نوع مقاله : مقاله پژوهشی

نویسندگان

1 دانشجوی کارشناسی ارشد، مهندسی مکانیک، دانشگاه آزاد اسلامی واحد تهران جنوب، تهران

2 استادیار، مهندسی مکانیک، دانشگاه آزاد اسلامی واحد تهران جنوب، تهران

چکیده

در این مقاله تاثیر نانو سیلیکا بر مقاومت به ضربه پانل‌های ساندویچی با رویه بازالت و پانل‌های ساندویچی با رویه هیبریدی بازالت و کولار بررسی شده است. پانل‌های ساندویچی با رویه بازالت شامل چهار لایه پارچه بازالت به عنوان رویه بالایی و پایینی که هسته فوم بین آن قرار دارد. پانل ساندویچی با رویه هیبریدی از چهار لایه پارچه بازالت/کولار/کولار/بازالت به عنوان رویه بالایی و پایینی ساخته شده که هسته فوم ما بین آنها قرار دارد. از پارچه‌های کولار با چگالی 200 گرم بر متر مربع، پارچه بازالت با چگالی 350 گرم بر متر مربع، فوم پلی اورتان با چگالی 140 گرم بر سانتی متر مربع، رزین اپوکسی EPR1080 و درصدهای وزنی مختلف نانو سیلیکا برای ساخت نمونه‌های پانل ساندویچی استفاده شده است. فرآیند ساخت نمونه‌های آزمایش با روش لایه‌گذاری دستی انجام گرفت. همچنین برای پخش و توزیع بهتر ذرات نانوسیلیکا در ماتریس اپوکسی از دستگاه آلتراسونیک استفاده شد. آزمایش‌های ضربه سرعت پایین با استفاده از دستگاه وزنه افتان با انرژی ضربه ثابت بر روی نمونه‌ها انجام گردید. نتایج نشان داد افزودن نانو به پانل ساندویچی سبب بهبود مقاومت به ضربه می‌شود و بیشترین نیروی تماسی ماکزیمم مربوط به پانل ساندویچی با 1/1% نانوسیلیکا می‌باشد.

کلیدواژه‌ها

عنوان مقاله [English]

An investigation of impact resistance of sandwich panel with basalt skin and basalt/Kevlar hybrid skin with nano silica

نویسندگان [English]

  • Mohsen Hafezi 1
  • Mehdi Yarmohammad Tooski 2

1 Department of Mechanical Engineering, South Tehran Branch, Islamic Azad University, Tehran, Iran.

2 Department of Mechanical Engineering, South Tehran Branch, Islamic Azad University, Tehran, Iran.

چکیده [English]

In this paper, the effect of nano silica on impact resistance of sandwich panels with basalt skin and hybrid sandwich panel with basalt and kevlar skin is investigated. Sandwich panels with a basalt skin consist of four layers of basalt fabric as the top and bottom skins which the foam core is located between them. Sandwich panels with a hybrid skin consist of four layers of basalt/Kevlar/Kevlar/basalt fabric as the top and bottom skins which the foam core is located between them. Kevlar fabrics with a density of 200 g /m2, basalt fabrics with a density of 350 g /m2, a polyurethane foam with a density of 140 g/cm2, EPR1080 epoxy resin and different weight percentages of nano silica were used to make sandwich panels. All panels are fabricated using Hand Lay-up method. Ultrasonic device was also used for homogenization and better dispersion of nano silica in epoxy matrix. Low velocity impact tests were performed using drop weight equipment at constant impact energy on the specimens. The results showed that the addition of nano into the sandwich panel improved the impact resistance and the maximum contact force is related to the sandwich panel with 1.1% nano silica.

کلیدواژه‌ها [English]

