Journal of Chemical Engineering and Materials Science
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Article Number - 438B1FC66341

Vol.8(6), pp. 46-65 , September 2017
DOI: 10.5897/JCEMS2016.0282
ISSN: 2141-6605

Full Length Research Paper

Failure of Nickel-based super alloy (ME3) in aerospace gas turbine engines

  • Anvari
  • Department of Mechanical and Aerospace Engineering, University of Missouri-Columbia, Columbia, Missouri, U.S.A.
  • Google Scholar

 Received: 28 December 2016  Accepted: 18 July 2017  Published: 31 October 2017

Copyright © 2017 Author(s) retain the copyright of this article.
This article is published under the terms of the Creative Commons Attribution License 4.0

The significant goal of this study is to develop a system to determine the margin of safety for ME3 super alloy in aerospace gas turbine engines. This margin of safety can be defined as critical temperature, force stress, exposure time, and cycles. In this research, by applying analytical solutions and using experimental data, equations are obtained to predict the life of a nickel-base super alloy in aerospace gas turbine engines. The experimental data that are applied to obtain the equations are achieved by gas turbine environment simulation experiments. This environment is contained with mechanical cycles at high temperature. The results that are achieved by these solutions are compared with the data from an experiment on a composite material. This comparison has proved that the results of this study seem logical. Ultimately, by employing of convex, concave, and linear equations, many results to predict the life of ME3 are obtained. Main reasons in ME3 failure at gas turbine engine environment is determined by this method. Based on the results of this research, the most important cause of ME3 failure is due to maximum mechanical force at high temperatures close to 763°C.

Key words: Failure, nickel-base super alloy, gas turbine engines, mechanical fatigue, high temperature.

Adair BS (2013). Characterization and modeling of thermo-mechanical fatigue crack growth in a single crystal superalloy, Ph.D. thesis, Georgia institute of technology, USA.


Anvari A (2014). Fatigue life prediction of unidirectional carbon fiber/epoxy composite in earth orbit. Int. J. Appl. Math. Mech. 10(5):58-85.


Anvari A (2016). Friction coefficient variation with sliding velocity in copper with copper contact. Periodica Polytech. Mech. Eng. 60(3):137-141.


Anvari A (2017). Crack growth as a function of temperature variation in carbon fiber/epoxy. J. Chem. Eng. Mater. Sci. 8(3):17-30.


Anvari A (2017a). Effect of nano-carbon percentage on properties of composite materials. J. Chem. Eng. Mater. Sci. 8(4):31-36.


Anvari A (2017b). Fatigue life prediction of unidirectional carbon fiber/epoxy composite on Mars. J. Chem. Eng. Mater. Sci. Under press.


Adibnazari S, Anvari A (2017). Frictional effect on stress and displacement fileds in contact region. J. Mech. Eng. Res. 9(4):34-45.


Assoul Y, Benbelaid SV, Zeravcic VS, Bakic G, Dukic M (2008). Life estimation of first stage high pressure gas turbine blades. Scientific Technical Rev. 58(2):8-13.


Basan R, Franulovic M, Krizan B (2010). On estimation of Basquin-Coffin-Manson fatigue parameters of low-alloy steel AISI4140, 14th International Research/Expert Conference "Trends in the development of machinery and associated technology", (TMT 2010, Mediterranean Cruise). pp. 453-456.


Bhattacharjee A (2013). Elastostatic problem of a series of collinear cracks in an orthotropic medium. Int. J. Appl. Math. Mech. 9(20):81-97.


Chen DC, You CS (2015). Fracture criterion for the tensile test of 7075 aluminum allo. J. Strength Mater. 47(1):122-127.


El-Sayed AF (2017). Aircraft Propulsion and Gas Turbine Engines, (CRC Press, Taylor & Francis Group. P 496.


Gabb P, Telesman J, O'Connor K, Kantzos PT (2002). Characterization of the temperature capabilities of advanced disk alloy ME3, Glenn Research Center, Cleveland, Ohio1, Ohio aerospace institute, Brook park, Ohio2.


Gao Y, Kumar M, Nalla RK, Ritchie RO (2005). High-cycle fatigue of Nickel-based superalloy ME3 at ambient and elevated temperatures: role of grain-boundary engineering. Metallurg. Mater. Transactions A, 36A:3325-3329.


Gao Y, Stolken JS, Kumar M, Ritchie RO (2007). High-cycle fatigue of nickel-base super alloy Rene 104 (ME3): Interaction of microstructurally small cracks with grain boundaries of known character, Acta Materialia. 55:3155-3167.


Getsov LB, Semenov AS, Semenov SG, Tikhomirova EA, NPO CKTI, Saint-Petersburg state polytechnical university and JSK Klimov (2014). Experiments and failure criteria for single crystal alloys of gas turbine engine under static and thermocyclic loading, 29th Congress of the International Council of the Aeronautical Sciences, (St Petersburg, Russia, pp. 1-6.


Jiang R, Everitt S, Gao N, Soady K, Brooks JW, Reed PAS (2015). Influence of oxidation on fatigue crack initiation and propagation in turbine disc alloy N18, Materials research group.


Liu S, Nairn JA (1990). Fracture mechanics analysis of composite microcracking: experimental results in fatigue, in Proceeding of the 5th Technical Conference on Composite Materials, American Society of Composites, (East Lansing, Michigan). pp. 287-295.


Maciejewski K (2013). The role of microstructure on deformation and damage mechanisms in a Ni-based superalloy at elevated temperatures, Ph.D. thesis, University of Rhode Island.


Misra A (2012). Durability challenges for next generation of gas turbine engine material, NASA Glenn research center, Cleveland, OH 44134.


Nembach E, Neite G (1985). In progress in materials science (ed Christian JW, Haasen P, Massalski TB). Pergamon press Oxford 29:177.


Roy SS, De J (2014). Interfacial crack problems in dissimilar bonded materials. Int. J. Appl. Math. Mech. 10(7):16-27.


Sawant A, Tin S, Zhao JC (2008). High temperature nanoindentation of ni-base super alloys, TMS (The Minerals, Metals & Materials Society).


Winston MR, Brooks JW (2008). Advanced high temperature materials: aeroengine fatigue, Physical sciences department, defence science and technology laboratory, Porton Down, Salisbury, SP4 0JQ, UK1, QinetiQ Ltd., Cody Technology Park, Farnborough, GU14 0LX, UK2.


Xue F, Yu WW, Yu M, Liu W, Shu GG (2015). Long-term aging effect on the crack growth in the main circulating pump casing material. J. Strength Mater. 47(1):100-107.


Yang B, Ma BQ, Zhao YX, Xiao SN (2015). Short fatigue crack growth at different maintenance times for LZ50 steel. J. Strength Mater. 47(1):114-121.


Zaretsky EV, Litt JS, Hendricks RC, Soditus SM (2012). Determination of turbine blade life from engine field data, NASA Glenn researchcenter, Cleveland, Ohio 441351, United airlines maintenance, San Francisco, California 941282.



APA Anvari, A. (2017). Failure of Nickel-based super alloy (ME3) in aerospace gas turbine engines. Journal of Chemical Engineering and Materials Science, 8(6), 46-65.
Chicago A. Anvari. "Failure of Nickel-based super alloy (ME3) in aerospace gas turbine engines." Journal of Chemical Engineering and Materials Science 8, no. 6 (2017): 46-65.
MLA A. Anvari. "Failure of Nickel-based super alloy (ME3) in aerospace gas turbine engines." Journal of Chemical Engineering and Materials Science 8.6 (2017): 46-65.
DOI 10.5897/JCEMS2016.0282

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