علوم و فناوری کامپوزیت

علوم و فناوری کامپوزیت

بررسی تأثیر الیاف شیشه، بازالت و هیبرید آنها بر رفتار مکانیکی و جذب انرژی چندلایه های الیافی – فلزی با پایه آلیاژ آلومینیوم 5052

نوع مقاله : مقاله پژوهشی

نویسندگان
1 دانشجوی کارشناسی ارشد، دانشکده مهندسی مکانیک، دانشکدگان فنی، دانشگاه تهران، تهران.
2 استاد، دانشکده مهندسی مکانیک، دانشکدگان فنی، دانشگاه تهران، تهران.
3 استادیار، مهندسی مکانیک، دانشکده فنی و مهندسی ، دانشگاه بناب، بناب.
چکیده
در این پژوهش اهمیت چندلایه‌های الیافی–فلزی به‌عنوان نسل نوین مواد مهندسی با ویژگی‌هایی همچون استحکام بالا، شکل‌پذیری مناسب و مقاومت مطلوب در برابر آسیب بررسی شده است. این ساختارها به‌دلیل عملکرد ترکیبی فلز و کامپوزیت، در صنایع دریایی و هوافضا کاربرد گسترده‌ای دارند. سه نوع چندلایه شامل گلر، بارال و یک نمونه ترکیبی شیشه/بازالت–آلومینیوم با آرایش ثابت FML 5-3/2 ساخته شدند. لایه‌های فلزی از آلومینیوم آلیاژ 5052-H32 و لایه‌های کامپوزیتی از الیاف شیشه، بازالت و ترکیب شیشه/بازالت در زمینه رزین وینیل‌استر تهیه گردیدند. به‌منظور ارزیابی رفتار مکانیکی، آزمون‌های کشش، خمش و ضربه سرعت پایین در سه سطح انرژی انجام شد. نتایج نشان داد گلر بیشترین استحکام کششی با 315 مگاپاسکال را داشته و بارال با 281 مگاپاسکال رفتار تردتری از خود نشان داد، در حالی‌که نمونه ترکیبی با 287 مگاپسکال عملکرد میانی ارائه کرد. در خمش، تنش بیشینه برای گلر 285، بارال 250 و نمونه ترکیبی 227 مگاپاسکال به دست آمد. در آزمون ضربه نیز جذب انرژی عمدتاً ناشی از تغییر شکل پلاستیک آلومینیوم و جدایش بین‌لایه‌ای بود. به‌کارگیری رزین وینیل‌استر به‌جای اپوکسی رایج و استفاده از آلیاژ آلومینیوم 5052-H32 همراه با نمونه ترکیبی شیشه/بازالت، مسیری متفاوت از رویکردهای مرسوم ایجاد کرده است که مقایسه نتایج نشان می‌دهد این انتخاب‌ها نقش قابل توجهی در تغییر رفتار مکانیکی و ظرفیت جذب انرژی دارند.
کلیدواژه‌ها

موضوعات


عنوان مقاله English

Investigation of Glass, Basalt, and Hybrid Fibers Effect on the Mechanical Behavior and Energy Absorption of Fiber–Metal Laminates Based on 5052 Aluminum alloy

نویسندگان English

Pooya Parvandeh 1
Mohsen Hamedi 2
Hadi Rezghi Maleki 3
1 School of Mechanical Engineering, College of Engineering, University of Tehran, Tehran, Iran
2 School of Mechanical Engineering, College of Engineering, University of Tehran, Tehran, Iran.
3 Department of Mechanical Engineering, Faculty of Engineering, University of Bonab, Bonab, Iran
چکیده English

