The Application of Empty Palm Fruit Bunch (EPFB) As A Material for Fixed Wing Type Unmanned Aerial Vehicle Fuselage Production

  • Muhammad Teguh Teguh Mechanical Engineering Department, Universitas Riau, Indonesia
  • Kaspul Anuar Mechanical Engineering Department, Universitas Riau, Indonesia
  • Muhammad Taslim Mechanical Engineering Department, Universitas Riau, Indonesia
  • Rexy Guruh Saputra Mechanical Engineering Department, Universitas Riau, Indonesia

Abstract

One of a potential application of Empty Palm Fruit Bunch (EPFB) is the material of fuselage on Unmanned Aerial Vehicle (UAV). This study was began by Alkali Treatment on EPFB. Then, the fuselage was molded using Vacuum Bagging Method. There are three unit of mold with combination of fiberglass + carbon fiber, fiberglass + EPFB fiber and full EPFB fiber. The measurement show fuselage with hybrid composite material (fiberglass and EPFB) has the lightest mass of 559 gram. Deflection Test of all three fuselages show that the maximum deflections were under 1 mm. Next, the Static Impact Test show no damages or cracks on all three fuselages. The result of Flight Test show all fuselages could do well fly and survive belly landing.


 

##Keywords:## Empty Palm Fruit Bunch, Fuselage,Composite, Alkali Treatment
Published
Nov 30, 2019
How to Cite
TEGUH, Muhammad Teguh et al. The Application of Empty Palm Fruit Bunch (EPFB) As A Material for Fixed Wing Type Unmanned Aerial Vehicle Fuselage Production. Journal of Ocean, Mechanical and Aerospace -science and engineering-, [S.l.], v. 63, n. 3, p. 13-16, nov. 2019. ISSN 2527-6085. Available at: <https://isomase.org/Journals/index.php/jomase/article/view/133>. Date accessed: 19 aug. 2024. doi: http://dx.doi.org/10.36842/jomase.v63i3.133.

References

1. Achille S., Sismonetta G., Massimo F. 2010. Fiberglass dermatitis Clinics in Dermatology, Volume 10, Issue 2, April–June 2010, Pages 167-174.
2. Arianto,F., Burmawi., Marthiana, W. 2015. Analisa Kekuatan Tarik Dan Impak Material Komposit Dengan Variasi Panjang Serat Tkks Yang Disusun Secara Acak Menggunakan Matriks Polimer Resin Polyester.1-6.
3. Anonim.2011.Vacum BagProcess. http://mymachining.blogspot.co.id/2012/01/vacuum-bag- process. html. Diakses Tanggal 18 April 2018.
4. Badan Pusat Statistik Provinsi Riau , 2015. Luas Areal Perkebunan Kelapa Sawit. Riau : Badan Pusat Statistik.
5. Estu Nugroho, G. 2017. Karakteristik Komposit Berpenguat Serat Tandan Kosong Kelapa Sawit Menggunakan NaOH Dengan Fraksi Volume 4%, 6%, dan 8%. Skripsi.Fakultas Sains dan Teknologi Universitas Sanata Dharma, Yogyakarta.
6. Rahmasita, E,M.,Farid,M.,Ardhyananta,M.. 2017. Analisa Morfologi Serat Tandan Kosong Kelapa Sawit Sebagai Bahan Penguat Komposit Absorpsi Suara. Jurnal Teknik ITS.6. 2. 2337-3520.
7. Nugroho,G.,Budiana,O. 2017. Pengaruh Teknik Isolasi terhadap Kekuatan Tarik dan Lengkung Material Komposit pada Pembuatan Fuselage Pesawat Tanpa Awak. BKSTM-Indonesia. 9. 40-47.
8. Haryanti,A.,Norsamsi.,Sholiha,P.,Putri,N. 2014. Studi Pemanfaatan Limbah Padat Kelapa Sawit. Konversi.3. 2. 20-29.
9. Lusiani,R.,Sunardi.,Ardiansyar,Y. 2015. Pemanfaatan Limbah Tandan Kosong Kelapa Sawit Sebagai Papan Komposit Dengan Variasi Panjang Serat. Jurnal Teknik Mesin Untirta. 1. 1. 46-54.
10. Moenif, Eddon M. 2012. Potensi,Pengembangan, dan Target Implementasi Energi Terbarukan di Propinsi Riau. www.eepindonesia.org , Dinas Pertambangan dan Energi (diakses tanggal 28 Mei 2013).
11. Rahmat, Zarli R., Badri,M. 2018. Studi Karakteristik Kekuatan Tarik Dan Harga Impak Material Polymeric Foam Sandwich Panels Komposit Dengan Variasi Perlakuan Serat Tandan Kosong Sawit. JOM FTEKNIK. 5. 1. 1 - 8.
12. Savetlana, S. & Andriyanto, A. 2012.Sifat - Sifat Mekanik Komposit Serat TKKS Poliester. Jurnal Mechanical. 3. 1. 45-50.