Pemanfaatan Serabut Kelapa sebagai Bahan Pembuatan Rangka Drone

Muhammad Ikhsan; Indra  Permana; Riza Arif  Pratama; Sahid Bayu  Setiajit; Dimas Ahsan  Assidiqi; Sandy Laila Suci  Ramadhani

doi:10.37031/jt.v23i1.524

Muhammad Ikhsan Universitas Tunas Pembangunan Surakarta
Indra Permana Universitas Tunas Pembangunan Surakarta
Riza Arif Pratama Universitas Tunas Pembangunan Surakarta
Sahid Bayu Setiajit Universitas Tunas Pembangunan Surakarta
Dimas Ahsan Assidiqi Universitas Tunas Pembangunan Surakarta
Sandy Laila Suci Ramadhani Universitas Tunas Pembangunan Surakarta

DOI: https://doi.org/10.37031/jt.v23i1.524

Abstract

Drones are one of the latest technologies that are developing rapidly to provide positive benefits in society. Drone development can be done in various ways, including by improving the performance of the drone frame. Drone frames can be made of various types of materials, one of which is composite material that has mechanical properties that can be adjusted to needs. In this study, coconut fiber was chosen as the composite material because of its abundant availability, light weight, and environmentally friendly. Coconut fiber composites are made to be one of the alternatives for drone frames. To overcome its low strength, coconut fiber is used together with fiberglass to become a hybrid composite. Tensile tests, bending tests, and impact tests were carried out to determine the mechanical characteristics of the hybrid composite. The test results are then used as the basis for determining the drone design. Two types of tensile test specimens were made using the hand lay-up method where the type of fiber was varied to see the effect of variations in fiber types on the strength of the composite. The first type is a composite with fiber in the form of coconut fiber mats and fiberglass mats, and the second type is a composite with fiber in the form of coconut fiber mats and WR (Woven Roving) fiberglass. The tensile test results show that the second type of composite is more recommended because of its higher strength and more consistent results. The test results show that the second type of composite has a tensile strength of 32.7 MPa, a flexural strength of 82.4 MPa, and is able to absorb impact energy of 2.34 Joules. And finally, in this research, the hybrid composite was made into a drone frame and then integrated with electrical components so that the drone can fly

Keywords: coconut fiber, drone frame, composite, mechanical properties

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References

Akil, Hm., Omar, M. F., Mazuki, A. A. M., Safiee, S., Ishak, Z. A. M., & Bakar, A. A. (2011). Kenaf fiber reinforced composites: A review. Materials & Design, 32(8–9), 4107–4121.

Aparna, A.R., Shamanth, P.V., Fernandes, A.J., Janani, B.S., Chaitra, G., Bhansali, D., Raju, D.S., Kumar, N. (2024). EMI Shielding Materials in Drones. AAJ, 3(4) 545-552. DOI: 10.61359/11.2106-2456.

Badan Pusat Statistik Indonesia. (2022, Maret 31). Produksi Perkebunan Rakyat Menurut Jenis Tanaman, 2021. https://www.bps.go.id/id/statistics- table/2/NzY4IzI%3D/produksi-perkebunan-rakyat-menurut-jenis-tanaman.html

Bangkui, F.A.N., Yun, L., Ruiyu, Z., Qiqi, F.U. (2020). Review on the Technological Development Application of UAV Systems. CJE, 29(2), 199-207. DOI: 10.1049/cje.2019.12.006.

Cikal, A. (2024). Pengembangan Komposit Serat Alam Limbah Sabut Kelapa untuk Aplikasi Industri Berkelanjutan. SENS 9, 9(1), 433-435.

Gundara, G., & Nur Rahman, M. B. (2019). Sifat Tarik, Bending dan Impak Komposit Serat Sabut Kelapa-Polyester dengan Variasi Fraksi Volume. JMPM (Jurnal Material dan Proses Manufaktur), 3(1). https://doi.org/10.18196/jmpm.3132

Harika, C., Kumar, A.S., & Rao, M.V.R. (2024). Comparative Study on Effect of Material on structural Performance of a Quadcopter Drone with 'X- Frame'. Journal of Physics: Conference Series 2837. DOI:10.1088/1742-6596/2837/1/012099.

