Articles
Análise da influência do desvio geométrico nas características aerodinâmicas de pás de ventilador
Publicado 2019-09-26
Palavras-chave
- Aerodynamic characteristics, fan, gas turbine engine, geometric deviations, low-pressure compressor, NUMECA, robust optimization, Siemens NX.
Como Citar
Arkhipov, A. N., Bugryashova, E. V., Ravikovich, Y. A., Kholobtsev, D. P., & Shevyakov, A. O. (2019). Análise da influência do desvio geométrico nas características aerodinâmicas de pás de ventilador. Amazonia Investiga, 8(22), 443–452. Recuperado de https://amazoniainvestiga.info/index.php/amazonia/article/view/768
Resumo
Neste artigo são apresentados os resultados dos cálculos das características aerodinâmicas das pás do ventilador do motor de turbina de gás para um avião regional, tendo em conta os desvios de produção. Além disso, são descritos os modelos analisados de lâminas com diferentes desvios geométricas de perfil aerodinâmico, o modelo calculado da fase do ventilador e as características aerodinâmicas estimadas. Por sua vez, os resultados do cálculo são ilustrados com um exemplo.
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Referências
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.
