ANALISIS GAYA DORONG (THRUST) PROPELLER PADA PESAWAT MODEL REMOTE CONTROL (UAV)

Josua Cornel Roni Sihaan, Al Munawir, Zakir Husin

Abstract


Unmanned aircraft or known as UAV (Unmanned Aerial Vehicle) is an aircraft technology that is controlled ly by the operator using  Control. The thrust is determined according to the needs of the aircraft itself. This study uses a thrust test stand that uses a mass measuring device as a measuring force, using a brushless motor and 3 different types of propellers, namely propeller two with a size of 8 x 4 inches and 10 x 7 inches, three propellers with a size of 6 x 3 inc to determine the optimal thrust for missions flying -controlled model aircraft (UAV). After testing, it was found that the smallest thrust force of the 6x3 inch blade type propeller, on this type of propeller only 3,874 N of thrust is produced at 100% throttle percentage and uses a 3 cell battery. While the greatest thrust generated from the propeller with a type of two when 10x7 inches, on this propeller and using a 4 cell battery can produce a Thrust of 13,194 N with a percentage of full throttle or 100%. The thrust required for the aircraft to fly cruising in the air is 0.806 N, while the thrust required for the aircraft to take off is 6.513 N.

Keywords: Control Model Aircraft, Propeller, Thrust

Full Text:

PDF

References


Hernawan Kristianto (2015), Kontrol Daya Dorong Pesawat Terhadap Perubahan Flow Udara, Universitas Brawijaya

Saroinsong, H.S., Poekoel, V.C. dan Pinrolinvic D.K Manembu (2018), Rancang Bangun Wahana Pesawat Tanpa Awak (Fixed Wing) Berbasis Ardupilot, TEKNIK ELEKTRO dan KOMPUTER, 7(1), 2301–8402.

Ananda R.R.A, Mufti A, dan Endah Y (2020), Estimasi Gaya Dorong Dari Motor Brushless Dengan Variasi Propeller Untuk Pesawat Model X-UAV Mini Talon Dengan Menggunakan Pengukur Massa. Jurnal Teknologi Kedirgantaraan, Vol, V No. 2, Agustus 2020

Jakubowski, A. 2015 . Analysis Thrust for Different Kind of Propellers. Institute of Mechanical Technology, Poznan University of Technology, Poznan .

Miftah Ilhami (2015), Rancang Bangun Pesawat Uav Hexacopter Dengan Kendali Pid, Institut Teknologi Sepuluh Nopember Surabaya.

Utomo A. B, Derajat dan Aman Q (2017), Perhitungan Gaya Dorong Pesawat N219 Dengan Menggunakan Pemodelan Matematik Dari Data Engine Deck Pesawat N219, Seminar Nasional Iptek Penerbangan dan Antariksa XXI-2017.

Atmasari N, Muksin , Hartono dan Ryan (2020), Analysis of Engine and Propeller Selection for Unmanned Aircraft LSU-05 NG, Angkasa Jurnal Ilmiah Bidang Teknologi

Nopias B, Muhajir K dan Toto R (2017), Pengaruh Gaya Dorong Propeler Pada Engine Fora Terhadap Kecepatan Pesawat Model F2d Combat, Jurnal Teknologi, Vol 10, No 1, Juni 2017 59-64.

Randis, Dharmawan I.B dan Syahruddin (2017), Rancang Bangun Alat Uji Gaya Dorong (Trust Force) Motor Brushless, jurnal teknologi terpadu vol. 5 no. 2 oktober 2017.

Adiansyah Y ,Isranuri I, Alfian H ,Sabri M, Bustami (2018), simulasi tegangan propeller al-mg yang dirancang untuk propeller rendah bising, Jurnal Dinamis, Vol.6, No.3 September 2018 ISSN 0216-7492.

Ardhianto , Kurniawan. 2011. Desain dan Analisis Propeller pada Unmanned Aerial Vehicle (UAV). AAU Journal of Defense Science and Technology Volume 2, Number 1, 1 July 2011, 125 – 133.

Tri hartanto (2015), Analisa aerodinamika flap dan slat pada airfoil naca 2410 terhadap koefisien lift dan koefisien drag dengan metode computational fluid dynamic. Naskah publikasi karya ilmiah, muhammadiyah surakarta




DOI: https://doi.org/10.35308/jmkn.v8i1.5698

Refbacks

  • There are currently no refbacks.


Creative Commons License
This work is licensed under a Creative Commons Attribution-ShareAlike 4.0 International License.