Effect of environment and thermal cycles on tensile behavior ofhybrid single lap joints for fiber metal laminates

Publish Year: 1392
نوع سند: مقاله کنفرانسی
زبان: English
View: 875

This Paper With 8 Page And PDF Format Ready To Download

  • Certificate
  • من نویسنده این مقاله هستم

استخراج به نرم افزارهای پژوهشی:

لینک ثابت به این Paper:

شناسه ملی سند علمی:

WMECH02_162

تاریخ نمایه سازی: 21 تیر 1393

Abstract:

This experimental study investigates the effects of sea water and thermal cycling conditions on strength of hybrid lap joints made by fiber metal laminate (FML) and 430 stainless steel adherends subjected to tensile loading. The FMLs are made of three alternative layers of two 430 stainless steel sheets and one prepreg glass fiber reinforced composite (G10) layer. The adherends are bonded by infusion of AD-314 resin mixed with HA-34 hardener and also steel bolt is used for the mechanical fastening to make hybrid single lap joint. The joints are kept in the sea water taken from Persian Gulf for 30 days in the laboratory. Some of the specimens are then thermally cycled for 0, 5 and 10 cycles from 40 to 100 ◦C for the dwell time of 20 min in an oven and from -40 to -100 ◦C for the dwell time of 10 min by liquid nitrogen, and afterwards tested in Tensile loading. One specimen is also tested with 0 thermal cycling at ambient environment for comparison purpose. Experimental results revealed that the bond failure of adhesive in hybrid single lap joint specimens subjected to sea water is 62.75% of the same specimens in the ambient environment and the adhesive strength is improved by 47.34% and 52.16% for 5 and 10 thermal cycling at high temperature and also by 24.76% and 49.5% for 5 and 10 thermal cycling at cryogenic temperatures with respect to sea water at 0 thermal cycling. The ultimate strength of the hybrid lap joint specimens subjected to sea water is 91.3% of the same in ambient environment.

Authors

S. M. R Khalili

Professor, Center of Excellence for Research in Advanced Materials and Structures, Faculty of Mechanical Engineering, K.N. Toosi University of Technology, Tehran, Iran

M Sharafi

M.sc Graduated Student, Department of Mechanical Engineering, South Tehran Branch, Islamic Azad University, Tehran, Iran

مراجع و منابع این Paper:

لیست زیر مراجع و منابع استفاده شده در این Paper را نمایش می دهد. این مراجع به صورت کاملا ماشینی و بر اساس هوش مصنوعی استخراج شده اند و لذا ممکن است دارای اشکالاتی باشند که به مرور زمان دقت استخراج این محتوا افزایش می یابد. مراجعی که مقالات مربوط به آنها در سیویلیکا نمایه شده و پیدا شده اند، به خود Paper لینک شده اند :
  • Jin-Hwe Kweon, Jae-Woo Jung, Tae-Hwan Kim, Jin-Ho Choi, Dong-Hyun Kim. ...
  • Vlot A, Vogelesang LB, De Vries TJ. Towards application of ...
  • Gunnink JW, Vlot A, De Vries TJ, Van Der Hoeven ...
  • Vlot A. Impact loading On fibre metal laminates. Int J ...
  • Vogelesang LB, Vlot A. Development of fibre metal laminates for ...
  • Wu HF, Wu LL, Slagter W.J. An investigation on the ...
  • Van Rooijen RG, Sinke J, De Vries TJ, Van Der ...
  • Meola M, Squillace A, Giorleo G, Nele L. Experimental ch ...
  • Icten BM, Sayman O. Failure analysis of pin-loaded a luminiumglass- ...
  • Wu HF, Slagter WJ. Parametric studies of bearing strength for ...
  • Woerden HJM, Sinke J, Hooijmeijer PA. Maintenance of GLARE structures ...
  • Abrao AM, Faria PE, Campos Rubio JC, Reis P, Paulo ...
  • Kelly G. Load transfer in hybrid (bon ded/bolted) composite singlelap ...
  • Hart-Smith LJ. Bonded-bolted composite joints. J Aircraft 1985;22: 993-1000. ...
  • نمایش کامل مراجع