Advanced Composite Materials

  • 제18권3호
  • /
  • Pages.233-249
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  • 2009
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  • 0924-3046(pISSN)
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  • 1568-5519(eISSN)
한국복합재료학회 (The Korean Society for Composite Materials)
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Failure Pressure Prediction of Composite Cylinders for Hydrogen Storage Using Thermo-mechanical Analysis and Neural Network

  • Hu, J. (Department of Mechanical and Aerospace Engineering, Missouri University of Science and Technology) ;
  • Sundararaman, S. (Department of Mechanical and Aerospace Engineering, Missouri University of Science and Technology) ;
  • Menta, V.G.K. (Department of Mechanical and Aerospace Engineering, Missouri University of Science and Technology) ;
  • Chandrashekhara, K. (Department of Mechanical and Aerospace Engineering, Missouri University of Science and Technology) ;
  • Chernicoff, William (US Department of Transportation)
  • 투고 : 2008.02.13
  • 심사 : 2008.07.26
  • 발행 : 2009.09.01
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초록

Safe installation and operation of high-pressure composite cylinders for hydrogen storage are of primary concern. It is unavoidable for the cylinders to experience temperature variation and significant thermal input during service. The maximum failure pressure that the cylinder can sustain is affected due to the dependence of composite material properties on temperature and complexity of cylinder design. Most of the analysis reported for high-pressure composite cylinders is based on simplifying assumptions and does not account for complexities like thermo-mechanical behavior and temperature dependent material properties. In the present work, a comprehensive finite element simulation tool for the design of hydrogen storage cylinder system is developed. The structural response of the cylinder is analyzed using laminated shell theory accounting for transverse shear deformation and geometric nonlinearity. A composite failure model is used to evaluate the failure pressure under various thermo-mechanical loadings. A back-propagation neural network (NNk) model is developed to predict the maximum failure pressure using the analysis results. The failure pressures predicted from NNk model are compared with those from test cases. The developed NNk model is capable of predicting the failure pressure for any given loading condition.

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참고문헌

  1. N. Takeichia, H. Senoha, T. Yokotab, H. Tsurutab, K. Hamadab, H. Takeshitac, H. Tanakaa, T. Kiyobayashia, T. Takanod and N. Kuriyamaa, Hybrid hydrogen storage vessel, a novel highpressure hydrogen storage vessel combined with hydrogen storage material, Intl J. Hydrogen Energy 28, 1121–1129 (2003)
  2. C. Liang, H. Chen and C.Wang, Optimum design of dome contour for filament-wound composite pressure vessels based on a shape factor, Compos. Struct. 58, 469–482 (2002)
  3. V. V. Vasiliev, A. A. Krikanov and A. F. Razin, New generation of filament-wound composite pressure vessels for commercial applications, Compos. Struct. 62, 449–459 (2003)
  4. P. Y. Tabakov and E. B. Summers, Lay-up optimization ofmultilayered anisotropic cylinders based on a 3-D elasticity solution, Comput. Struct. 84, 374–384 (2006)
  5. J. Park, C. Hong, C. G. Kim and C. U. Kim, Analysis of filament wound composite structures considering the change of winding angles through the thickness direction, Compos. Struct. 55, 63–71 (2002)
  6. S. Kobayashi, T. Imai and S. Wakayama, Burst strength evaluation of the FW-CFRP hybrid composite pipes considering plastic deformation of the liner, Composites Part A 38, 1344–1353 (2007)
  7. M. Z. Kabir, Finite element analysis of composite pressure vessels with a load sharing metallic liner, Compos. Struct. 49, 247–255 (2000)
  8. D. L. Gray and D. J. Moser, Finite element analysis of a composite overwrapped pressure vessel, in: 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Fort Lauderdale, FL, USA, AIAA 2004–3506, pp. 1–15, July 11–14 (2004)
  9. I. H. Akcay and I. Kaynak, Analysis of multilayered composite cylinders under thermal loading, J. Reinf. Plast. Compos. 24, 1169–1179 (2005)
  10. O. Sayman, Analysis of multi-layered composite cylinders under hygrothermal loading, Composites Part A 36, 923–933 (2005)
  11. J. M. Schneider, Gaseous hydrogen station test apparatus: verification of hydrogen dispenser performance utilizing vehicle representative test cylinders, in: SAE World Congress and Exhibition, Detroit, MI, USA, pp. 1–10, April (2005)
  12. J. Hu, J. Chen, S. Sundararaman, K. Chandrashekhara and W. Chernicoff, Analysis of composite hydrogen storage cylinders subjected to localized flame impingements, Intl J. Hydrogen Energy 33, 2738–2746 (2008)
  13. K. Chandrashekhara and A. Bhimaraddi, Thermal stress analysis of laminated doubly curved shells using a shear flexible finite element, Comput. Struct. 52, 1023–1030 (1994)
  14. K. Chandrashekhara and T. Schroeder, Nonlinear impact analysis of laminated cylindrical and doubly curved shells, J. Compos. Mater. 29, 2160–2179 (1995)
  15. F. Mitlitsky, A. H. Weisberg and B. Myers, Vehicular hydrogen storage using lightweight tanks, Proc. U.S. DOE Hydrogen Prog. Rev. NREL/CP-570-28890 (2000)
  16. S.W. Tsai and E.M.Wu, A general theory of strength for anisotropic materials, J. Compos. Mater. 5, 58–80 (1971)
  17. K. J. Yoon and J. Kim, Prediction of thermal expansion properties of carbon/epoxy laminae for temperature variation, J. Compos. Mater. 34, 90–100 (2000)