Syarifudin, Dhoni Wahyu (2022) Desain dan Prototipe Sistem Pembangkit Mandiri Menggunakan BLDC Generator Untuk Aplikasi Unmanned Aerial Vehicle. Other thesis, Institut Teknologi Sepuluh Nopember.
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Abstract
Teknologi Unmanned Aerial Vehicle (UAV) kini semakin banyak dikembangkan. Penelitian dan pengembangan dilakukan untuk menghasilkan Unmanned Aerial Vehicle (UAV) menjadi semakin efektif dan efisien dalam mengatasi keterbatasan sumber yang selama ini hanya mengandalkan baterai sebagai sumber utama. Tidak dapat dipungkiri bahwa pembangkit mandiri dalam hal ini sangat dibutuhkan untuk Unmanned Aerial Vehicle (UAV) mampu terbang lebih lama dengan daya jelajah yang lebih jauh. Penggunaan BLDC Generator sebagai pembangkit listrik mandiri menjadi sebuah pilihan karena dari segi konstruksi yang tidak memerlukan perawatan khusus, mudah dibawa kemanapun serta harga yang cukup murah.
Berdasarkan latar belakang tersebut, Penelitian ini akan membahas sebuah desain, perancangan hingga proses pembuatan prototipe sistem pembangkit mandiri menggunakan BLDC Generator. Desain sistem pembangkit terdiri dari BLDC Generator dan Gasoline Engine yang terkopel satu sama lain dengan spesifikasi yang telah ditentukan. Setelah semua komponen sistem prototipe telah terancang akan dilakukan pengujian. Pengujian dilakukan tanpa beban dan berbeban. Pada pengujian tanpa beban didapatkan tegangan maksimal sebesar 80 volt dc dengan kecepatan 11050 rpm, dan daya output yang terukur dalam keadaan berbeban sebesar 515 watt dengan kecepatan 6100 rpm.
Dari hasil penelitian didapatkan implementasi perancangan prototipe sistem pembangkit BLDC Generator dapat bekerja sesuai desain yang diinginkan, daya yang terukur sebesar 515 watt sudah memenuhi akumulasi perhitungan kebutuhan daya relative UAV jenis quadcopter saat takeoff.
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Unmanned Aerial Vehicle (UAV) technology is now increasingly being developed. Research and development is carried out to produce Unmanned Aerial Vehicles (UAVs) to be more effective and efficient in overcoming resource limitations which so far have only relied on batteries as the main source. It is undeniable that an independent generator in this case is very much needed for an Unmanned Aerial Vehicle (UAV) to be able to fly longer with a longer cruising range. The use of a BLDC Generator as an independent power plant is an option because in terms of construction that does not require special maintenance, is easy to carry anywhere and the price is quite cheap.
Based on this background, this research will discuss a design, design to the process of prototyping a self-supporting generation system using a BLDC Generator. The design of the generating system consists of a BLDC Generator and Gasoline Engine that are closely coupled with each other with predetermined specifications. After all the components of the prototype system have been designed, testing will be carried out. Testing is carried out without load and weight. In the no-load test, a maximum voltage of 80 volts dc with a speed of 11050 rpm was obtained, and the rated output power in a loaded state of 515 watts with a speed of 6100 rpm.
From the results of the study, it was obtained that the implementation of the design of the BLDC Generator generation system prototype could work according to the desired design, the measured power of 515 watts has met the accumulated calculation of the relative power needs of the quadcopter type UAV during takeoff.
Item Type: | Thesis (Other) |
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Additional Information: | RSE 621.313 2 Sya d-1 2022 |
Uncontrolled Keywords: | BLDC Generator, Prototype, Unmanned Aerial Vehicle (UAV). |
Subjects: | T Technology > TK Electrical engineering. Electronics Nuclear engineering > TK2681.B47 Electric motors, Direct current. |
Divisions: | Faculty of Intelligent Electrical and Informatics Technology (ELECTICS) > Electrical Engineering > 20201-(S1) Undergraduate Thesis |
Depositing User: | - Davi Wah |
Date Deposited: | 16 Dec 2024 02:53 |
Last Modified: | 16 Dec 2024 02:53 |
URI: | http://repository.its.ac.id/id/eprint/115974 |
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