Microstructural Characterization of Inconel 718 for Future Ultrasonic Fatigue Testing-Reference-Cited by-同舟云学术

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Microstructural Characterization of Inconel 718 for Future Ultrasonic Fatigue Testing

Published:2017-10-21 Issue: Volume: Page:3-16
ISSN:
Container-title:Proceedings of the Symposium of Aeronautical and Aerospace Processes, Materials and Industrial Applications
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Author:

Guzmán-Tapia Manuel,Domínguez Almaraz Gonzalo Mariano,Zúñiga Tello Ishvari Fernanda,Gutiérrez Martínez Alberto,Verduzco Juárez Julio Cesar

Publisher

Springer International Publishing

Link

http://link.springer.com/content/pdf/10.1007/978-3-319-65611-3_1

Reference20 articles.

1. Mazur, Z., Luna-Ramírez, A., Islas, J. A., & Campos-Amezcua, A. (2005). Failure analysis of a gas turbine blade made of Inconel 738LC. Engineering Failure Analysis, 12, 474–486. doi: 10.1016/j.engfailanal.2004.10.002 .

2. Kargarnejad, S., & Djavanroodi, F. (2012). Failure assessment of Nimonic 80A gas turbine blade. Engineering Failure Analysis, 26, 211–219. http://dx.doi.org/10.1016/j.engfailanal.2012.05.028 .

3. Yu-jiang, X., Mao-cai, W., Ge, Z., & Min, C. (2006). Analysis of superalloy turbine blade tip cracking during service. Engineering Failure Analysis and Prevention, 13, 1429–1436. doi.org/ 10.1016/j.engfailanal.2005.07.022 .

4. Kosieniak, E., Biesiada, K., Kaczorowsky, J., & Innocenti, M. (2012). Corrosion failure in gas turbine hot components. Journal of Failure Analysis and Prevention, 12, 330–337. doi: 10.1007/s11668-012-9571-3 .

5. Blachnio, J. (2011). Analysis of causes of decohesion of a gas turbine blade made of EI867-WD alloy. Aircraft Engineering and Aerospace Technology, 83, 14–20. doi: 10.1108/00022661111119874 .

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1. Investigating laser power in AM-LMD process on the Inconel 718 powder deposited profile microstructure, aiming to repair gas turbine blades;Canadian Metallurgical Quarterly;2024-06-18

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