Optical measurement of aircraft engine turbine blades

• Autorzy: Budzik G. , Kubiak K. , Rokicki P. , Dziubek T. , Nowotnik A. , Matysiak H. , Cygan R. , Tutak M. , Boś P.
• Języki publikacji: EN

Abstrakty

EN

Manufacturing of aircraft engine turbine blades requires control of blade geometric parameters at different stages of technological process. Acceleration and automation of measurement process can affect the duration of the finished item production. Modern technologies for measurement of aircraft engine turbine blades are based on numerical machines - measurement process is based on processing of numerical data obtained by measurement using coordinate measuring machines. The paper presents the opportunity of automation of aircraft engine turbine blades measurements using scanner ATOS II Triple Scan with blue light source technology. Coordinate measuring technique allows to specify full methodology for designation of complex dimensions of physical objects and transform them into a computer program space of coordinate measuring devices. Presented paper includes capabilities of device used in the study to improve the measurement process in the technological and economical aspects. Another issue described in the paper is impact of measurement performance in automatic mode on the quality of performance – the numerical model of surface, from the standpoint of accuracy and number of collected data points in time. The paper includes an analysis of conditions related to the measurement works, such as the process of preparing the model, measurement equipment and data processing capacity. As the result methodology for automated scanning measurements of aircraft engine turbine blades will be presented.

Słowa kluczowe

EN

aircraft engines turbine blades; optical measurements; coordinate measuring technique

• Wydawca: Łukasiewicz Research Network - Institute of Aviation ; European Science Society of Powertrain and Transport KONES Poland ; Wydawnictwo Instytutu Technicznego Wojsk Lotniczych
• Czasopismo: Journal of KONES
• Rocznik: 2013
• Tom: Vol. 20, No. 2
• Strony: 21--26
• Opis fizyczny: Bibliogr. 9 poz., rys.

Twórcy

autor

Budzik G.

• Rzeszow University of Technology Faculty of Mechanical Engineering and Aeronautic Powstańców Warszawy Av. 8, 35-959 Rzeszów, Poland

autor

Kubiak K.

• Rzeszow University of Technology Faculty of Mechanical Engineering and Aeronautic Powstańców Warszawy Av. 8, 35-959 Rzeszów, Poland

autor

Rokicki P.

• Rzeszow University of Technology Faculty of Mechanical Engineering and Aeronautic Powstańców Warszawy Av. 8, 35-959 Rzeszów, Poland

autor

Dziubek T.

• Rzeszow University of Technology Faculty of Mechanical Engineering and Aeronautic Powstańców Warszawy Av. 8, 35-959 Rzeszów, Poland

autor

Nowotnik A.

• Rzeszow University of Technology Faculty of Mechanical Engineering and Aeronautic Powstańców Warszawy Av. 8, 35-959 Rzeszów, Poland

autor

Matysiak H.

• Research Center Functional Materials, Warsaw University of Technology Wołoska Street 141, 02-507 Warszawa, Poland

autor

Cygan R.

• WSK PZL-Rzeszów S.A. Hetmańska Street 120, 35-959 Rzeszów, Poland

autor

Tutak M.

• WSK PZL-Rzeszów S.A. Hetmańska Street 120, 35-959 Rzeszów, Poland

autor

Boś P.

• PWSZ w Krośnie Rynek 1, 38-400 Krosno, Poland tel.: [phone], fax: [phone]

Bibliografia

• [1] Budzik, G., Geometrical Accuracy of Aircraft Engine Turbine Blades, Oficyna Wydawnicza Politechniki Rzeszowskiej, Rzeszów 2013.
• [2] Budzik, G., Possibilities of Using Vacuum Casting Process for Manufacturing Cast Models of Turbocharger Impeller, Journal of KONES Powertrain and Transport, Vol. 14, No. 3, pp. 125-130, Warszawa 2007.
• [3] Hu, D., Wang, R., Tao, Z., Probabilistic design for turbine disk at high temperature, Aircraft Engineering and Aerospace Technology, Vol. 83, Is. 4, pp. 199-207, 2011.
• [4] Hu D., Wang R., Combined fatigue experiments on full scale turbine components, Aircraft Engineering and Aerospace Technology, Vol. 85, Is. 1, pp. 4-9, 2013.
• [5] Lin, T., Lee, J., Lwin, T., Integrated approach for rotor blade manufacturing cost estimate, Aircraft Engineering and Aerospace Technology, Vol. 83, Is. 4, pp. 235-244, 2011.
• [6] Onyszko, A., Kubiak, K., Bogdanowicz, W., Sieniawski, J., X-ray topography and crystal orientation study of nickel-based CMSX-4 superalloy single crystal, Crystal Research and Technology 45, 12 pp. 1326-1332, 2010.
• [7] Piccione, E., Bernardini, G., Gennaretti, M., Structural-aeroelastic finite element modeling for advanced-geometry rotor blades, Aircraft Engineering and Aerospace Technology, Vol. 84, Is. 6, pp. 367-375, 2013.
• [8] Ratajczyk, E., Współrzędnościowa technika pomiarowa, Oficyna Wydaw. Politechniki Warszawskiej, Warszawa 2005.
• [9] Witek, L., Orkisz, M., Wygonik, P., et al. Fracture analysis of a turbine casing, Engineering Failure Analysis, Elsevier, Vol. 18, Is. 3 pp. 914-923.