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http://dx.doi.org/10.12989/amr.2019.8.1.011

Analysis and structural design of various turbine blades under variable conditions: A review  

Saif, Mohd (Department of Mechanical Engineering, Sam Higginbottom University of Agriculture Technology & Sciences)
Mullick, Parth (Department of Mechanical Engineering, Sam Higginbottom University of Agriculture Technology & Sciences)
Imam, Ashhad (Department of Civil Engineering, Sam Higginbottom University of Agriculture Technology & Sciences)
Publication Information
Advances in materials Research / v.8, no.1, 2019 , pp. 11-24 More about this Journal
Abstract
This paper presents a review study for energy-efficient gas turbines (GTs) with cycles which contributes significantly towards sustainable usage. Nonetheless, these progressive engines, operative at turbine inlet temperatures as high as $1600^{\circ}C$, require the employment of highly creep resistant materials for use in hotter section components of gas turbines like combustion chamber and blades. However, the gas turbine obtain its driving power by utilizing the energy of treated gases and air which is at piercing temperature and pushing by expanding through the several rings of steady and vibratory blades. Since the turbine blades works at very high temperature and pressure, high stress concentration are observed on the blades. With the increasing demand of service, to provide adequate efficiency and power within the optimized level, turbine blades are to be made of those materials which can withstand high thermal and working load condition for longer cycle time. This paper depicts the recent developments in the field of implementing the best suited materials for the GTs, selection of proper Thermal Barrier Coating (TBC), fracture analysis and experiments on failed or used turbine blades and several other designing and operating factors which are effecting the blade life and efficiency. It is revealed that Nickel based Superalloys were promising, Cast Iron with Zirconium and Pt-Al coatings are used as best TBC material, material defects are the foremost and prominent reason for blade failure.
Keywords
gas turbine blade; turbine inlet temperature; thermal barrier coating; finite element analysis; failure analysis; blade efficiency; metallurgical analysis;
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1 Mazarbhuiya, H.M.S.M. and Pandey, K.M. (2017), "Steady state analysis of high pressure gas turbine blade using finite element analysis", Mater. Sci. Eng. IOP Conference Series, 225(1), 012113. https://doi.org/10.1088/1757-899X/225/1/012113   DOI
2 Ali, R., Shehbaz, T. and Bemporad, E. (2018), "Investigation on Failure in Thermal Barrier Coating on Gas Turbine First-Stage Rotor Blade", J. Fail. Anal. Prevention, 18(5), 1062-1072. https://doi.org/10.1007/s11668-018-0530-5   DOI
3 Almasi, A., Avval, H.B. and Ahmadi, P. (2011), "Thermodynamic modelling, energy and exergoeconomic analysis and optimization of marsh gas turbine plant", Proceeding of The Global Conference on Global Warming, Lisbon, Portugal, July.
4 Begum, F., Reddy, V.R. and Ramanjaneyulu, S. (2016), "Design and thermal analysis of cooling of gas turbine blade through radial holes", Material Today, ICAAMM, 4, 7714-7722. https://doi.org/10.1016/j.matpr.2017.07.106
5 Beghini, M., Bertini, L. and Santus, C. (2017), "High temperature fatigue testing of gas turbine blades", Procedia Structural Integrity, FDMD, 7, 206-213. https://doi.org/10.1016/j.prostr.2017.11.079
6 Bons, J.P. (2010), "A review of surface roughness effect in gas turbine", J. Turbomach., 132 (2), 1-16. https://doi.org/10.1115/1.3066315
7 Brandao, P., Infante, V. and Deus, A.M. (2016), "Thermo-mechanical modelling of a high pressure turbine blade of an airplane gas turbine engine", Proceedings of the 15th Portuguese Conference on Fracture, Paco de Arcos, Portugal, February.
