DOI QR코드

DOI QR Code

Effect of Surface Properties on Adhesive Strength of Joint of Glass Fiber/Polyester Composite Panels

유리섬유/폴리에스테르 복합재료 패널 접합부의 접착강도에 관한 표면성질의 효과

  • 팜탄눗 (울산대학교 기계공학부) ;
  • 염영진 (울산대학교 기계공학부)
  • Received : 2012.05.22
  • Accepted : 2012.08.10
  • Published : 2012.12.01

Abstract

Adherend samples were made from unsaturated polyester and woven and mat glass fibers by the hand layup and vacuum methods. The mechanical properties of the adhesive, composite adherends, and terminal-joint and secondary-joint specimens were determined experimentally. Combinations of the experiment results and the bonding theory were used in this study. The maximum and average shear stresses were calculated based on the maximum tensile force and geometry parameters of the joint specimens. The results of the maximum and average shear stresses were compared and evaluated for six joints. The results showed that the grinding and grind/acetone joint had the highest strength among three types of terminal-joints. Similarly, the mat-mat and mat-woven joints had the highest strength among three types of secondary-joints with the same value. Conversely, no treatment and woven-woven bonding had very low strength. In each case, failure occurred always at two ends and then moved toward the middle area of the overlap length.

복합재료 접합부의 접착강도에 대한 접착면 성질의 영향을 알아 보기 위해 불포화폴리에스테르, 우븐과 매트 유리섬유를 사용하여 복합재료 접합시편들을 제작하였다. 접착제, 복합재료 접착물, 말단접합과 이차접합 시편들의 기계적 성질을 실험에 의해 구하고 실험결과를 접합이론에 적용하였다. 6 개의 접합부들에서 발생하는 최대 및 평균 전단 응력은 최대 인장력과 접합 시편의 기하학적 변수들로부터 계산되었다. 실험 결과 접합면을 연마한 후 아세톤으로 처리한 경우가 말단접합의 3 가지 형태 중 가장 큰 강도를 가지고 있음이 관찰되었다. 마찬가지로 매트-매트와 매트-우븐 접합이 거의 같은 값으로 이차 접합의 3 가지 형태 중 가장 큰 강도를 가지고 있었다. 반대로 아무 처리도 하지 않은 접합시편과 우븐-우븐 접합시편은 매우 낮은 강도를 가졌다. 각각의 경우 파손은 접합부 양끝에서 심하게 발생하였고 접합부 가운데로 이동하였다.

Keywords

References

  1. Clyne, B., 2000, "Mechanics of Composite Materials," Version 2.1,University of Cambridge.
  2. Kim, H. and Kedward, K., T.,2001, "Stress Analysis of Adhesive Bonded Joints Under in-Plane Shear Loading," Jo.adhesion.
  3. Kim, K.-S., Yoo, J.-S., Yi, Y.-M. and Kim, C.-G., 2006, "Failure Mode and Strength of Uni-Directional Composite Single Lap Bonded Joints with Different Bonding Methods," Composite Structures, 72, pp. 477-485. https://doi.org/10.1016/j.compstruct.2005.01.023
  4. Slaviša, P., Branislav, B., Dragana, V., Marina, S. and Vladimir, P., 2009, "The Interlaminar Strength of the Glass Fiber Polyester Composite," Chemical Industry & Chemical Engineering Quarterly, 15(1), pp. 45-48.
  5. Seong, M.-S., Kim, T.-H., Nguyen, K.-H., Kweon, J.- H. and Choi, J.-H., 2008, "A Parametric Study on the Failure of Bonded Single-Lap Joints of Carbon Composite and Aluminum," Composite Structures, 86, pp. 135-145. https://doi.org/10.1016/j.compstruct.2008.03.026
  6. Magalhães, A. G., de Moura, M.F.S.F. and Gon-calves, J.P.M., 2005, "Evaluation of Stress Concentration Effects in Single-Lap Bonded Joints of Laminate Composite Materials," International Journal of Adhesion & Adhesives, 25, pp. 313-319. https://doi.org/10.1016/j.ijadhadh.2004.10.002
  7. Broughton, W. R. and Hinopoulos, G., 1999, "Evaluation of the Single-Lap Joint Using Finite Element Analysis," NPL Report CMMT(A), 206.
  8. Department of Defense, 2002, "Composite Materials Hand-Book: Polymer Matrix Composites Materials Usage, Design, and Analysis," MIL-HDBK-17-3F, Volume 3.
  9. Kim, H. and Kedward, K., 2001, "Stress Analysis of In-Plane, Shear-Loaded, Adhesively Bonded Composite joints and Assemblies," DOT/FAA/AR-01/7.
  10. Veselovsky, R. A. and Kestelman, V. N., 2002, "Adhesion of Polymers," McGraw-Hill eBook.
  11. Chadegani, A. and Batra, R. C., 2011, "Analysis of Adhesive-Bonded Single-Lap Joint Withan Interfacial Crack and a Void," International Journal of Adhesion & Adhesives, 31, pp. 455-465. https://doi.org/10.1016/j.ijadhadh.2011.02.006
  12. Miyazaki, Y. and Furusako, S., 2007, "Tensile Shear Strength of Laser Welded Lap Joints," Nippon steel Technical Report No. 95.
  13. "Standard Test Method for Strength Properties of Adhesives in Shear by Tension Loading of Single Lap-Joint Laminated Assemblies," ASTM, D3165 - 07.