Identyfikatory
Warianty tytułu
Języki publikacji
Abstrakty
The article presents a concept of an expert diagnostic system of the turbine engine’s flow path (compressor – combustion chamber – turbine) elements. The system adopts diagnostic signals obtained with the use of non-destructive methods implemented on the non-operating engine. The aim is to detect and assess early stages of damage to selected elements of the engine. The achievement of a reliable diagnosis on the condition of the elements requires the application of a set of diagnostic methods and carrying out the inference, including knowledge about the degradation processes of elements and correlation of the diagnostic (signals) tests results obtained with various methods. A convenient tool, which supports solution of such a set problem is an expert system, which on the one hand, makes it possible to organise the existing formal knowledge, and on the other hand – to use non-formal, or even uncertain, knowledge. The presented concept of the expert diagnostic system is based on PC-Shell system of AITECH Polish Company.
Słowa kluczowe
Wydawca
Czasopismo
Rocznik
Tom
Strony
25--32
Opis fizyczny
Bibliogr. 34 poz., rys.
Twórcy
autor
- Air Force Institute of Technology Ks. Boleslawa Street 6, 01-494 Warsaw, Poland tel.:+48 22 261851313, fax: +48 22 261851313
autor
- Air Force Institute of Technology Ks. Boleslawa Street 6, 01-494 Warsaw, Poland tel.:+48 22 261851313, fax: +48 22 261851313
Bibliografia
- [1] Air Force Institute of Technology Reports, Warsaw, Poland 2000-2016.
- [2] Blachnio, J., Analysis of causes of decohesion of a gas turbine blade made of EI 867-WD alloy, Aircraft Engineering and Aerospace Technology, 83(1), pp. 14-20, 2011.
- [3] Blachnio, J., Bogdan, M., A non-destructive method to assess condition of gas turbine blades, based on the analysis of blade-surface images, Russian Journal of Nondestructive Testing, 46(11), pp. 860-866, 2010.
- [4] Błachnio, J., Analysis of technical condition assessment of gas turbine blades with non-destructive methods, Acta Mechanica et Automatica, 7(4), pp. 203-208, 2013.
- [5] Błachnio, J., Capabilities to assess health/maintenance status of gas turbine blades with non-destructive methods, Polish Maritime Research, 21(4), pp. 41-47, 2014.
- [6] Błachnio, J., The effect of changing loads affecting the marten site steel on its structure and the Barkhausen noise level, NDT and E International, 41(4), pp. 273-279, 2008.
- [7] Błachnio, J., The effect of high temperature on the degradation of heat-resistant and high-temperature alloys, in Solid State Phenomena, pp. 744-751, 2009.
- [8] Błachnio, J., Bogdan, M., Zasada, D., Increased temperature impact on durability of gas turbine blades, Operation and Reliability, 19(1), pp. 48-53, 2017.
- [9] Błachnio, J., Kułaszka, A., The active thermography method as used to assess the bearing of temperature on thermophysical properties of superalloy of a gas-turbine blade, in Solid State Phenomena, Trans Tech Publications Ltd., pp. 502-507, 2013.
- [10] Błachnio, J., et al., Assessment of technical condition demonstrated by gas turbine blades by processing of images for their surfaces, Journal of KONBIN, 21(1), pp. 41-50, 2012.
- [11] Błachnio, J., et al., The attempt to assess the technical condition of a gas turbine blade when information on its operating condition is limited, Journal of KONBIN, 30(1), pp. 75-86, 2014.
- [12] Błachnio, J., Zabrocka, I., Image of the surface of gas turbine blade as a diagnostic signal, Acta Mechanica et Automatica, 7(4), pp. 209-214, 2013.
- [13] Borowczyk, H., Expert system for supporting the diagnostic inference, Problems of comprehensive diagnosing the bearings of the helicopter's turbine engine, Borowczyk, H., Editor, Air Force Institute of Technology, Warsaw 2011.
- [14] Borowczyk, H., Model of the airframe's diagnostic system and the aircraft's drive unit., in V Int. Conf. Airplanes and Helicopters Diagnostics Airdiag 97, Air Force Institute of Technology, Warsaw 1997.
