Articles
Analysis of the geometric deviation influence on the aerodynamic characteristics of the fan blades
Published 2019-09-26
Keywords
- Aerodynamic characteristics, fan, gas turbine engine, geometric deviations, low-pressure compressor, NUMECA, robust optimization, Siemens NX.
How to Cite
Arkhipov, A. N., Bugryashova, E. V., Ravikovich, Y. A., Kholobtsev, D. P., & Shevyakov, A. O. (2019). Analysis of the geometric deviation influence on the aerodynamic characteristics of the fan blades. Amazonia Investiga, 8(22), 443–452. Retrieved from https://amazoniainvestiga.info/index.php/amazonia/article/view/768
Abstract
In this article there are the results of the aerodynamic characteristic calculations for the fan blades of the gas turbine engine for the regional aircraft, considering production deviations. The analyzed models of blades with different geometric airfoil deviations, the calculated model of the fan stage, the estimated aerodynamic characteristics are described. Here you can find the example of the calculation results.
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References
Arkhipov A.N., Ravikovich Yu.A., Fedorov I.M., Kholobtsev D.P. (2017). Constructing 3D fan blade models in cadsystem on the basis of coordinate measuring techniques. Vestnik of Samara University. Aerospace and Mechanical Engineering, 16(3), 7-16.
Arkhipov A.N., Bugryashova E.V., Ravikovich Yu.A., Savin R.A., Terentjev V.V., Shevyakov A.O. (2018). Automated construction of a fan blade model according to data of CAD profile measurements. Vestnik of Samara University. Aerospace and Mechanical Engineering, 17(4), 7-17.
Arkhipov A.N., Ravikovich Yu.A., Matushkin A.A., Kholobtsev D.P. Shevjakov A.O. (2018). Automation program for the construction of a fan blade using NX CAD systems according to KIM. Certificate of state registration of a computer program ?2018665345. 04 December 2018.
Baturin O.V., Goryachkin E.S., Kolmakova D.A., Popov G.M., Ledenev A.I. (2013). Numerical simulation of the working process of a free turbine together with low-pressure turbines, a transition channel and an output device. Electronic textbook. Samara: Samara state aerospace university.
Bestle D., Flassig P.M. (2010). Optimal Aerodynamic Compressor Blade Design Considering Manufacturing Noise. Conference: Association for Structural and Multidisciplinary Optimization in the UK.
Bestle D., Flassig P.M., Dutta A.K. (2011). Robust Design of Compressor Blades in the Presence of Manufacturing Noise. Conference: 9th European Conference on Turbomachinery.
Inozemtsev, A.A., Nikhamkin, M.A., Sandratskii, V.L. (2008). Fundamentals of the Design of Aircraft Engines and Power Plants. Moscow: Mashinostroenie.
Ma C., Gao L., Cai Y., Li R. (2017). Robust Optimization Design of Compressor Blade Considering Machining Error. Turbomachinery Technical Conference and Exposition. ASME Turbo Expo.
NUMECA Int., «Flow Integrated Enviroment», User Manual, Numeca Int., Brussels, Belgium, 2014.
Li Z., Liu Y., Agarwal R.K. (2018). Robust Optimization Design of Single-Stage Transonic Axial Compressor Considering the Manufacturing Uncertainties. Turbomachinery Technical Conference and Exposition. ASME Turbo Expo.
Skibin, V.A., Solonin, V.I., Sosunov, V.A., Temis, Yu.M. (2010). Machine Building. Encyclopedia. Moscow: Mashinostroenie, 2010
Vinogradov K.A., Kretinin G.V., Leshenko I.A., Otriakhina K.V., Fedechkin K.S., Vinogradova O.V., Bushmanov V.V., Khramin R.V. (2018). Robust Multiphysics Optimization for Fan Blade Aerodynamic Efficiency, Structural Properties and Flutter Sensitivity. Turbomachinery Technical Conference and Exposition. ASME Turbo Expo.
Arkhipov A.N., Bugryashova E.V., Ravikovich Yu.A., Savin R.A., Terentjev V.V., Shevyakov A.O. (2018). Automated construction of a fan blade model according to data of CAD profile measurements. Vestnik of Samara University. Aerospace and Mechanical Engineering, 17(4), 7-17.
Arkhipov A.N., Ravikovich Yu.A., Matushkin A.A., Kholobtsev D.P. Shevjakov A.O. (2018). Automation program for the construction of a fan blade using NX CAD systems according to KIM. Certificate of state registration of a computer program ?2018665345. 04 December 2018.
Baturin O.V., Goryachkin E.S., Kolmakova D.A., Popov G.M., Ledenev A.I. (2013). Numerical simulation of the working process of a free turbine together with low-pressure turbines, a transition channel and an output device. Electronic textbook. Samara: Samara state aerospace university.
Bestle D., Flassig P.M. (2010). Optimal Aerodynamic Compressor Blade Design Considering Manufacturing Noise. Conference: Association for Structural and Multidisciplinary Optimization in the UK.
Bestle D., Flassig P.M., Dutta A.K. (2011). Robust Design of Compressor Blades in the Presence of Manufacturing Noise. Conference: 9th European Conference on Turbomachinery.
Inozemtsev, A.A., Nikhamkin, M.A., Sandratskii, V.L. (2008). Fundamentals of the Design of Aircraft Engines and Power Plants. Moscow: Mashinostroenie.
Ma C., Gao L., Cai Y., Li R. (2017). Robust Optimization Design of Compressor Blade Considering Machining Error. Turbomachinery Technical Conference and Exposition. ASME Turbo Expo.
NUMECA Int., «Flow Integrated Enviroment», User Manual, Numeca Int., Brussels, Belgium, 2014.
Li Z., Liu Y., Agarwal R.K. (2018). Robust Optimization Design of Single-Stage Transonic Axial Compressor Considering the Manufacturing Uncertainties. Turbomachinery Technical Conference and Exposition. ASME Turbo Expo.
Skibin, V.A., Solonin, V.I., Sosunov, V.A., Temis, Yu.M. (2010). Machine Building. Encyclopedia. Moscow: Mashinostroenie, 2010
Vinogradov K.A., Kretinin G.V., Leshenko I.A., Otriakhina K.V., Fedechkin K.S., Vinogradova O.V., Bushmanov V.V., Khramin R.V. (2018). Robust Multiphysics Optimization for Fan Blade Aerodynamic Efficiency, Structural Properties and Flutter Sensitivity. Turbomachinery Technical Conference and Exposition. ASME Turbo Expo.
