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Numerical Simulation of Rotary Forging Inconel 718 Superalloy Applied to Aeronautical Components

Published online by Cambridge University Press:  02 March 2016

A. Loyda
Affiliation:
Universidad Autónoma de Nuevo León. Facultad de Ingeniería Mecánica y Eléctrica. Centro de Investigación e Innovación en Ingeniería Aeronáutica, Ave. Universidad S/N, Cd. Universitaria, San Nicolás de los Garza, N.L. C.P. 66451
G.M. Hernández-Muñoz
Affiliation:
Universidad Autónoma de Nuevo León. Facultad de Ingeniería Mecánica y Eléctrica. Centro de Investigación e Innovación en Ingeniería Aeronáutica, Ave. Universidad S/N, Cd. Universitaria, San Nicolás de los Garza, N.L. C.P. 66451
L.A. Reyes-Osorio
Affiliation:
Universidad Autónoma de Nuevo León. Facultad de Ingeniería Mecánica y Eléctrica. Centro de Investigación e Innovación en Ingeniería Aeronáutica, Ave. Universidad S/N, Cd. Universitaria, San Nicolás de los Garza, N.L. C.P. 66451
P. Zambrano
Affiliation:
Universidad Autónoma de Nuevo León. Facultad de Ingeniería Mecánica y Eléctrica. Centro de Investigación e Innovación en Ingeniería Aeronáutica, Ave. Universidad S/N, Cd. Universitaria, San Nicolás de los Garza, N.L. C.P. 66451
F. Montemayor-Ibarra
Affiliation:
Universidad Autónoma de Nuevo León. Facultad de Ingeniería Mecánica y Eléctrica. Centro de Investigación e Innovación en Ingeniería Aeronáutica, Ave. Universidad S/N, Cd. Universitaria, San Nicolás de los Garza, N.L. C.P. 66451
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Abstract

Nowadays the aeronautical industry keeps strict quality standards in its dimensional specifications, mechanical properties and microstructural characteristics. Therefore, the involved manufacturing processes require keeping high standards. The nickel based superalloys are present in many components of the jet engines, being the Inconel 718MR superalloy the most common, making up to 50% of the jet engine. This is designed to resist high temperatures, corrosion and creep. The process of rotary forging is a manufacturing process that is currently under scientific and technological development in the aeronautical industry. An Avrami model coupled with a commercial FEM platform (DEFORMTM 3D) was developed to evaluate the average grain size, as a function of the working conditions at 980 °C and 1000 °C. The results provide a better understanding of the influence of temperature in the grain size evolution during the rotary forging process, compared with previous reports.

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Articles
Copyright
Copyright © Materials Research Society 2016 

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References

REFERENCES

Campbell, F., Manufacturing Technology for Aerospace Structural Materials, 1st ed. (Elsevier, Amsterdam, 2006), pp. 219223.Google Scholar
Chamanfar, A., Sarrat, L., Jahazi, M., Asadi, M., Weck, A. and Koul, A., Mater. Design 52, 791800 (2013).CrossRefGoogle Scholar
Mangas, Á., Santos, M., San José, J., Atxaga, G. and Adarraga, O., Key Eng. Mater. 504-506, 169174 (2012).CrossRefGoogle Scholar
Grieve, D., PhD. Thesis, University of Nottingham, 1991.Google Scholar
Mangas, Á., Santos, M., Zarazua, J., San José, J., Atxaga, G. and Adarraga, O., Key Eng. Mater. 554-557, 234247 (2013).CrossRefGoogle Scholar
Thomas, A., El-Wahabi, M., Cabrera, J.M. and Prado, J.M., J. Mater. Process. Technol. 177(1), 469472 (2006).CrossRefGoogle Scholar
Han, X. and Hua, L., J. Mater. Process. Technol. 209, 53535362 (2009).CrossRefGoogle Scholar
Deng, X., Hua, L., Han, X. and Song, Y., Mater. Design 32, 13761389 (2011).CrossRefGoogle Scholar
Beaudoin, , Srinivasan, R. and Semiatin, S., J.O.M. 54, 2529 (2002).Google Scholar
Reyes Osorio, L., PhD. Thesis, Universidad Autónoma de Nuevo León, México, 2013.Google Scholar