Analysis and Simulation of The Effects That Cause Fatigue in the Frame Structure 308 of the Uh-60 Helicopter

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Jimmy Anderson Florez Zuluaga
Andrés Márquez Atrio
Andres Ayala Angel
Carlos Jahir Carreño Hernández


Introduction: This is a product of the research “Study of operational maneuvers for the detection of structural fatigue in the UH-60 helicopter”, developed through COLCIENCIAS project number 56742, at the Colombian Air Force-Aerospace Technology Development Centre for the Defense - CETAD, during 2017-2019.

The objective of the project was to design and develop a system that would allow studying the strain generated by operational maneuvers and the relation between them and the structural fatigue of frame 308 of the UH-60.

Methodology: The project was based on the integration of strain and vibration data from the helicopter’s frame 308 instrumentalization to development a relevant simulation and analysis.

Results: In the first instance, the data collection was synchronized with the flight maneuvers, identifying the strain generated in each position. This helped establish the range of the loads on the beam during operational maneuvers.

Conclusions: In this project, a series of sensors and data acquisition and recording devices were integrated into the aircraft in order to identify the maneuvers that generate strain in frame 308, based on the use of the manufacturer's manuals and engineering processes.

Originality: This document formulates data from possible situations for the first time, because there is no history of literature on the study, characterization or materials on frame 308 of the UH-60 helicopter.

Limitations: Insufficient public information about the UH-60 aircraft.


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J. A. Florez Zuluaga, A. Márquez Atrio, A. Ayala Angel, and C. J. Carreño Hernández, “Analysis and Simulation of The Effects That Cause Fatigue in the Frame Structure 308 of the Uh-60 Helicopter”, ing. Solidar, vol. 15, no. 29, Sep. 2019.
Research Articles


[1] A. Faccenda, R. Canadale, and S. Sweikar, “Integration of Externally Carried Weapon Systems with Military Helicopters (L’Integration des Systemes d’Armes Transportes en Charge Externe sur les Helicopters Militaires),” 1990, pp. 58-65.

[2] Army Science, Conference Proceedings, 12-15 June 1990, vo. 2, 1990, pp. 474-486.

[3] Helicopter/Weapon System Integration (l’Integration des systems d’armes des helicopters), 1997, pp. 36-56

[4] Williamsburg, B. D. Davidson, J. G. Ratcliffe, and M. W. Czabaj, Proceedings of the American Society for Composites, Thirty-First Technical Conference : September 19-21, 2016, Williamsburg Lodge, Williamsburg, VA. .CD

[5] S. K. Yang and T. S. Liu, “State estimation for predictive maintenance using Kalman filter,” Reliab. Eng. Syst. Saf., vol. 66, no. 1, pp. 29–39, 1999. [Online]. doi:

[6] Department of the Army Headquarters, General aircraft maintenance manual. 1970, CH4-p, pp. 474-486.

[7] C. L. Kee, “Military Operations Research Society Symposium (70th): Military Operations Research at the Next Frontier. Held at Fort Leavenworth, Kansas on 18-20 June 2002. Final Program and Book of Abstracts,” 2002.

[8] J. I. Group, “UH‐60S ORDERED,” Jane’s Def. Wkly, 1990.

[9] J. I. Group, “Switchboards in the sky,” Int. Def. Rev., 2001.

[10] G. R. Humphrey and R. W. Martin, “1998 Technology Showcase. JOAP International Condition Monitoring Conference,” 1998, pp. 215-224.

[11] “dod Modeling and Simulation (M&S) Glossary,” 1998, pp. 8-182

[12] G. S. Frankel, “Corrosion Degradation of Coated Aluminum Alloy Systems through Galvanic Interactions,” 2017, pp. 2-9

[13] A. D. 222599 Number, S-70A-9 Black Hawk Helicopter: Internal Cracking Investigation. Department of Defense, 1997, pp. 65,67,105,116.

[14] M. R. Mofakhami and J. Pinsonnault, “A prospective for Structural Health Monitoring system implementation on civil aircraft,” 2011 Cansmart Cinde Izfp, no. November, pp. 1-7, 2011.

