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Influence of Film-Cooling Hole Arrangement on Mechanical Properties of Cooled Turbine Blade Based on the Crystal Plastic Theory

Published online by Cambridge University Press:  08 August 2019

Y. Lian*
Affiliation:
School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical University, Xi'an 710072, P.R.China.
Z. Xu
Affiliation:
School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical University, Xi'an 710072, P.R.China.
H. Pei
Affiliation:
School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical University, Xi'an 710072, P.R.China.
C. Liang
Affiliation:
School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical University, Xi'an 710072, P.R.China.
Y. Zhang
Affiliation:
School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical University, Xi'an 710072, P.R.China.
Z. Wen
Affiliation:
School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical University, Xi'an 710072, P.R.China.
Z. Yue
Affiliation:
School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical University, Xi'an 710072, P.R.China.
*
*Corresponding author ([email protected])
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Abstract

The crystal plastic theory was used to examine the effect of film-cooling hole arrangements on mechanical properties of cooled turbine blade. The finite element method was used to analyze the maximum von Mises stress and resolved shear stress of an octahedral slip system considering the number of rows, diameter, spacing, and tangential-to-longitudinal hole spacing (h/l) ratio. The different arrangements were found to have a significant influence on the maximum von Mises stress and resolved shear stress. For the triangular arrangement, the von Mises stress and resolved shear stress were highest with double rows, followed by a single row and then triple rows. For the quadrilateral arrangement, the stresses were highest with double rows, followed by triple rows and then a single row. Increasing the spacing or decreasing the diameter reduced the maximum von Mises stress and weakened the multi-hole interference effect. Both the maximum von Mises stress and resolved shear stress decreased with the h/l ratio.

Type
Research Article
Copyright
© The Society of Theoretical and Applied Mechanics 2019 

