Proceedings of the Adisutjipto Aerospace, Science and Engineering International Conference (AASEIC 2024)

Performance Analysis of a 2-Blades Propeller Design for USV (Unmanned Surface Vehicle)

Authors
Rochmad Eko Prasetyaning Utomo1, *, Prabuditya Bhisma Wisnu Wardhana1, Mega Lazuardi Umar1, Agung Fauzi Hanafi1
1Politeknik Negeri Banyuwangi, Banyuwangi, 68461, Indonesia
*Corresponding author. Email: rochmad@poliwangi.ac.id
Corresponding Author
Rochmad Eko Prasetyaning Utomo
Available Online 31 March 2025.
DOI
10.2991/978-94-6463-668-0_7How to use a DOI?
Keywords
Pitch Blade Analysis; 2 Blades Propeller; Unmanned Surface Vehicle
Abstract

USV (Unmanned Surface Vehicle) is a tool that can facilitate human work. Conducting surveys, searching in vulnerable areas, mapping, or even exploring for a long time can be done easily by USV. USV technology is currently experiencing very rapid progress. However, this sophistication cannot be separated from USV’s main need, which is to move. To move the USV requires a force which is commonly referred to as thrust. The required thrust is usually generated through a certain instrument, in this case the propeller. Different propeller design would produce different thrust. Likewise with the obstacles from the shape of the USV building itself, it will also provide different obstacles. So it is necessary to do a study to find out which propeller fits a certain USV shape. Every USV needs special propeller design based on the USV design to optimize the energy consumption. In this observation an adjustment will be made to the pitch of the propeller. So that the maximum thrust required by USV can be obtained. In this study the performance of propeller will be observe. With the motor that can produced various rpm. Modeling will be carried out with measurable parameters for each design that has been made, then an analysis will be carried out to find out which design has the best thrust. The results of the observations show the increase of power are influenced by the increase of rpm. Maximum increase of power has been surpassed the power of stock model propeller.

Copyright
© 2025 The Author(s)
Open Access
Open Access This chapter is licensed under the terms of the Creative Commons Attribution-NonCommercial 4.0 International License (http://creativecommons.org/licenses/by-nc/4.0/), which permits any noncommercial use, sharing, adaptation, distribution and reproduction in any medium or format, as long as you give appropriate credit to the original author(s) and the source, provide a link to the Creative Commons license and indicate if changes were made.

Download article (PDF)

Volume Title
Proceedings of the Adisutjipto Aerospace, Science and Engineering International Conference (AASEIC 2024)
Series
Advances in Engineering Research
Publication Date
31 March 2025
ISBN
978-94-6463-668-0
ISSN
2352-5401
DOI
10.2991/978-94-6463-668-0_7How to use a DOI?
Copyright
© 2025 The Author(s)
Open Access
Open Access This chapter is licensed under the terms of the Creative Commons Attribution-NonCommercial 4.0 International License (http://creativecommons.org/licenses/by-nc/4.0/), which permits any noncommercial use, sharing, adaptation, distribution and reproduction in any medium or format, as long as you give appropriate credit to the original author(s) and the source, provide a link to the Creative Commons license and indicate if changes were made.

Cite this article

TY  - CONF
AU  - Rochmad Eko Prasetyaning Utomo
AU  - Prabuditya Bhisma Wisnu Wardhana
AU  - Mega Lazuardi Umar
AU  - Agung Fauzi Hanafi
PY  - 2025
DA  - 2025/03/31
TI  - Performance Analysis of a 2-Blades Propeller Design for USV (Unmanned Surface Vehicle)
BT  - Proceedings of the Adisutjipto Aerospace, Science and Engineering International Conference (AASEIC 2024)
PB  - Atlantis Press
SP  - 48
EP  - 56
SN  - 2352-5401
UR  - https://doi.org/10.2991/978-94-6463-668-0_7
DO  - 10.2991/978-94-6463-668-0_7
ID  - Utomo2025
ER  -