[15] U. G. Goranson, “Fatigue issues in aircraft maintenance and repairs,” Int. J. Fatigue, vol. 20, no. 6, pp. 413–431, Jul. 1998. doi:

[16] B. Kamsu-Foguem, “Knowledge-based support in Non-Destructive Testing for health monitoring of aircraft structures,” Adv. Eng. Informatics, vol. 26, no. 4, pp. 859–869, 2012. [Online]. doi:

[17] A. Katunin, K. Dragan, and M. Dziendzikowski, “Damage identification in aircraft composite structures: A case study using various non-destructive testing techniques,” Compos. Struct., vol. 127, pp. 1–9, Sep. 2015. . [Online]. doi:

[18] F.-K. Chang, United States. Air Force. Office of Scientific Research., United States. Army Research Office., and National Science Foundation (U.S.), Structural health monitoring 2003 : from diagnostics & prognostics to structural health management : proceedings of the 4th International Workshop on Structural Health Monitoring, Stanford University, Stanford, CA, September 15-17, 2003. Destech Pub, 2003, pp. 16,20,34

[19] X. J. Sun Bo, Kang Rui, “Research and application of the prognostic and health management system,” Systems Engineering and Electronics," 2007. [Online]. Available:

[20] M. Q. Le et al., “Review on energy harvesting for structural health monitoring in aeronautical applications,” Prog. Aerosp. Sci., vol. 79, pp. 147–157, Nov. 2015. [Online]. doi:

[21] A. Standard, “Standard test methods for tension testing of metallic materials metric,” Annu. B. ASTM Stand., vol. 3, pp. 57–72, 2004. [Online]. doi:

[22] ASM International, ASM International Handbook Committee (1992). Properties and Selection Nonferrous Alloys and Special – Purpose Materials.ORG: Autor.pp451-462., vol. 2. 1992. [Online]. doi:

[23] D. R. Askeland, “Ciencia e Ingenieria de los Materiales - Donald Askeland - 3edicion.pdf,” p. 737, 1998.

[24] D. O. T. A. Headquarters, “Chapter 6 Maintenance Instructions,” In Tm 1-1520-237-23-6 Aviation Unit And Intermediate Maintenance For Army Models Uh-60a, Uh-60l, Eh-60a, Uh-60q And Hh-60l Helicopters, no. April, 2006, pp: 6,114,115,180,181,189-195

[25] Fuerza Aerea Colombiana, “Manual de Mantenimiento Aeronáutico-MAMAE,” Man. Manten., vol. 4.1.1-0, pp. 307–309, 2016.

[26] Fuerza Aerea Colombiana, Manual Para El Transporte De Mercancías Peligrosas Por Vía Aérea Para La Aviación De Estado. 2016, pp:36-40.

[27] R. K. J. Budynas, “Diseño en Ingenieria Mecanica de Shigley,” p. 933-956, 2008.
[28] B E. Russell Johnston and Ferdinand P. Beer, Mecánica Vectorial Para Ingenieros. 2007, pp. 285-345.

[29] K. A. Latorella and P. V Prabhu, “A review of human error in aviation maintenance and inspection,” Int. J. Ind. Ergon., vol. 26, no. 2, pp. 133–161, Aug. 2000. [Online]. doi:

[30] A. Unit, I. M. For, G. Information, and E. Description, TM 1-1520-237-23-1 Aviation Unit And Intermediate Maintenance For Equipment Description And Data, no. April. 2006.pp 72-74

[31] Department of Army, TM 1-1520-23-10 “Operator’s Manual for UH-60A UH-60L EH-60A,” no. October, 1996, pp. 384,400.

[32] A. A. A. M. Command, “Dmwr 1-1520-237-3 Airframe Depot Maintenance Work Requirement Containing For Army Models Uh-60a , Eh-60a , And Uh-60l Helicopters Nsn 1520-01-035-0266 NSN 1520-01-082-0686,” no. January 2004, 2003, pp103-111.

[33] D. N. E., Mechanical Behavior of Materials. Norman E.Dowling, 2012, pp. 148-154

[34] Department of Army, “Headquarters, Department of the Army. (2006) Aviation unit and intermediate maintenance for army models UH-60A, UH-60L, EH-60A, UH-60Q and HH- 60L helicopters Chapter 1 General TM 1-1520-237-10,” pp. 72,74,103, 2006.

[35] CETAD, “Informe final proyecto 40176,” 2014.