• Title/Summary/Keyword: V-Scarf joint

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A Study on the Strength Characteristics of the FRP Bonding Method (FRP 이음방식에 따른 구조강도 특성에 관한 연구)

  • Kim, Kung-Woo;Kang, Dae-Kon;Baek, Myoung-Kee;Park, Jai-Hak
    • Journal of the Korean Society of Marine Environment & Safety
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    • v.21 no.6
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    • pp.778-783
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    • 2015
  • We studied about the strength characteristics of the FRP bonding method due to reduce accident on the oceans and protect life for my people. We test tension and bending strength of butt joint, lap joint, V-scarf joint, X-scarf joint. The result of test, it's pattern is similar both tension and bending strength. Tension strength and bending strength was excellent in order to X-scarf-butt joint-V-scarf-lap joint. The tension strength is the best properties X-scarf showed a 57% strength rate of the basic material, and bending strength showed a 77% strength rate of the basic material. Overall, the X-scarf 12t joint has most excellent properties of tension and bending strength. The lap joint has worst properties of tension and bending strength. We have to test having different over-lay of V-scarf and X-scarf joint each 12t, 16t, 20t. V-scarf of 20t over-lay has excellent character of tension and bending strength. But X-scarf of 12t over-lay has excellent character of tension and bending strength. The results are shown to the contrary. The ship is received a lot of stress. it's hard to compare a direction both actual and test. But we can acknowledge material basic characteristic of strength through tension and bending test. We give the four repair method; butt joint, lap joint, V-scarf joint, X-scarf joint and the reduced ratio in comparison with basic material; In addition give the separated data for V-scarf and X-scarf characteristic of 12t, 16t, 20t overlay length. For our study repair man can select good repair method in his work station.

Geometrical parameters optimizations of scarf and double scarf bounded joint

  • Fekih, Sidi Mohamed;Madani, Kuider;Benbarek, Smail;Belhouari, Mohamed
    • Advances in aircraft and spacecraft science
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    • v.5 no.3
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    • pp.401-410
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    • 2018
  • The aim of this work is to optimize the geometrical parameters as the adhesive thickness and the beveled angle to reduce the edge effect of the scarf and V bounded joint. A finite element analysis is done to define the generated stresses in the bounded joint. The geometrical optimum is obtained using the Experimental Design Method. Results show that the double scarf (V) joint is better than the simple scarf bounded joint.