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The Condition Assessment Of In-Service Vanes Of Gas Turbine Nozzle Unit With Help Of Digital Analysis Of Vane Surface

Treść / Zawartość
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
The paper presents the methodology of condition assessment of in-service vanes of gas turbine nozzle unit with help of digital processing and analysis of vane surface. Included are 3D distribution graphs of basic RGB component colours (red, green and blue) for vane surface images registered with a digital camera (lab conditions) and with two types of commonly used videoscopes (working conditions). The graphs are coupled with results of examination of vane material. Considered were also both alteration of protective coating and core microstructure. The examinations were realised on metallographic sections with help of a SEM. The core microstructure was analysed mainly from the standpoint of modification of reinforcing phase gamma and alteration of phase gamma and carbides. Size and distribution of phase gamma particles determines creep resistance properties (material criterion as the assessment criterion of vane condition). The analysis of images of gas turbine nozzle guide vane surface consists in counting of overheating area in relation to non-overheated area – the ratio is expressed in percentage terms (the criterion – the colour of the surface of a vane considered serviceable in relation to other distributions of colours on surfaces of vanes of different degree of overheating). The proposed approach is aimed at assessment of degree of overheating by reference to discolouration of vane surfaces after certain operational period.
Słowa kluczowe
Rocznik
Strony
23--30
Opis fizyczny
Bibliogr. 7 poz., rys., tab., fot.
Twórcy
autor
autor
  • Białystok Technical University Faculty of Mechanical Engineering, Department of Automatics and Robotics Wiejska 45c Street 15-351 Białystok, Poland, marbog@doktoranci.edu.pl
Bibliografia
  • [1] Błachnio, J., Technical analysis of failures and damage, Basics of aircraft operation, Edited by J., Lewitowicz, Editions Air Force Institute of Technology, Vol. 4, pp. 181-264 Warszawa 2007 (in Polish).
  • [2] Hlebowicz, J., Visual examinations. General principles and exemplary applications, Warszawa, Editions Biuro Gamma, Warszawa 1997.
  • [3] Skočovský, P., Podrábský, T., Belan, J., Operational degradation of aluminium-silicon layer of turbine vanes made from a Ni-based alloy, The Archive of Machinery Technology and Automation, Vol. 24, No 1, pp. 45 – 52, Poznań 2004.
  • [4] Mikułowski, B., Creep-resistant and heat-resistant alloys – superalloys, Editions AGH, Kraków 1997.
  • [5] Sims, C.T., Stoloff, N.S, Hagel, W.C., Superalloys II, Wiley & Sons, New York 1987.
  • [6] Błachnio, J., Bogdan, M., A non-destructive method to assess a degree of overheating of gas turbine vanes, V International Scientific - Technical Conference Explo-Diesel and Gas Turbine'07, Journal of Polish CIMAC (2007), Vol. 2, No 2, pp. 43-50.
  • [7] Bogdan, M., Błachnio, J., The Assessment of Degree of Gas-Turbine Vane Condition as Based on the Analysis of Light Reflected from the Vane Surface. Archives of Transport. No 4, Vol 19, 2007, pp 5-16.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-BPG8-0015-0003
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