Analysis model and classification of the geometry of gas turbine engine blades

Aeronautical and Space-Rocket Engineering

Aircraft engines and power generators


Аuthors

Pechenin V. A.*, Bolotov M. A.**

Samara National Research University named after Academician S.P. Korolev, 34, Moskovskoye shosse, Samara, 443086, Russia

*e-mail: vadim.pechenin2011@yandex.ru
**e-mail: maikl.bol@gmail.com

Abstract

The quality of aircraft engines (specific consumption, gas-dynamic stability, reliability, service life) is embedded in the course of the design process, fixed outat the stage of finalization, providedin the course of production, and implemented during operation. Account for actual geometry of the partsduring design process, and forming the best for current manufacturing environment conditions geometry of the products during manufacturing and assembling is one of the reserves allowing aircraft engine quality increase. Realization of the above mentioned reserve becomes possible with implementation of intellectual system of aircraft engines quality provision. The article presents the technique for the intellectual system of aircraft engines quality provision forming. It shows the structure of the intellectual system of aircraft engines quality provision. Mathematical model of the system with regard to analysis and clustering of complex shapes and surfaces is built. The analysis allows calculating parameters of a part location deviation from nominal geometry, and calculation deviation of parts shapes. Analysis tools are as follows: an iterative algorithm of nearest points, piecewise splines approximation of surface points, Fourier transform. We used an algorithm of k-means and self-organizing Kohonens neural networks as clustering methods. For adequate profile parameters clastering (shape and position) these parameters were normalized to the range of [0,1]. Complex shape geometry intellectual analysis model was implemented in MATLAB®. Within the framework of the developed system using obtained models, clustering of series of GTE backet compressor blades, obtained as a result of measuring with CMMs DEA Global Performance 07.10.07. Implementation of neural networks seems to be more promising for the tasks of clustering solving compared to static methods, due to the possibility of learning and clustering of new objects on the basis of accumulated know-how. For further model realization in manufacturing building of new program modules is necessary

Keywords:

analysis, Fourier transformation, clustering, neural network

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