Ikhsan, M., Permana, I., Pratama, R. A., Setiajit, S. B. (2024) Pengembangan Komposit Serat Sabut Kelapa Sebagai Bahan Pembuatan Rangka Surveillance Drone. Teknika STTKD: Jurnal Teknik, Elektronik, Engine. DOI:10.56521/teknika.v10i1.1048.

Ilham, Bakri, & Magga, R. (2019). Sifat Kuat Tarik Material Komposit Hibrid Berpenguat Serat Ijuk dan Sabut Kelapa dengan Orientasi Serat Acak. Jurnal Mekanikal, 10(2), 980–991.

Mawardi, I., & Hanif. (2018). Sifat Mekanis Komposit Polimer Hibrid Diperkuat Serat Sabut Kelapa-E-Glass. Ethos, 6(2), 297–304.

Mittal, O., Sahu, A., & Kulkarni, N. (2024). Design of Multi-Rotor Flying Wing Configuration Quadplane Unmanned Aerial Vehicle. AAJ, 3(3), 495-504. DOI: 10.61359/11.2106-2447.

Putra, F. U., Paundra, F., Muhyi, A., Hakim, F., Triawan, L., & Aziz, A. (2023). Pengaruh Variasi Tekanan dan Fraksi Volume pada Hybrid Composite Serat Sabut Kelapa dan Serat Bambu Bermatriks Resin Polyester terhadp Kekuatan Tarik dan Bending. Foundry, 6(1), 8–15.

Rajoo, P. G., Thariq, M., Sultan, H., Syazwani Shahar, F., Łukaszewicz, A., Basri, A. A., Umaira, A., Shah, M., Nayak, S. Y., Grzejda, R., & Holovatyy, A. (2023). The Development of UAV Airframes Made of Natural Fibers: A Review. Preprints. https://doi.org/10.20944/preprints202307.0528.v1

Retyo Titani, F., Logys Imalia, C., & Haryanto. (2018). Pemanfaatan Serat Sabut Kelapa Sebagai Material Penguat Pengganti Fiberglass Pada Komposit Resin Polyester Untuk Aplikasi Bahan Konstruksi Pesawat Terbang. Techno, 19(1), 23–28. http://jurnalnasional.ump.ac.id/index.php/Techno

Setiajit, S. B., Permana, I., Ikhsan, M. (2024). Studi Variasi Fraksi Berat Terhadap Kekuatan Tarik Glass Fiber Reinforced Polymer Hybrid Sabut Kelapa. Teknika STTKD: Jurnal Teknik, Elektronik, Engine, 9(1), 96-102.

Shelake, P.R., Ambad, T.M., Kumbhar, B.B., Deshmukh, B.M., & Jadhav, A.A. (2024). Fabrication of Drone Components by Using Composite Glass Fibre. IJSRSET, 11(7), 993-998.

Siswanto, Wiyono, T., Heru Sudargo, P., & Rachmadi, A. (2023). Studi Rekayasa Peningkatan Sifat Mekanik Komposit Polyester Berpenguat Serat Ampas Tebu dengan Menggunakan Silane Coupling Agent. Teknika, 8(1), 66–71.

Somasekhar, Y. (2024). Indigenous Multi-Role X-Quadcopter: Design, Development, Advancements and its Applications. AAJ, 3(3), 479-486. DOI: 10.61359/11.2106-2445.

Sulistyo, A.B., & Wirawan, W.A. (2024). Evaluation of Tensile Strength and Flexural Strength of GFRP Composites in different types of matrix polymers. Journal of Achievements in Materials and Manufacturing Engineering, 123(2), 49-57. https://doi.org/10.5604/01.3001.0054.6847.

Suprayogi, A., Permana, I., dan Setiajit, S.B. (2025). Gaya Tarik Maksimal Komposit GFRP dengan Metode Hand Lay-Up pada Variasi Ketebalan. JTREMM, 1(1), 26-31.

Wijaya, D., & Hidayat, S. (2022). Pengaruh Fraksi Volume Serat pada Komposit Hibrid Serat Tebu dan Serat Sabut Kelapa terhadap Kekuatan Tarik. Prosiding The 13th Industrial Research Workshop and National Seminar, 78–83.

Zulkifli, Bagus Dharmawan, I., & Anhar, W. (2020). Analisa pengaruh perlakuan kimia pada serat terhadap kekuatan impak charpy komposit serat sabut kelapa bermatriks epoxy. Jurnal Polimesin, 18(1), 47–52.


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