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References

REFERENCES

Ito, S. et al.Conceptual design and cooling blade development of 1700°C class high-temperature gas turbine”, Journal of Engineering for Gas Turbines & Power, 127, pp. 829842 (2003).Google Scholar
He, K., “Investigations of film cooling and heat transfer on a turbine blade squealer tip”, Applied Thermal Engineering, 110, pp. 630647 (2017).CrossRefGoogle Scholar
Xie, G.N., Liu, J., Ligrani, P.M. and Sunden, B., “Flow structure and heat transfer in a square passage with offset mid-truncated ribs”, International Journal of Heat & Mass Transfer, 71, pp. 4456 (2014).CrossRefGoogle Scholar
Han, J.C., “Turbine blade cooling studies at Texas A&M University: 1980–2004”, Journal of Thermophysics & Heat Transfer, 20, pp. 161187 (2006).CrossRefGoogle Scholar
Sun, W.K., Xu, Y.M., Hu, C.Y. and Liu, X.L., “Effect of film-hole configuration on creep rupture behavior of a second generation nickel-based single crystal superalloys”, Materials Characterization, 130, pp. 298310 (2017).CrossRefGoogle Scholar
Wang, C.H., Zhang, J.Z. and Zhou, J.H., “Optimization of a fan-shaped hole to improve film-cooling performance by RBF neural network and genetic algorithm”, Aerospace Science & Technology, 58, pp. 1825 (2016).CrossRefGoogle Scholar
Fan, X.J., Du, C.H., Li, L. and Li, S., “Numerical simulation on effects of film hole geometry and mass flow on vortex cooling behavior for gas turbine blade leading edge”, Applied Thermal Engineering, 112, pp. 472483 (2016).CrossRefGoogle Scholar
Wen, Z.X., Li, Z.W., Zhang, Y.M., Wen, S.F. and Yue, Z.F., “Surface slip deformation characteristics for perforated Ni-based single crystal thin plates with square and triangular penetration patterns”, Materials Science & Engineering A, 723, pp. 5669 (2018).CrossRefGoogle Scholar
He, K.., “Investigations of film-cooling and heat transfer on a turbine blade squealer tip”, Applied Thermal Engineering, 110, pp. 630647 (2017).CrossRefGoogle Scholar
Ochrymiuk, T., “Numerical prediction of film-cooling effectiveness over flat plate using variable turbulent Prandtl number closures”, Journal of Thermal Science, 25, pp. 280286 (2016).CrossRefGoogle Scholar
Wang, J., Cui, P., Sundén, B. and Vujanoviä, M., “Effects of deposition height and width on film-cooling”, Numerical Heat Transfer, 70, pp. 673687 (2016).CrossRefGoogle Scholar
Nikparto, A. and Schobeiri, M.T., “Experimental investigation of film-cooling effectiveness of a highly loaded turbine blade under steady and periodic unsteady flow conditions”, ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition, Seoul, South Korea (June 13–17, 2016).CrossRefGoogle Scholar
Sarkar, S. and Gupta, P., “Thermal analysis of a turbine blade: Effect of film-cooling and internal convective cooling”, ASME 2015 Gas Turbine India Conference, Hyderabad, India (December 2–3, 2015).CrossRefGoogle Scholar
Wen, Z.X., Pei, H.Q., Yang, H., Wu, Y.W. and Yue, Z.F., “A combined CP theory and TCD for predicting fatigue lifetime in single-crystal superalloy plates with film cooling holes”, International Journal of Fatigue, 111, pp. 243255 (2018).CrossRefGoogle Scholar
Wen, Z.X. et al, “Prediction method for creep life of thin-wall specimen with film cooling holes in Ni-based single-crystal superalloy International”, Journal of Mechanical Sciences, 141, pp. 276289 (2018).CrossRefGoogle Scholar
Rezasoltani, M., Lu, K., Schobeiri, M.T. and Han, J.C., “A combined experimental and numerical study of the turbine blade tip film-cooling effectiveness under rotation condition”, Journal of Turbomachinery, 137, pp. 051009 (2014).CrossRefGoogle Scholar
Chen, A.F., Shiau, C.C. and Han, J.C., “Turbine blade platform film-cooling with simulated swirl purge flow and slash face leakage conditions”, Journal of Turbomachinery, 139, pp. 031012 (2016).CrossRefGoogle Scholar
Forghan, F., Askari, O., Narusawa, U. and Metghalchi, H., “Cooling of turbine blade surface with extended exit holes: Computational suction-side analysis”, Journal of Energy Resources Technology, 138, pp. 051602 (2016).CrossRefGoogle Scholar
Taylor, G.I., “Plastic Strain in Metals”, Our.inst.metals, 62, pp. 307325 (1938).Google Scholar
Taylor, G.I. and Elam, C.F., “The plastic extension and fracture of aluminium crystals”, Proceedings of the Royal Society of London. A, 108, pp. 2851 (1925).Google Scholar
Taylor, G.I. and Elam, C.F., “The distortion of an aluminum crystal during a tensile test”, Proceedings of the Royal Society of London, 102, pp. 643667 (1923).Google Scholar
Asaro, R.J., “Crystal plasticity”, Journal of Applied Mechanics, 50, pp. 921934 (1983).CrossRefGoogle Scholar
Peirce, D., Asaro, R.J. and Needleman, A., “Material rate dependence and localized deformation in crystalline solids”, Acta Metallurgica, 31, pp. 19511976 (1983).CrossRefGoogle Scholar
Hutchinson, J.W., “Bounds and self-consistent estimates for creep of polycrystalline materials”, Proceedings of the Royal Society A: Mathematical, Physical and Engineering Sciences, 348, pp. 101127 (1976).Google Scholar
Pan, J. and Rice, J.R., “Rate sensitivity of plastic flow and implications for yield-surface vertices”, International Journal of Solids & Structures, 19, pp. 973987 (1983).CrossRefGoogle Scholar
Asaro, R.J., “Micromechanics of crystals and polycrystals”, Advances in Applied Mechanics, 23, pp. 1115 (1983).CrossRefGoogle Scholar
Wen, Z.X., Zhang, D.X., Li, S.W., Yue, Z.F. and Gao, J.Y., “Anisotropic creep damage and fracture mechanism of nickel-base single crystal superalloy under multiaxial stress”, Journal of Alloys and Compounds, 692, PP. 301312 (2017).CrossRefGoogle Scholar
Wen, Z.X., Zhang, Y.M., Li, Z.W. and Yue, Z.F., “Equivalent and simplification of nickel-based single crystal plates with film cooling holes”, Aerospace Science and Technology, 82–83, pp. 119139 (2018).CrossRefGoogle Scholar