PSI - Issue 39
Gonzalo M. Domínguez Almaraz et al. / Procedia Structural Integrity 39 (2022) 281–289 Author name / Structural Integrity Procedia 00 (2019) 000–000
288
8
for the commercial I-718. A study in this direction is expected in the future. Further investigations should be carried out in order to assess the quantitative effects of heats treatments related to: the chemical composition of parent material and the resulting mechanical properties.
Acknowledgments The authors express their special mention of gratitude to CONACYT (The National Council for Science and Technology, Mexico), for the financial support destined to this study through the program grant: CB-241117-2014. An additional mention of gratitude to the University of Michoacán in Mexico for the received support in the development of this work.
Disclosure statement No potential conflict of interest was reported by the authors.
References
[1] Ma, X., Duan, Z., Shi, H., Murai, R., Yanagisawa, E. 2010. Fatigue and fracture behavior of nickel-based superalloy Inconel 718 up to very high cycle regime, J. of Zhejiang University- SCIENCE A App. Phys. & Eng. 11(10), 727-737. [2] Chen, Q., Kawagoishi, N., Wang, Q.Y., Yan, N., Ono, T., Hashigushi, G. 2005 Small crack behavior and fracture of nickel-based superalloy under ultrasonic fatigue. Int. J. of Fat. 27, 1227-1232. [3] Mazur, Z., Luna-Ramírez, A., Islas, J.A., Campos-Amezcua, A. 2005. Failure analysis of a gas turbine blade made of Inconel 738LC. Eng. Fail. Anal. 12, 474-486. [4] Garay, F. et al. 2020. Computational Analysis of the IN718 Material Microstructure (Nickel-Based INCONEL Superalloy): Potential Applications in the Military Industry. Applied Computer Sciences in Engineering. WEA 2020. Communications in Computer and Information Science, vol. 1274. Springer, Cham. https://doi.org/10.1007/978-3-030-61834-6_30 [5] Acka, E., Gursel, A.A. 2015. Review on superalloys and IN718 Nickel-based Inconel superalloy. Period. of Eng. And Nat. Sci. 3, 15-27. [6] Fabry, E., Ceskovic, M. 2017. Aircraft gas turbine engine vibration diagnostic. Magaz. of Aviat. and Devel. 24-28. [7] Wang, J., Xu, J., Zhang, X., Ren, X., Song, X., Chen, X. 2018. An investigation of surface corrosion behavior of Inconel 718 after robotic belt grinding. Mater. 11, 2440. [8] Liu, C., Ramgopal, T., Li, X. 2019. Hydrogen Embrittlement of Additively Manufactured Inconel 718. Paper presented at the CORROSION 2019, Nashville, Tennessee, USA, March 2019. [9] Engler, Ch.T., Klapper, H.S., Oechsner, M. 2021. On the influence of the microstructure upon the fatigue and corrosion fatigue behavior of UNS N07718. Metals 11, 117. [10]Wang, X., Chou, K. 2019. The effects of stress relieving heat treatment on the microstructure and residual stress of Inconel 718 fabricated by laser metal powder bed fusion additive manufacturing process. J. of Manuf. Proc. 48, 154-163. [11]Zhang, P., Zhu, Q., Hu, C., Wang, C.J., Chen, G., Qin, H. 2015. Cyclic deformation behavior of a nickel-base superalloy under fatigue loading. Mat. and Design, 69, 12-21. [12]Sui, S., Zhong, Ch., Chen, J., Gasser, A., Huang, W., Schleifenbaum, J.H. 2018. Influence of solution heat treatment on microstructure and tensile properties of Inconel 718 formed by high-deposition-rate laser metal deposition. J. of Alloy and Comp. 740, 389-399. [13]Tucho, W.M., Hansen, V. 2019. Characterization of SLM-fabricated Inconel 718 after solid solution and precipitation hardening heat treatments. J. of Mat. Scie. 54, 823–839. [14]Popovich, A.A., Sufiiarov, V.Sh., Polozov, I.A., Borisov, E.V. 2015. Microstructure and mechanical properties of Inconel 718 produced by SLM and subsequent heat treatment. Key Eng. Mat. 651-653, 665-670. [15]Guzmán Tapia, M., Dominguez Almaraz, G.M., Bermúdez Reyes, B., Zuñiga Tello, I.F, , Ruiz Vilchez, J.A. 2021. Failure analysis on pre corroded specimens of Inconel alloy 718, under ultrasonic fatigue tests at room temperature. Eng. Fail. Anal. 120, 105064. [16] Preuss, M., Withers, P.J., Baxter, G.J. 2006. A comparison of inertia friction welds in three nickel base superalloys. Mater. Sci. Eng. A. 437, 38-45. [17] Hari Krishna, E., Prasad, K., Singh, V., Kumar, V. 2015. A comparative evaluation of low cycle fatigue behavior of conventional and modified INCONEL 718. Transact. of The Indian Instit. of Metals, 63, 515-516. [18] Mahobia, G.S., Paulose, N., Sreekanth, K., Mannan, S.L., Sudhakar Rao, G., Singh, V. 2015. Effect of saline Environment on LCF Behavior of Inconel 718 at 550 º C. J. Mater. Eng. Perform. 24, 338-344. [19] Wanhill, R.J.H. 2004. Fatigue of Air Supply Manifold Support Rod in Military Jet Engines. J. of Failure Anal. and Prev. 4(1), 53-61. [20] Reicman, S., Duhl, D.N., Maurer, G., Antolovich, C., Lund C. 1998. Proceedings of the Sixth International Symposium on Superalloys, Chamption, PA, USA, TMS, Warrendale, PA, USA, 3-12.
Made with FlippingBook Ebook Creator