In this study, the significance of fiber–metal laminates (FMLs) as a new generation of engineering materials with superior properties such as high strength, good ductility, and enhanced damage resistance was investigated. Due to their combined metallic–composite performance, these structures are widely applied in marine and aerospace industries. Three types of laminates, including GLARE, BARAL, and a novel hybrid glass/basalt–aluminum configuration with a constant FML 5-3/2 lay-up, were fabricated. The metallic layers consisted of 5052-H32 aluminum alloy, while the composite layers were reinforced with unidirectional glass, basalt, and glass/basalt hybrid fibers in a vinyl ester matrix. To evaluate the mechanical behavior, tensile, flexural, and low-velocity impact tests were performed at three energy levels. The results showed that GLARE exhibited the highest tensile strength of 315 MPa, BARAL displayed a more brittle behavior with 281 MPa, and the hybrid laminate presented an intermediate performance with 287 MPa. Under flexural loading, the maximum stresses were measured as 285 MPa for GLARE, 250 MPa for BARAL, and 227 MPa for the hybrid laminate. In the impact tests, the primary energy absorption mechanisms were identified as plastic deformation of the aluminum layers and interfacial delamination. The use of vinyl ester resin instead of conventional epoxy, along with the employment of 5052-H32 aluminum alloy and the incorporation of a glass/basalt hybrid configuration, introduced a distinctive approach compared to conventional practices, with the comparative results highlighting their significant influence on mechanical response and energy absorption capacity.