  • Hybrid sandwich panel
  • nano silica
  • Low velocity impact
  • Kevlar
  • basalt
[1] Jafari, S.S., and Feli, S., “Analytical investigation of impact of blunt projectile with different ended into sandwich panels,” in Persian, Journal of Modeling in Engineering, Vol. 3, No. 42, pp. 65-77, 2015.
[2] Gustin, J., Joneson, A., Mahinfalah, M., Stone, J., “Low velocity impact of combination Kevlar/carbon fiber sandwich composites,” Composite structures, Vol. 69, No. 4, pp. 396-406, 2005.
[3] Mahdian, M., and Ebrahimi, H., “Analytical and numerical analysis of low speed impact on sandwich panel with metal and polyurethane foam core,” in Persian, The International Conference on New Research in Industry and Mechanical Engineering.
[4] Fan, J., Cantwell, W., Guan, Z., “The low-velocity impact response of fiber-metal laminates,” Reinforced Plastics and Composites, Vol. 30, No. 1, pp. 26-35, 2011.
[5] Chen, C., Justice, R. S., Schaefer, D. W., Baur, J. W., “Highly dispersed nanosilica–epoxy resins with enhanced mechanical properties,” Polymer, Vol. 49, pp. 3805-3815, 2008.
[6] Ghofrani, M., Pishan, S., Talaei, A., “The effect of core type and skin on the mechanical properties of lightweight sandwich Panels,” in Persian, Iranian Journal of Wood and Paper Science Research, Vol. 28, No. 4, pp.720-731, 2014.
[7] Azarafza, R., Davar, A., and Mahmoodi, A., “Three-point bending test of metal and composite sandwich panels with grid stiffened core,” in Persian, Journal of Science and Technology of Composites, Vol. 3, No. 4, pp. 377-388, 2017.
[8] Khoshgoftar, M., Liaghat, G., “Experimental and Numerical Investigation of Perforation Behavior of Composite Laminates Reinforced with Carbon Nanotubes,” in Persian, Tarbiat Modares University, Mechanical Engineering Department, 2010.
[9] Payganeh, Gh., Malekzade Fard K., Rashed Saghavaz, F., and Asgari, M., “Analysis of laminated composite sandwich plates with magnetorheological fluid core under low velocity impact,” in Persian, Modares Mechanical Engineering, Vol. 16, No. 12, pp. 114-124, 2016.
[10] Alavi Nia, A., and Kazemi, M., “Analytical study of high velocity impact on sandwich panels with foam core and aluminum face-sheets,” in Persian, Modares Mechanical Engineering, Vol. 15, No. 6, pp.231-239, 2015.
[11] Malekzadeh Fard, K., Ebrahimi, M., Nazari, A., and Irani, S., “Buckling Analysis of Composite Sandwich Panel with Symmetric FGM Core,” in Persian, Using Improved High-order Theory, Aerospace Mechanics Journal, Vol. 8, No. 1, pp. 55-70, 2012.
[12] Pirmohammadi, N., Liaghat, Gh. H., Pol, M. H., and Sabouri, H., “Analytical, experimental and numerical investigation of sandwich panels made of honeycomb core subjected projectile impact,” in Persian, Modares Mechanical Engineering, Vol. 14, No. 5, pp. 153-164, 2014
[13] Hassanpour Roudbeneh, F., Liaghat, Gh., Sabouri, H., Hadavinia, H., “Investigation of Interaction between Aluminum Facing and Honeycomb Structure in Quasi-static and Impact Loading,” in Persian, Modares Mechanical Engineering, Vol. 16, No. 7, pp. 23-31, 2016
[14] Jabbari, M., Tatari, A. A., and Ghafari, M., “Effect of Faces Type and Thickness on Mechanical Properties of Sandwich Panels,” in Persian, Iranian Journal of Wood and Paper Industries, Vol. 5, No. 1, pp. 85-92, 2014.
[15] Reis, P., Santos, P., J.A.M. Ferreira, M. Richardson, “Impact response of sandwich composites with nano-enhanced epoxy resin,” in Persian, Journal of Reinforced Plastics and Composites, Vol. 32, No. 12, pp. 898-906, 2018.
[16] Khansari, M., Khodarahmi H., Vaziri, A., “Experimental study of ballistic properties of hybrid aluminum and epoxy matrix composite reinforced with carbon nanotube,” in Persian, Modares Mechanical Engineering, Vol. 17, No. 8, pp. 126-132, 2017.
[17] Hassanpour Roudbeneh, F., Liaghat, Gh., Sabouri, H., “Experimental Investigation of foam filled Sandwich Panels in Concentrated and Distributed Compressive loading,” in Persian, Modares Mechanical Engineering, Vol. 16, No. 12, pp. 648-656, 2016.
[18] Payganeh, Gh., Ghasemi, I., Rahmani, M., Kazemnejad, A., “An investigation on the impact properties of nanocomposite based on polypropylene/graphene nanosheets/ nano clay using response surface methodology,” in Persian, Modares Mechanical Engineering, Vol. 15, No. 9, pp. 271-279, 2015.
[19] Pramanik, B., Raju Mantena, P., “Energy Absorption of Nano-Reinforced and Sandwich Composites in Ballistic and Low-Velocity Punch-Shear,” Open Journal of Composite Materials, Vol. 2, No. 3, pp. 87-96, 2012.
[20] Hoo Fatt, M. S., Park, K. S., “Dynamic model for low-velocity impact damage of composite sandwich panels – part A: Deformation,” Composite Structures, Vol. 52, pp. 335-351, 2001.
[21] Haque, A., Shamsuzzoha, M., Hussain, F., Dean, D., “S2-Glass/Epoxy polymer nanocomposites: manufacturing, structures, thermal and mechanical properties,” Journal of Composite Materials, Vol. 37, pp. 1821-1837, 2003.
[22] Khodaei, M., Haghighi-Yazdi, M., Safarabadi, M., “Numerical modeling of high velocity impact in sandwich panels with honeycomb core and composite skin including composite progressive damage model,” Journal of Sandwich Structures & Materials, doi.org/10.1177/1099636218817894
[23] Vishwas, M., Joladarashi, sh.,Kulkarani SM., “Investigation on effect of using rubber as core material in sandwich composite plate subjected to low velocity normal and oblique impact loading,”Scientia Iranica, Vol. 26, No. 2, pp897-907.
[24] Khondabi, R., Khodarahmi, H., Hosseini, R., Zia Shamami, M., “Experimental and numerical investigation into the effect of core density on the energy absorption of sandwich panels with Aluminum face sheets and Polyurethane foam core,” in Persian, Amirkabir Journal of Mechanical Engineering, Vol. 52, No. 10, pp. 131-140, 2019.