Analysis of dimensional accuracy of blade of aircraft engine using a coordinate measuring machine

• Autorzy: Budzik G. , Kubiak K. , Zaborniak M. , Przeszłowski Ł. , Dziubek T. , Cygan M. , Tutak M. , Matysiak H.

Identyfikatory

DOI

10.5604/12314005.1133862

• Języki publikacji: EN

Abstrakty

EN

Technological process of aircraft engine turbine blades requires control of blade geometric parameters. Innovation technologies for measurement of aircraft engine turbine blades are based on coordinate numerical machines – measurement process is based on processing of numerical data obtained by measurement using coordinate measuring machines. The paper presents the opportunity of analysis of dimensional accuracy of aircraft engine turbine blades measurements using coordinate measuring machine (CMM). Coordinate measuring machine allows specifying full methodology for designation of complex dimensions of physical objects (blade of aircraft engine) and transforming 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 and blades geometry analysis 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 geometry, from the standpoint of accuracy and number of collected data points in time. Measurements using a coordinate measuring machine are among the most accurate methods of measuring. 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 of (CMM) 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: 2014
• Tom: Vol. 21, No. 2
• Strony: 33--37
• Opis fizyczny: Bibliogr. 8 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

Zaborniak M.

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

autor

Przeszłowski Ł.

• 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

Cygan M.

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

autor

Tutak M.

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

autor

Matysiak H.

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

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.