8 Caron, P. and Khan, T. (1999), "Evolution of Ni-based superalloys for single crystal gas turbine blade application", Aerosp. Sci. Technol., 3, 513-523. https://doi.org/10.1016/S1270-9638(99)00108-X   DOI
9 Marcin, J.D. and Gupta, D.K. (1994), "Protective coating in the gas turbine engine", Surf. Coat. Technol., 68/69, 1-9. https://doi.org/10.1016/0257-8972(94)90129-5   DOI
10 Carter, T.J. (2005), "Common failures in gas turbine blade", Eng. Fail. Anal., 12, 237-247. https://doi.org/10.1016/j.engfailanal.2004.07.004   DOI
11 Casadei, F., Bertoldi, K. and Clarke, D.R. (2013), "Finite element study of multi-modal vibration damping for thermal barrier coating applications", Comput. Mater. Sci., 79, 908-917. https://doi.org/10.1016/j.commatsci.2013.07.027   DOI
12 Chintala, G. and Gudimetla, P. (2014), "Optimum material evaluation for gas turbine using RE and FEA", Proceedings of the 12th Global Conference on Manufacturing and Management, Vellore, India, December.
13 Chung, H., Sohn, H. and Park, J.S. (2016), "Thermo-structural analysis of the cracks on the gas turbine vane segment having multiple airfoils", Energy, 118, 1275-1285. https://doi.org/10.1016/j.energy.2016.11.005   DOI
14 Aabid, A. and Khan, S.A. (2018), "Optimization of heat transfer on thermal barrier coated gas turbine blade", Mater. Sci. Eng., 370 (1), 1-9. https://doi.org/10.1088/1757-899X/370/1/012022   DOI
15 Al Ali, A.R. and Janajreh, I. (2015), "Numerical simulation of turbine blade cooling via jet impringement", Proceeding of the 7th International Conference on Applied Energy, Abu Dhabi, United Arab Emirates, March.
16 Cowles, B.A. (1996), "High cycle fatigue in aircraft gas turbines - an industry perspective", Int. J. Fracture, 80, 147-163. https://doi.org/10.1007/BF00012667   DOI
17 Rani, S., Agrawal, A.K. and Rastogi, V. (2017), "Failure analysis of a first stage IN738 gas turbine blade tip cracking in a thermal power plant", Case Studies Eng. Fail. Anal., 8, 1-10. https://doi.org/10.1016/j.csefa.2016.11.002   DOI
18 Mazur, Z., Luna-Ramirez, A. and Islas, J.A. (2005), "Failure analysis of a gas turbine blade made up of Inconel 738LC alloy", Eng. Fail. Anal., 12, 474-486. https://doi.org/10.1016/j.engfailanal.2004.10.002   DOI
19 Mirzaei, M. and Karimi, R. (2001), "Stress analysis and life assessment of a gas turbine blade", ICF100312OR.
20 Poursaeidi, E., Aieneravaie, M. and Mohammadi, M.R. (2008), "Failure analysis of second stage blade in a gas turbine engine", Eng. Fail. Anal., 15, 1111-1129. https://doi.org/10.1016/j.engfailanal.2007.11.020   DOI
21 Rao, V.N.B., Kumar, I.N.N. and Prasad, K.B. (2014), "Failure analysis of gas turbine blades in a gas turbine engine used for marine applications", Int. J. Eng. Sci. Technol., 6(1), 43-48.   DOI
22 Ravindra, K. and Raju, P.V.D. (2017), "Modelling and analysis of gas turbine rotor blade", Int. Res. J. Eng. Technol., 4(12), 141-146.
23 Reyhani, M.R., Alizadeh, M., Fathi, A. and Khaledi, H. (2013), "Turbine blade temperature calculation and life estimation- a sensitive analysis", Propuls. Power Res., 2(2), 148-161. https://doi.org/10.1016/j.jppr.2013.04.004   DOI
24 Saini, A.K. and Shandil, N. (2015), "Thermal analysis of partially stabilised zirconia and lanthanum magnesium Hexa-aluminate as Thermal Barrier coating over Hastealloy X gas turbine blade", J. New Technol. Mater., 5(2), 8-19. https://doi.org/10.12816/0019427   DOI
25 Ujade, G.D. and Bhambere, M.B. (2014), "Review of structural and thermal analysis of gas turbine", Int. J. Mech. Eng. Rob. Res., 3(2), 347-352.
