish)
  • [8] Hodor K.: Gradient structure of the external layers coated with superalloys on the basis of Ni and Ni-Fe. PhD Thesis, AGH University of Technology, Cracow, 2002. (in Polish)
  • [9] Poznańska A.: Lifetime of vanes made of the EI-867 alloy and used for the assembly of avionic motors with the aspect of non-uniform deformation and structural alterations. PhD Thesis, University of Technology in Rzeszów, Rzeszów, 2000.
  • [10] Lewitowicz J. [ed.] et al. Fundamentals for the theory of aircraft operation, Vol. 4 Publishing House of the Air Force Institute of Technology (ITWL), Warsaw, 2007.
  • [11] Pawlak W. et al. Identification of the relationship between the technical condition of turbojet engines and the distribution of temperature fields upstream turbines. Report on the R&D project KBN No 8T12D0142, Institute of Aviation, Warsaw, 2003. (in Polish)
  • [12] Błachnio J., Bogdan M.: A non-destructive method to assess a degree of overheating of gas turbine blades. -:5th International Scientific - Technical Conference, Explo-Diesel and Gas Turbine'07, Poland, 2007.
  • [13] http://iar-ira.nrc-cnrc.gc.ca/gtl/gtl_10e_e.html - National Research Concil Canada.
  • [14] Oliferuk W.: Infrared thermography for non-destructive testing of materials and equipment. Gamma Office, Warsaw 2008. (in Polish)
  • [15] Kułaszka A., Błachnio J., Kornas Ł.: Analysis of feasibility to assess microstructure of gas turbine blades by means of the thermographic method. Journal of KONBIN, No 1(13), 2010, pp. 325-340.
  • [16] Carl. V., Becker E., Sperling A.: Thermography inspection system for gas turbine blades. 7th European Conference on non-destructive testing, Copenhagen, 1998, pp. 2658 - 2665.
  • [17] Data sheets from YXLON International GmbH.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-BPG8-0035-0027
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