- [15] Borowczyk, H., Problems of comprehensive diagnosing the bearings of the helicopter's turbine engine, Warsaw Eds., Air Force Institute of Technology, 163, 2011.
- [16] Borowczyk, H., Błachnio, J., Spychała, J., Scopus as a meta-source of knowledge about turbine blade damage in the aspect of designing an expert diagnostic system, Journal of KONBiN, p. 18, 2017.
- [17] Borowczyk, H., Kwieciński, R., Expert diagnostic system of the afterburner control system of the jet turbine engine, Diagnostics, 39, p. 6, 2006.
- [18] Borowczyk, H., Kwieciński, R., Design of the knowledge base of the expert diagnostic system of the jet turbine engine's afterburner control system, DPP2005, Measurements Automation Control, No. 9bis, pp. 148-150, Diagnostics of industrial processes, 2005.
- [19] Borowczyk, H., Kwieciński, R., Creation of a base of rules of the expert diagnostic system with the use of the diagnosed object's identified model, in 8th Int. Conf. Aircraft and helicopter diagnostics, AIRDIAG'2005, Warsaw 2005.
- [20] Borowczyk, H., Lindstedt, P., Formalisation of expertise in diagnosis of control systems of the aircraft turbine engines, in DPP 2007: Diagnostics of processes and systems, ed. by Józef Korbicz, Krzysztof Patan, Marek Kowal, Warsaw: Akademicka Oficyna Wydawnicza EXIT, pp. 141-148, Modern Science Problems: Theory and Application. Automation and Robotics, 2007.
- [21] Cernuschi, F., et al., Solid particle erosion of standard and advanced thermal barrier coatings, Wear, 348-349, pp. 43-51, 2016.
- [22] Kirschner, M., et al., Erosion testing of thermal barrier coatings in a high enthalpy wind tunnel, American Society of Mechanical Engineers (ASME), 2014.
- [23] Lindstedt, P., Borowczyk, H., Aircraft's comprehensive diagnostic system, Problems of the aircraft technology research and operation, pp. 131-152, Warsaw 1999.
- [24] Michalik, K., PC SHELL 4.5, Expert shell system, K. Michalik, AITECH, Artificial Intelligence Laboratory, Katowice 2006.
- [25] Mulawka, J., Expert systems, WNT, Warsaw1996.
- [26] Naeem, M., Implications of turbine erosion for an aero-engine's high-pressure-turbine blade's low-cycle-fatigue life-consumption, Journal of Engineering for Gas Turbines and Power, 131(5), 2009.
- [27] Niziński, S., Michalski, R., Diagnostics of technical objects, Faculty of Transport and Electrical Engineering, Radom 2002.
- [28] Pawlak, M., Expert systems in the machinery operation, Lublin of University of Technology Lublin 1996.
- [29] Tong, J., et al., Assessment of service induced degradation of microstructure and properties in turbine blades made of GH4037 alloy, Journal of Alloys and Compounds, 657, pp. 777-786, 2016.
- [30] Walter, K., Greaves, W., Life assessment of gas turbine components using nondestructive inspection techniques, American Society of Mechanical Engineers (ASME), 1997.
- [31] Woźny, P., Błachnio, J., Analysis of Damage Arising from Exploitation of the Aircraft. Journal of KONBIN, 32(1), pp. 5-18, 2014.
- [32] Zhao, L., Au, P., The microstructure and high-temperature erosion behavior of an aluminide-coated turbine blade, 2013.
- [33] Żółtowski, B., Foundations of the machinery diagnostics, WATR, Bydgoszcz 1996.
- [34] Żółtowski, B., Cempel, C., Engineering of the machinery diagnostics, Faculty of Transport and Electrical Engineering, Radom 2004.
Uwagi
PL
Opracowanie rekordu w ramach umowy 509/P-DUN/2018 ze środków MNiSW przeznaczonych na działalność upowszechniającą naukę (2018).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-ae11e97c-ca86-4039-8db7-4b24989931c5