26 Saini, A.K., Das, D. and Pathak, M.K. (2012), "Thermal barrier coating- application, stability and longevity aspect", Procedia Eng., 38, 3173-3179. https://doi.org/10.1016/j.proeng.2012.06.368   DOI
27 Salehnasab, B., Hajjari, E. and Mortazavi, S.A. (2017), "Failure assessment of the first stage blade of a gas turbine engine", Transact. Indian Inst. Metals, 70(8), 1-8. https://doi.org/10.1007/s12666-016-1031-4   DOI
28 Tong, F., Gou, W. and Li, L. (2018), "Thermo-mechanical stress analysis for gas turbine blade with cooling structures", Multidiscipl. Model. Mater. Struct., 14(4), 722-734. https://doi.org/10.1108/MMMS-08-2017-0081   DOI
29 Xue, X., Yu, Y. and Xie, J. (2017), "The influence of the nozzle diameters on the interaction characteristics of combustion gas jets and liquid", Defence Technology, 13, 257-262. https://doi.org/10.1016/j.dt.2017.05.016   DOI
30 Zhu, J. and Ma, K. (2014), "Microstructure and mechanical properties of thermal barrier coating at $1400^{\circ}C$ treatment", Theoret. Appl. Mech. Lett., 4, 1-5. https://doi.org/10.1063/2.1402108
31 Gurajarapu, N., Rao, V.N.B. and Kumar, I.N.N. (2014), "Selection of a suitable material and failure investigation on a turbine blade of marine gas turbine engine using Reverse Engineering and FEA Techniques", Int. J. u- and e- Service, Sci. Technol., 7(6), 297-308.   DOI
32 Hou, J., Wicks, B.J. and Antoniou, R.A. (2002), "An investigation of fatigue failures of turbine blades in a gas turbine engine by mechanical analysis", Eng. Fail. Anal., 9, 201-211. https://doi.org/10.1016/S1350-6307(01)00005-X   DOI
33 Huda, Z. (2009), "Metallurgical failure analysis for a blade failed in a gas turbine engine of a power plant", Mater. Des., 30, 3121-3125. https://doi.org/10.1016/j.matdes.2008.11.030   DOI
34 Kim, K.M., Yun, N. and Jeon, Y.H. (2010), "Conjugated heat transfer and temperature distributions in a gas turbine combustion liner under base-load operation", J. Mech. Sci. Technol., 24 (9), 1939-1946. https://doi.org/10.1007/s12206-010-0625-8   DOI
35 Huda, Z. (2017), "Energy-efficient gas-turbine blade-material technology - a review", Mater. Technol., 51(3), 355-361. https://doi.org/10.17222/mit.2015.196
36 Kanesund, J., Brodin, H. and Johansson, S. (2019), "Hot corrosion influence on deformation and damage mechanisms in turbine blade made of IN-792 during service", Eng. Fail. Anal., 96, 118-129. https://doi.org/10.1016/j.engfailanal.2018.10.004   DOI
37 Khawaja, H. and Motamedi, M. (2014), "Selection of high performance alloy for gas turbine blade using multiphysics analysis", Int. J. Multiphys. Volume, 8(1), 91-100. http://dx.doi.org/10.1260/1750-9548.8.1.91   DOI
38 Kini, C.R., Shenoy, B.S. and Sharma, N.Y. (2014), "Thermo-structural analysis of HP stage gas turbine blades having helicoidal cooling ducts", Int. J. Adv. Mech. Aeronaut. Eng., 1(2), 57-60.
39 Kumar, R.R. and Pandey, K.M. (2016), "Static structural analysis of gas turbine blade", J. Basic Appl. Eng. Res., 3(3), 276-281. https://doi.org/10.1088/1757-899X/225/1/012102
40 Kumar, G.M. and Rose, J.B.R. (2015), "Comparative analysis of advanced gas turbine blade materials used in aircraft application", Int. J. Innov. Res. Technol. Sci. Eng., 1(4), 34-43.
41 Li, B., Fan, X., Li, D. and Jiang, P. (2017), "Design of thermal barrier coatings thickness for gas turbine blade based on Finite Element Analysis", Report No. ID 2147830; State Key Laboratory for Strength and Vibration of Mechanical Structures, School of Aerospace Engineering, Xi'an Jiaotong University, Xi'an, China.
42 Madhu, P. (2016), "Stress analysis and life estimation of gas turbine blisk for different materials of a jet engine", Int. J. Sci. Res., 5(6), 1103-1107. http://dx.doi.org/10.21275/v5i6.NOV164440