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Fatigue strength investigation of bonded joints

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EN
Abstrakty
EN
Numerous advantages of the bonded joints result in wide application in the aircraft, motor industry or powertrain components. These types of joints enable joining materials with different mechanical properties (e.g. Stiffness) and dimensions without structure change. Proper joint design limits the field of local stress concentrations or even eliminates them. The structural integrity of complete structure depends on the fatigue estimation of the bonded joint. Application of the finite element method to life prediction of the double lap bonded joint metal-composite-metal is presented. Three dimensional numerical models are generated by professional engineering software tools. The contact problem is modelled between the epoxy resin and metal and composite surfaces. A laminated composite consists of the epoxy woven carbon prepreg. Elasto-plastic materials models of the adhesion and metal and orthotropy composite model allowed determining the contact normal stress in the interfaces in each deformation increment which is induced by an external load. MSC.Marc was used to determine the strain and stress distribution in the double lap bonded joint including contact normal stress in the steel/adhesive and laminated composite/adhesive interfaces. Two numerical models of the double lap bonded joint were compared. The use of the presented method is more suitable for structure optimisation than numerical analysis.
Twórcy
autor
  • Military University of Technology Faculty of Mechanical Engineering Department of Mechanics and Applied Computer Science Gen. Sylwestra Kaliskiego 2, 00-908 Warsaw, Poland tel.: +48 022 683 92 26, fax: +48 022 683 94 61, r.gieleta@wme.wat.edu.pl
Bibliografia
  • [1] Broughton, W. R., Crocker, L. E., Gower, M. R. L., Design Requirements for Bonded and Bolted Composite Structures, NPL Report MATC(A)65, UK, 2002.
  • [2] Derewońko, A., Godzimirski, J., Kosiuczenko, K., Niezgoda, T., Kiczko, A., Strength Assessment of Adhesive-Bonded Joints, 16th International Workshop on Computational Mechanics Of Materials mat. konf., Lublin, 2006.
  • [3] Godzimirski, J., Wytrzymałość doraźna konstrukcyjnych połączeń klejowych, WNT, 2002.
  • [4] Godzimirski, J., Tkaczuk, S., Określanie właściwości mechanicznych spoin klejowych, Technologia i Automatyzacja Montażu 3, 4/2004.
  • [5] Jaeger, J., New Solutions in Contact Mechanics, WIT Press 2005.
  • [6] Lee M. C. H., Short W. T., Abdi F., Qian J., A Math-Based Methodology for Fatigue Longevity Prediction of 3D Woven Fiberglass Reinforced Vinyl-ester Composites, SAE Technical Paper Series 2006.
  • [7] MSC.Fatigue. Theory. The MacNeal-Schwendler Corporation.
  • [8] MSC.Marc Volume A: Theory and User Information., The MacNeal-Schwendler Corporation,Version 2005.
  • [9] Sun, H., Pan N., Mechanical characterization of the interfaces in laminated composites, Composite Structures 74, s. 25-29, 2006.
  • [10] Toubal, L., Karama, M., Lorrain, B., Damage evolution and infrared thermography in woven composite laminates under fatigue loading, Int. J. of Fatigue 28, 1867-1872, 2006.
  • [11] Zhu, Y., Kedward, K., Methods of analysis and failure predictions for adhesively bonded joints of uniform and variable bondline thickness, DOT/FAA/AR-05/12, U.S. Department of Transportation, Federal Aviation Administration, 2005.
  • [12] SGL CARBON GROUP, Carbon Composites, www.sglcarbon.com, 2000.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-BUJ5-0036-0091
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