Analysis of Cracking Process in Conditions of High-Temperature Creep of Castings Form the Modified Superalloy IN-713C

Article Preview

Abstract:

mpact of complex modification and filtration during pouring into moulds on durability has been evaluated in this study in conditions of high-temperature creep of castings made from nickel superalloy IN-713C post production rejects. The conditions of initiation and propagation of cracks in the specimens were analysed with consideration of morphological properties of material macro-, micro-and substructure. It has been demonstrated that in conditions of high-temperature creep at temperature 980°C with stress σ =150 MPa creep resistance of the IN-713C superalloy increases significantly with the increase of macrograin size. Creep resistance of specimens made of coarse grain material was significantly higher than the resistance of fine grain material.

You might also be interested in these eBooks

Info:

Periodical:

Solid State Phenomena (Volume 212)

Pages:

247-254

Citation:

Online since:

December 2013

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2014 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] Y. Tamarin, Protective coatings for turbine blades, ASM International, The Materials Information Society, Materials Park, Ohio, (2002).

Google Scholar

[2] A.K. Koul, V.R. Parameswaran, J-P. Immarigeon, W. Wallace, Advances in High Temperature Structural Materials and Protective Coatings, A Publication from National Research Council of Canada, Ottawa, (1994).

Google Scholar

[3] J. Sieniawski, Criteria and methods of assessment of materials intended for elements of aircraft turbine engines, Ed. Oficyna Wyd. Politechniki Rzeszowskiej, (1995).

Google Scholar

[4] Seon-gab Kim, Young-ha Hwang, Tae-gu Kim, Chang-min Shu, Failure analysis of J85 engine turbine blades, Engineering Failure Analysis, 15 (2008) 394-400.

DOI: 10.1016/j.engfailanal.2007.01.015

Google Scholar

[5] Haijun Tang, Dashu Cao, Hongyu Yao, Mingli Xie, Ruichun Duan, Fretting fatigue failure of an aero engine turbine blade, Engineering Failure Analysis, 16 (2009) 2004-(2008).

DOI: 10.1016/j.engfailanal.2008.07.010

Google Scholar

[6] A. Strang, E. Lang, R. Pichoir, Practical implications of the use of aluminide coatings for the corrosion protection of superalloys in gas turbines, Materials Substitution and Recycling, AGARD Conference Proceedings SMP 356 (1983).

Google Scholar

[7] A. Strang, High Temperature Properties of Coated Superalloys, Behaviour of High Temperature Alloys in Aggressive Environmeents, The Metals Society, London, UK (1980) 595-611.

Google Scholar

[8] M. Cieśla, Durability of ŻS6U nickel superalloy with aluminide protective layer in thermal and mechanical load conditions, Monograph, Ed. Wydawnictwo Pol. Śl. (in polish), (2009).

Google Scholar

[9] J. Okrajni, M. Cieśla, L. Swadźba, High-Temperature Low-Cycle Fatigue and Creep Behaviour of Nickel-Based Superalloys with Heat-Resistant Coatings, Fatigue and Fractute of Materials and Engineering Structures, 21 (1998) 947-954.

DOI: 10.1046/j.1460-2695.1998.00090.x

Google Scholar

[10] R. Castillo R., A.K. Koul, J-P. Immarigeon, The Effects of Sernice Exposure on the Creep Properties of Cast IN-738LC Subjected to Low Stress High Temperature Creep Conditions, Superalloys 88, S. Reichman, D.N. Duhl, G. Maurer, S. Antolovich, C. Lund, Eds., The Metallurgical Society, (1988).

DOI: 10.7449/1988/superalloys_1988_805_814

Google Scholar

[11] H.J. Frost, M.F. Ashby, Deformation-Mechanism Maps. The plasticity and creep of metals and ceramics, Oxford, Pergamon press (1982) 166.

Google Scholar

[12] M. Zielińska, J. Sieniawski, M. Poreba, Microstructure and mechanical properties of high temperature creep resisting superalloy Rene 77 modified CoAl2O4, Archives of Materials Science and Engineering, 28 (2007) 629-632.

Google Scholar

[13] M. Zielińska, J. Sieniawski, M. Wierzbińska, Effect of modification on microstructure and mechanical properties of cobalt casting superalloy, Archives of Metallurgy and Materials, 53 (2008) 887-893.

Google Scholar

[14] F. Binczyk, J. Śleziona, Effect of modification on the mechanical properties of IN-713C alloy, Archives of Foundry Engineering, 10 (2010) 195-198.

Google Scholar

[15] F. Binczyk, J. Śleziona, Mechanical properties and creep resistance behaviour of IN-713C alloy castings, Archives of Foundry Engineering, 10 (2010) 9-13.

Google Scholar

[16] F. Binczyk, J. Śleziona, P. Gradoń, Modification of the macrostructure of nickel superalloys with cobalt nanoparticles, Composites, 1 (2011) 49-55.

Google Scholar

[17] F. Binczyk, J. Śleziona, P. Gradoń, Ceramic filters for bulk inoculation of nickel alloy castings, Archives of Foundry Engineering, 11 (2011) 29-33.

Google Scholar

[18] F. Binczyk, J. Śleziona, The ATD thermal analysis of selected nickel superalloys, Archives of Foundry Engineering, 10 (2010) 13-19.

Google Scholar

[19] M. Cieśla, F. Binczyk, M. Mańka, Impact of surface and volume modification of nickel superalloys IN-713C and MAR-247 on high temperature creep resistance, Archives of FoundaryEngineering, 12 (2012) 17-24.

DOI: 10.2478/v10266-012-0101-2

Google Scholar

[20] F. Binczyk, P. Gradoń, M. Mańka, Mechanical Properties And Creep Resistance of Nickel Alloys After Complex Modification And Double Filtration, Archives of FoundaryEngineering, 12 (2012) 5-8.

DOI: 10.2478/v10266-012-0026-9

Google Scholar

[21] J. Wyrzykowski, E. Pleszakow, J. Sieniawski, Deformation and cracking of metals (in polish), Ed. WNT, Warszawa, (1999).

Google Scholar

[22] M.Ł. Bernsztejn, W.A. Zajmowskij, Structure and mechanical properties of metals (in polish), WNT, Warszawa, (1973).

Google Scholar

[23] F.R.N. Nabarro, C.M. Cress, P. Kotschy, Thermodynamicdriving forse for rafting in superalloys, Acta materialia 44 (1996) 3189-3198.

DOI: 10.1016/1359-6454(95)00423-8

Google Scholar

[24] A. Epishin, T. Link, Mechanism of high temperature creep of nickel-based superalloys under low applied stresses, Philosophical Magazine 84 (2004) 1979-(2000).

DOI: 10.1080/14786430410001663240

Google Scholar