Study of the strength of the blade of aircraft turbine

Authors

  • Ubaldo Yancachajlla Tito Faculty of Mechanics Engineering, National University of Engineering

DOI:

https://doi.org/10.21754/tecnia.v16i2.395

Keywords:

aircraft turbine, resistence of the blade, alabe calculation, finite elements method

Abstract

The work consists of demonstrating the possible utilization of the methods of the finite element for the case of calculating of a blade of turbine of a plane by method of the finite elements, first we find the critical stress in the blade due to the solicitations of the centrifugal force and the gas-dynamics, these generate stress of  traction and flexion principally. Comparing these results with the obtained one previously for traditional methods, managing to validate our results for the finite element method. Finally we will find the manners of vibration and natural frequencies of the blade of the turbine, coming to conclusions that they reconcile to the published ones in the literature. The method of the finite element represents a powerful tool that can be used satisfactorily for the optimization of the such complex designs as of the turbine.

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References

[1] Oñate, E., "Cálculo de estructuras por el método de elementos finitos". Centro internacional de métodos numéricos en ingeniería. Barcelona-España 1992.
[2] Escubachevski, A., "Motores de aviación de turbina a gas, diseño y cálculo de sus piezas". Construcción de máquinas. Moscú 1992.
[3] Losissk, B., "Construcción y resistencia de motores de aviación de turbina gas". Transporte aéreo. Moscú 1992.
[4] Bor, V., "Cálculo de resistencia de piezas de máquinas". Manual, Moscú 1996.
[5] Balina, N., "Resistencia y durabilidad de construcciones durante la fluencia". San Petersburgo 1997.
[6] "Vibraciones mecánicas en ingeniería" Universidad Politécnica de Valencia - España, 1998.
[7] Willems, F. R., "Cálculo de resistencia de estructuras por métodos matriciales y de elementos finitos". Barcelona - España, 1993.
[8] Zienkiewicz, O. C., Taylor, R. L., "El método de los elementos finitos". Barcelona - España, 1993.
[9] Guía de usuario, "Cosmos/works". Estados Unidos, N. Y. 2006
[10] Tutoriales, "Cosmos/Works". Estados Unidos, N. Y. 2006.

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Published

2006-12-01

How to Cite

[1]
U. Yancachajlla Tito, “Study of the strength of the blade of aircraft turbine”, TEC, vol. 16, no. 2, pp. 77–91, Dec. 2006.

Issue

Vol. 16 No. 2 (2006)

Section

Articles

License

Copyright (c) 2006 TECNIA

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