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Fabrication of a test bed for performance testing of Unmanned Aerial Vehicle (UAV) propulsion system

This project report has been conducted because of the Unmanned Aerial Vehicle (UAV) power plant development performance testing (static test) facilities is not fully deployed. The main purpose of this project is to fabricate a test bed for the UAV propulsion system. To test the capability of measuri...

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Main Author: Adib, Azmi
Format: Undergraduates Project Papers
Language:English
Published: 2013
Subjects:
TA Engineering (General). Civil engineering (General)
Online Access:http://umpir.ump.edu.my/id/eprint/10631/1/FKM-DIPLOMA-ADIB%20BIN%20AZMI.pdf
http://umpir.ump.edu.my/id/eprint/10631/
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spelling my.ump.umpir.106312016-07-12T08:03:31Z http://umpir.ump.edu.my/id/eprint/10631/ Fabrication of a test bed for performance testing of Unmanned Aerial Vehicle (UAV) propulsion system Adib, Azmi TA Engineering (General). Civil engineering (General) This project report has been conducted because of the Unmanned Aerial Vehicle (UAV) power plant development performance testing (static test) facilities is not fully deployed. The main purpose of this project is to fabricate a test bed for the UAV propulsion system. To test the capability of measuring aircraft performance namely thrust, available power, brake shaft power, propulsive efficiency, brake specific fuel consumption and thrust coefficient. In this study, the test bed model was designed to test the nitro engine Radio Control (RC) which is a model of Thunder Tiger PRO .36. The unknown value of parameters can be determined by reading the sensors. Some sketches software had been used such as Autocad and Solidwork to draft out the shape of the test bed. The fabrication process for this project must through a lot of process that must be followed step by step. This is to ensure that the design had been fabricated by following the design specification. From this experiment, the result shows that the fabricated test bed can be used to study the engine performance and performance parameters are directly proportional to the engine speed which mean the speed of the engine affects the increasing of the parameters. Some methods of improvement for the combination of test bed are also provided for further improvement of the test bed. As the conclusion, all the engine performance parameter can be calculated from the test bed. 2013-06 Undergraduates Project Papers NonPeerReviewed application/pdf en http://umpir.ump.edu.my/id/eprint/10631/1/FKM-DIPLOMA-ADIB%20BIN%20AZMI.pdf Adib, Azmi (2013) Fabrication of a test bed for performance testing of Unmanned Aerial Vehicle (UAV) propulsion system. Faculty of Mechanical Engineering, Universiti Malaysia Pahang.
institution Universiti Malaysia Pahang
building UMP Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Malaysia Pahang
content_source UMP Institutional Repository
url_provider http://umpir.ump.edu.my/
language English
topic TA Engineering (General). Civil engineering (General)
spellingShingle TA Engineering (General). Civil engineering (General)
Adib, Azmi
Fabrication of a test bed for performance testing of Unmanned Aerial Vehicle (UAV) propulsion system
description This project report has been conducted because of the Unmanned Aerial Vehicle (UAV) power plant development performance testing (static test) facilities is not fully deployed. The main purpose of this project is to fabricate a test bed for the UAV propulsion system. To test the capability of measuring aircraft performance namely thrust, available power, brake shaft power, propulsive efficiency, brake specific fuel consumption and thrust coefficient. In this study, the test bed model was designed to test the nitro engine Radio Control (RC) which is a model of Thunder Tiger PRO .36. The unknown value of parameters can be determined by reading the sensors. Some sketches software had been used such as Autocad and Solidwork to draft out the shape of the test bed. The fabrication process for this project must through a lot of process that must be followed step by step. This is to ensure that the design had been fabricated by following the design specification. From this experiment, the result shows that the fabricated test bed can be used to study the engine performance and performance parameters are directly proportional to the engine speed which mean the speed of the engine affects the increasing of the parameters. Some methods of improvement for the combination of test bed are also provided for further improvement of the test bed. As the conclusion, all the engine performance parameter can be calculated from the test bed.
format Undergraduates Project Papers
author Adib, Azmi
author_facet Adib, Azmi
author_sort Adib, Azmi
title Fabrication of a test bed for performance testing of Unmanned Aerial Vehicle (UAV) propulsion system
title_short Fabrication of a test bed for performance testing of Unmanned Aerial Vehicle (UAV) propulsion system
title_full Fabrication of a test bed for performance testing of Unmanned Aerial Vehicle (UAV) propulsion system
title_fullStr Fabrication of a test bed for performance testing of Unmanned Aerial Vehicle (UAV) propulsion system
title_full_unstemmed Fabrication of a test bed for performance testing of Unmanned Aerial Vehicle (UAV) propulsion system
title_sort fabrication of a test bed for performance testing of unmanned aerial vehicle (uav) propulsion system
publishDate 2013
url http://umpir.ump.edu.my/id/eprint/10631/1/FKM-DIPLOMA-ADIB%20BIN%20AZMI.pdf
http://umpir.ump.edu.my/id/eprint/10631/
_version_ 1643666443380719616
score 13.211869

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