کلیدواژه‌ها English

GLARE
BARAL
Hybrid Glass Basalt Aluminum Laminate
Low velocity impact
Energy absorption
[1]  Zuo, P., Srinivasan, D. V.,  Vassilopoulos, A. P., “Review of Hybrid Composites Fatigue“ Composite Structures, Vol. 274, pp. 114358, 2021.
[2]  Alderiesten, R., “Fatigue in Fibre Metal Laminates: The Interplay between Fatigue in Metals and Fatigue in Composites“ Fatigue & Fracture of Engineering Materials & Structures, Vol. 42, No. 11, pp. 2414–2421, 2019.
[3]  Morinière, F., Alderliesten, R., Sadighi, M.,  Benedictus, R., “An Integrated Study on the Low-Velocity Impact Response of the Glare Fibre-Metal Laminate“ Composite Structures, Vol. 100, pp. 89–103, 2013.
[4]  Bieniaś, J., “Fibre Metal Laminates-Some Aspects of Manufacturing Process, Structure and Selected Properties“ Composites, Vol. 11, No. 1, pp. 39–43, 2011.
[5]  Sinmazçelik, T., Avcu, E., Bora, M. Ö.,  Çoban, O., “A Review: Fibre Metal Laminates, Background, Bonding Types and Applied Test Methods“ Materials & Design, Vol. 32, No. 7, pp. 3671–3685, 2011.
[6]  Xu, R., Huang, Y., Lin, Y., Bai, B.,  Huang, T., “In-Plane Flexural Behaviour and Failure Prediction of Carbon Fibre-Reinforced Aluminium Laminates“ Journal of reinforced plastics and composites, Vol. 36, No. 18, pp. 1384–1399, 2017.
[7]  Bellini, C., Di Cocco, V., Iacoviello, F.,  Sorrentino, L., “Influence of Structural Characteristics on the Interlaminar Shear Strength of Cfrp/Al Fibre Metal Laminates“ Procedia Structural Integrity, Vol. 18, pp. 373–378, 2019.
[8]  Das, R., Chanda, A., Brechou, J.,  Banerjee, A., “Impact Behaviour of Fibre-Metal Laminates“  in: Dynamic Deformation, Damage and Fracture in Composite Materials and Structures, Eds., pp. 535–598: Elsevier, 2023.
[9]  Rezghi Maleki, H.,  Parvandeh, P., “Study of the Flexural Strength and Low-Velocity Impact Behavior of Sandwich Structures with Basalt/Epoxy Face Sheets and a Cork Core“ Journal of Science and Technology of Composites, Vol. 11, No. 4, pp. 2634–2644, 2025.
[10] Khodaei, M., Safarabadi, M., Haghighi-Yazdi, M.,  Farzannia, M. A., “On the Ballistic Impact Behavior of Foam-Filled Honeycomb Core/Composite Skin Sandwich Panels“ Journal of the Brazilian Society of Mechanical Sciences and Engineering, Vol. 45, No. 5, pp. 244, 2023.
[11] Montazeri, A.,  Safarabadi, M., “A Comparative Study on Adding Chopped Kenaf Fibers to the Core of Glass/Epoxy Laminates under Quasi-Static Indentation: Experimental and Numerical Approaches“ Journal of Composite Materials, Vol. 56, No. 25, pp. 3821–3833, 2022.
[12] Sarkhosh, R., “Experimental Study of Energy Absorption Capacity of Spring-Reinforced Honeycomb Structures Filled with Polyurethane Foam under Quasi-Static Loading“ Journal of Science and Technology of Composites, Vol. 11, No. 3, pp. 2554–2562, 2024.
[13] Sarkhosh, R., “Experimental Study of Energy Absorption Characteristic of Sunflower-Inspired Foam-Filled Honeycomb Structure under out-of-Plane Loading“ Journal of Science and Technology of Composites, Vol. 11, No. 2, pp. 2512–2520, 2024.
[14] Zarei, H., Shahnazar, P., Meskini, M.,  Sarkhosh, R., “Ballistic Performance Analysis of Ultra High Molecular Weight Polyethylene (Uhmwpe) Composite“ Modares Mechanical Engineering, Vol. 22, No. 5, pp. 347–346, 2022.
[15] He, W., Wang, L., Liu, H., Wang, C., Yao, L., Li, Q.,  Sun, G., “On Impact Behavior of Fiber Metal Laminate (Fml) Structures: A State-of-the-Art Review“ Thin-Walled Structures, Vol. 167, pp. 108026, 2021.
[16] Zhou, J., Wen, P.,  Wang, S., “Numerical Investigation on the Repeated Low-Velocity Impact Behavior of Composite Laminates“ Composites Part B: Engineering, Vol. 185, pp. 107771, 2020.
[17] Demiral, M., Abbassi, F., Saracyakupoglu, T.,  Habibi, M., “Damage Analysis of a Cfrp Cross-Ply Laminate Subjected to Abrasive Water Jet Cutting“ Alexandria Engineering Journal, Vol. 61, No. 10, pp. 7669–7684, 2022.
[18] Chen, Y., Chen, L., Huang, Q.,  Zhang, Z., “Effect of Metal Type on the Energy Absorption of Fiber Metal Laminates under Low-Velocity Impact“ Mechanics of Advanced Materials and Structures, Vol. 29, No. 25, pp. 4582–4598, 2022.
