Chapter
Apr 15, 2021

Study on the Numerical Simulation Methodology of Kevlar Fabric Wraps Structure under the Impact of High-Speed Rotating Blade

Publication: Earth and Space 2021

ABSTRACT

According to the aero-engine containment structure application and loads, the numerical simulation method of Kevlar fabric wrap structure under the impact of high-speed rotating blade was studied and compared with test results. The mechanical properties of Kevlar fabric were investigated firstly, including static and dynamic tension, shear, and friction. Some test methods and fixtures were developed. The response behavior of Kevlar fabric under different loads were obtained and analyzed. Then MAT-214 material model in LS-DYNA was studied to characterize the Kevlar fabric, and the data obtained by the mechanical properties tests were applied. The numerical simulation model of subscale casing and blade was established to simulate the impact process of casing and rotating blade. The casing is composed of an inner thin aluminum ring and outer wrapping Kevlar fabric. The fabric was modeled as continuum by using shell element. The effect of mesh size and shell element layers was discussed. The impact process was analyzed, and it matched well with the high-speed photography. The blade kinetic energy and fabric deformation of simulation and test results also matched well.

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REFERENCES

[1] Xuan Haijun, Lu Xiao, Hong Weirong, and Liao Lianfang. Review of aero-engine case containment research[J], Journal of Aerospace Power, 2010, 25(8): 1860-1870.
[2] Mcmillan A. Material development for fan blade con-tainment ring[J]. Journal of Physics: Conference Series, 2008, 105: 12-22.
[3] Zhang Yifen, and Mu Jianchun. Advances in impact damage of composite laminated structures(I)[J]. Journal of Taiyuan University of Technology, 1999, 30(6): 563-566.
[4] Zhu D., Experimental study and finite element modeling of woven fabrics[D]. Arizona State University, 2009.
[5] Tabiei A., and Nilakantan G. Ballistic impact of dry woven fabric composites: a review[J]. Applied Mechanics Reviews. 2008, 61(1): 10801e-10813e.
[6] Roylance D., and Wang S.S., Penetration mechanics of textile structures[R]., 1979.
[7] Shim V. P. W., Lim C. T., and Foo K. J. Dynamic mechanical properties of fabric armour[J]. International Journal of Impact Engineering, 2001, 25(1): 1-15.
[8] Lim C. T., Shim V. P. W., and Ng Y. H. Finite-element modeling of the ballistic impact of fabric armor[J]. International Journal of Impact Engineering, 2003, 28(1): 13-31.
[9] Shahkarami A., Vaziri R., Poursartip A., et al. A numerical investigation of the effect of projectile mass on the energy absorption of fabric panels subjected to ballistic impact[C]. 20th International Symposium on Ballistics. 2002: 802-809.
[10] Tabiei A., and Jiang Y. Woven fabric composite material model with material nonlinearity for nonlinear finite element simulation[J]. International Journal of Solids and Structures, 1999, 36(18): 2757-2771.
[11] Jiang Y., Tabiei A., and Simitses G. J. A novel micromechanics-based approach to the derivation of constitutive equations for local/global analysis of a plain-weave fabric composite[J]. Composites Science and Technology, 2000, 60(9): 1825-1833.
[12] Tanov, R., and Tabiei, A. Computationally efficient micro-mechanical woven fabric constitutive[J]. Journal of Models Apply Mechnics, 2001, 68(4): 553-560.
[13] Barbero E. J., Lonetti P., and Sikkil K. K. Finite element continuum damage modeling of plain weave reinforced composites[J]. Composites Part B: Engineering, 2005, 37(2-3): 137-147.
[14] Duan Y., Keefe M., Bogetti T. A., et al. Finite element modeling of transverse impact on a ballistic fabric[J]. International Journal of Mechanical Sciences, 2006, 48(1): 33-43.
[15] Stahlecker Z., Mobasher B., Rajan S. D., et al., Development of reliable modeling methodologies for engine fan blade out containment analysis. Part II: Finite element analysis[J]. International Journal of Impact Engineering, 2009. 36(3): 447-459.
[16] Bansal S., Mobasher B., and Rajan S.D., Development of fabric constitutive behavior for use in modeling engine fan blade-out events[J]. Journal of Aerospace Engineering, 2009. 7: 249-259.
[17] Jeffrey Simmons, David Erlich, and Donald Shockey, Explicit finite element modeling of multilayer com-posite fabric for gas turbine engine containment systems. Phase 1 - Part 3: Model development and simulation of experiments, November 2004.
[18] J. M. Pereira, and Revilock D.M. Explicit finite element modeling of multilayer composite fabric for gas turbine engine containment systems. Phase 1 - Part 2: ballistic impact testing, Federal Aviation Administration, Report No. DOT/FAA/AR-04/40, P2, November 2004.
[19] S. D. Rajan, Mobasher B., Vaidya A., et al. Explicit finite element modeling of multilayer composite fabric for gas turbine engine containment systems. Phase 4, Federal Aviation Administration, May 2014.
[20] Simmons J., Erlich D., and Shockey D., Explicit finite element modeling of multilayer composite fabric for gas turbine engine containment systems. Phase 2- Part 3: Model development and simulation of experiments[R]., 2004.
[21] Murat, Buyuk, Steve, Kan, and Loikkanen Matti J. Explicit finite-element analysis of 2024-T3/T351 Aluminum material under impact loading for airplane engine containment and fragment shielding[J]. Journal of Aero-space Engineering, 2009, 7: 287-295.

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Earth and Space 2021
Pages: 243 - 252

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Published online: Apr 15, 2021

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1High-Speed Rotating Machinery Laboratory, College of Energy Engineering, Zhejiang Univ., Hangzhou, China. Email: [email protected]
Haijun Xuan
2High-Speed Rotating Machinery Laboratory, College of Energy Engineering, Zhejiang Univ., Hangzhou, China

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