접착이음의 파괴 기준 설정을 위한 연구

Establishment for Failure Criterion of Adhesively Bonded Joint

  • 이강용 (정회원, 연세대학교 기계공학과) ;
  • 공병석 (정회원, 현대자동차)
  • 발행 : 2000.01.01

초록

The objective of this work is to develop a criterion for predicting the failure strength of the joints bonded by ductile adhesives. To obtain a criterion, first, fracture tests were carried out for T-peel joint and Single-lap joint with widely differing joints geometries. Then using the fracture loads obtained at tests, the finite element analysis were performed, in which the stresses in the adhesive bonds were calculated in great detail. After examining four epoxy adhesives, it is concluded that the fracture of adhesively bonded joint occurs when the maximum of the ratio of the mean to effective stresses exceeds a constant value which can be determined from analysis and test for each adhesive.

키워드

참고문헌

  1. Journal of Mechanical Physics Solids v.17 On the Ductile Enlargement of Voids in Triaxial Stress Fields J. R. Rice;D. M. Tracey
  2. Journal of Engineering Materials and Technology v.99 Continuum Theory of Ductile Rupture by Void Nucleation and Growth:Part I -4 Yield Criteria and Flow Rules for Porous Ductile Media A. L. Gurson
  3. Ducitle Fracture of Metals P. F. Thomason
  4. Metallurgical Transactions v.6A A. S. Argon;J. IM;R. Saforglu
  5. International Journal of Fracture v.83 Prediction of Crack Growth Direction for Mode Ⅰ/Ⅱ Loading Using Small-scale Yielding and Void Initiation/growth Concepts M. A. Sutton;W. Zhao;M. L. Boone;A. P. Reynolds;D. S. Dawicke
  6. ASTM D 638, Standard Test Method for Tensile Properties of Plastics
  7. Coach Joint Fracture Test
  8. ASTM D 1002-72, Standard Test Method for Strength Properties of Adhesives in Shear by Tension Loading(Metal-to metal)
  9. ASTM D 3165-73 Standard Test Method for Strength Properties of Adhesives in Shear by Tension Loading of Laminated Assemblies
  10. ASTM B 209-95, Standard Specification for Aluminum and Aluminum-Alloy Sheet and Plate
  11. Smithells Metals Reference Book(sixth edition) E. A. Brandes
  12. Fiber Reinforced Epoxy Prepreg, 250°F Cure, DMS 2288 Douglas Aircraft Co.
  13. Hankuk Fiber Process Control Specification Hankuk Fiber Glass Co.