The Influence of Volume Fraction and Fiber Orientation of CERP Layer on Flexural properties of A17075/CFRP Multi-Layered Hybrid Laminate Material

Al Shee/CFRP 다적층 하이브리드 복합재료의 굴곡강도에 미치는 카본섬유 체적률 및 배열방향 영향

  • Published : 2004.12.01

Abstract

The A17075/CFRP multi-layered hybrid laminate material consists of the alternating A17075-T6 sheets and carbon/epoxy prepregs of M40 fade. The influence of volume fraction and fiber orientation of A17075/CFRP layer on flexural properties of A17075/CFRP laminate alternating A17075-T6 and carbon/epoxy prepreg was investigated. The results obtained from the experimental analysis are as follows: 1. In the $0^{\circ}$ fiber orientation, the mont of increase of the flexural rigidity was $20.5\%$ at the $26.5\%$ volume fraction and $38.0\%\;at\;the\;35.7\%$ volume fraction compared with the flexural rigidity level(20.0GPa) of the $10\%$ volume fraction of CFRP. 2. In the $\pm45^{\circ}$ fiber orientation the amount of decrease of the flexural rigidity was $23.5\%\;at\;the\;20.0\%$ volume fraction and $31.5\%\;at\;the\;33.3\%$ volume fraction compared with the flexural rigidity level of the $10\%$ volume fraction of CFRP. 3. In the $0^{\circ}$ fiber orientation, the flexural strength was 481.5MPa at the $10\%$ volume fraction of CFRP and 583.8MPa at the $26.5\%$ volume fraction and 653.7MPa at the $35.7\%$ volume faction. 4. In the $\pm45^{\circ}$ fiber orientation, the flexural strength was 354.0MPa at the $20.0\%$ volume fraction of CFRP and 340.5MPa at the $33.3\%$ volume fraction.

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References

  1. J. C. McMillian, 'Bonded Joints and Preparation for Bonding', NATOAGARD Lecture Series 102, 3, #7, p. 150, 1979
  2. D. H. Middleton, 'Composite Materials in Aircraft Structure The Involvement of the United States Aircraft Structure Industry in the Development of Advanced Composite Materials', Longman Scien tific & Technical, John Wiley Inc., New York, pp. 273-288, 1990
  3. R Marrissen, 'Flight Simulation Behavior Aramid Reinforced Aluminium Laminate (ARALL)', Eng. Fracture Mechanics, 19, pp. 261-277, 1984 https://doi.org/10.1016/0013-7944(84)90021-3
  4. R. Marrisen, 'Fatigue Mechanism in ARALL A Fatigue Resistant Hybrid Aluminium Aramid Composite Material', Fatigue, 87, Proc. 3rd Int. Cont. on Fatigue Threshold, Vol. 3, EMAS LTD, Warley, U.K, pp. 1271-1279, 1987
  5. H. K. Yoon, 'The Effect of Bridging on Fatigue Crack Growth Behavior in Aramid Patched Aluminium Alloy (APAL)', J. of KSME, Vol. 8, No.4, pp. 375-384, 1994 https://doi.org/10.1007/BF02944710
  6. G. L. Roderick, 'Debond Propagation in Composite Reinforced Metals', NASA TMX-71948, 1974
  7. I. C. Taig, 'Design Concepts for the Use of Composite in Airframes', British Aircraft Co., 1975
  8. S. Oken, 'Analytical and experimental Investigation of Aircraft Metal Structures Reinforced with Filamentary Composites', NASA CR-1859, 1971
  9. C. T. Lin, 'Fatigue Behaviour of Carbon Fiber Reinforced Aluminium Laminates', Composites, Vol. 22, pp. 135-141, 1991 https://doi.org/10.1016/0010-4361(91)90672-4
  10. D. L. Davidson, 'Fatigue Crack Growth through ARALL 4 at Ambient Temperature', Fatigue Fract. Eng. Mater. Struct., Vol. 14, No. 10, pp. 939-951, 1991 https://doi.org/10.1111/j.1460-2695.1991.tb00004.x
  11. F. A. Sandow, 'Composite Repair of Cracked Aluminum Alloy Aircraft Structure', AFWAL-TR-87-3072, 1987
  12. Kyung-Bong Lee, 'The effect of CFRP volume fraction and carbon fiber orientation on tensile/flexural properties in Al/CFRP laminate', Journal of the KIIS, Vol. 16, No.5, 13-16, 2001
  13. Kyung-Bong Lee, 'A study on mechanical and fatigue characteristics in a fiber reinforced metal laminates of Al/CFRP', Journal of KIIS, Vol. 14, No.5, pp. 11-15, 1999