[19] Vasudevan, B., Nagarajan, L., Durvasulu, R.,  Ansari, M. A., “Unlocking the Potential of Copper-Reinforced Fibre Metal Laminates: The Influence of Stacking Sequences“ Journal of Materials Research and Technology, Vol. 33, pp. 6546–6558, 2024.
[20] Jagadeesh, P., Puttegowda, M., Mavinkere Rangappa, S.,  Siengchin, S., “Influence of Nanofillers on Biodegradable Composites: A Comprehensive Review“ Polymer composites, Vol. 42, No. 11, pp. 5691–5711, 2021.
[21] Gao, H., Jiang, B., Lei, S., Hu, L., Dai, H., Cheng, Z., Li, X.,  Wang, L., “Comparisons between Basalt for Continuous Fiber and Ordinary Basalt“ Ceramics International, Vol. 51, No. 1, pp. 132–146, 2025.
[22] kumar Gara, D., Raghavendra, G.,  Prasad, P. S., “Enhanced Mechanical Properties of Glass Fibre Epoxy Composites by 2d Exfoliated Graphene Oxide Filler“ Ceramics International, Vol. 47, No. 24, pp. 34860–34868, 2021.
[23] Jamir, M. R., Majid, M. S.,  Khasri, A., “Natural Lightweight Hybrid Composites for Aircraft Structural Applications“  in: Sustainable Composites for Aerospace Applications, Eds., pp. 155–170: Elsevier, 2018.
[24] Alcaraz, M., Alderliesten, R. C.,  Mosleh, Y., “Flax‐Reinforced Aluminum (Flare): A Bio‐Based Fiber Metal Laminate Alternative Combining Impact Resistance and Vibration Damping“ Advanced Engineering Materials, Vol. 27, No. 5, pp. 2400183, 2025.
[25] Cheng, Z.-Q., Xia, J., Liu, H., Zhu, Z.-W.,  Tan, W., “Compressive Failure Mechanisms of Fibre Metal Laminates with 2/1 and 3/2 Configurations after Low-Velocity Impact“ Thin-Walled Structures, Vol. 211, pp. 113112, 2025.
[26] Hassan, M. K., Abdellah, M. Y., Azabi, S.,  Marzouk, W., “Investigation of the Mechanical Behavior of Novel Fiber Metal Laminates“ International Journal of Mechanical & Mechatronics Engineering IJMME-IJENS, Vol. 15, No. 3, pp. 112–118, 2015.
[27] Ansari, E., majzoobi, G., Rahmani, K.,  Kashfi, M., “The Effect of Middle Layer Material and Thickness on the Quasi-Static Energy Absorption of Fml“ Journal of Science and Technology of Composites, Vol. 5, No. 3, pp. 427–436, 2018.
[28] Eslami-Farsani, R., Asghari -Arpatappeh, F.,  Abdollahi -Azghan, M., “Effect of Cryogenic Environmental Condition Upon Flexural Properties of Aluminum- Epoxy/ Basalt Fibers- Glass Fibers Laminates“ Journal of Science and Technology of Composites, Vol. 6, No. 4, pp. 541–548, 2020.
[29] Abdollahi Azghan, M., Fallahnejad, M., Zamani, A.,  Eslami-Farsani, R., “Investigation the Flexural Behavior of Fiber Metal Laminates Containing Glass and Kevlar Fibers Subjected to Thermal Cycling“ Journal of Science and Technology of Composites, Vol. 7, No. 3, pp. 981–988, 2020.
[30] Malekzadeh-Fard, K., Azarnia, A. h.,  Zolghadr, N., “Analytical Modeling to Predict Dynamic Response of Fiber-Metal Laminated Panel Subjected to Low Velocity Impact“ Journal of Science and Technology of Composites, Vol. 5, No. 3, pp. 331–342, 2018.
[31] Mohamad Zaheri, F., Mohammadi, B.,  Taheri-Behrooz, F., “Study of Damage in Fiber Metal Laminate Including Matrix Cracking, Delamination and Plasticity of Metal Layer“ Journal of Science and Technology of Composites, Vol. 10, No. 4, pp. 2377–2386, 2024.
[32] Azhdari, S.,  Taheri-Behrooz, F., “An Experimental and Numerical Investigation on Bending after Impact Strength of Glass Laminate Aluminium Reinforced Epoxy“ Composites Part A: Applied Science and Manufacturing, Vol. 171, pp. 107578, 2023.
[33] Gonzalez-Canche, N., Flores-Johnson, E.,  Carrillo, J., “Mechanical Characterization of Fiber Metal Laminate Based on Aramid Fiber Reinforced Polypropylene“ Composite structures, Vol. 172, pp. 259–266, 2017.
[34] Rezghi Maleki, H.,  Parvandeh, P., “Comparison of Mechanical Properties and Low Velocity Impact Behavior of Basalt/Epoxy and Basalt/Vinyl Ester Composites“ Journal of Science and Technology of Composites, Vol. 11, No. 4, pp. 2584–2596, 2025.
[35] Astm D3039/D3039m-08 Standard Test Method for Tensile Properties of Polymer Matrix Composite Materials, ASTM.
[36] Astm D790-17 Standard Test Methods for Flexural Properties of Unreinforced and Reinforced Plastics and Electrical Insulating Materials, ASTM.
[37] Astm D7136/D7136m-15 Standard Test Method for Measuring the Damage Resistance of a Fiber-Reinforced Polymer Matrix Composite to a Drop-Weight Impact Event, ASTM.