System integration and counter-mass balance of fuel cell powered UAV / Mohd Hafiz Hussim

The primary objective of the study is to integrate a fuel cell, hydrogen tanks, brushless DC motor and other equipments. The invention of the fuel cell has brought new clean energy to industries, transportation and electrical appliances around the world, the problem are the past fuel cell system hav...

Full description

Saved in:

Bibliographic Details
Main Author:	Hussim, Mohd Hafiz
Format:	Thesis
Language:	English
Published:	2009
Subjects:	Power resources Machine design and drawing Renewable energy sources
Online Access:	https://ir.uitm.edu.my/id/eprint/36519/1/36519.pdf
Tags:	Add Tag No Tags, Be the first to tag this record!

id	my-uitm-ir.36519
record_format	uketd_dc
spelling	my-uitm-ir.365192020-11-12T04:16:33Z System integration and counter-mass balance of fuel cell powered UAV / Mohd Hafiz Hussim 2009 Hussim, Mohd Hafiz Power resources Machine design and drawing Renewable energy sources The primary objective of the study is to integrate a fuel cell, hydrogen tanks, brushless DC motor and other equipments. The invention of the fuel cell has brought new clean energy to industries, transportation and electrical appliances around the world, the problem are the past fuel cell system have had a low power to weight ratio. System integration is the bringing together of the component subsystems into one system and ensuring that the subsystems function together as a system. Every component like the hydrogen tank, the fuel cell, the brushless DC motor and the servos must be placed on the suitable place to ensure the space inside the structure to be completely occupied and the weight distribution for the whole UAV is right. Every component's weight must be measured first before it is placed on the UAV. For this semester, the other focus was fabricating the airframe of the UAV. As the fabrication goes on, the countermass balance of the UAV is also determined. The calculation was done by considering the Center of Pressure, Center of Gravity, the weight and length of the whole structure and some other parameters. 2009 Thesis https://ir.uitm.edu.my/id/eprint/36519/ https://ir.uitm.edu.my/id/eprint/36519/1/36519.pdf text en public degree Universiti Teknologi MARA Faculty of Mechanical Engineering Thomas, Arthur Ward (Dr)
institution	Universiti Teknologi MARA
collection	UiTM Institutional Repository
language	English
advisor	Thomas, Arthur Ward (Dr)
topic	Power resources Machine design and drawing Renewable energy sources
spellingShingle	Power resources Machine design and drawing Renewable energy sources Hussim, Mohd Hafiz System integration and counter-mass balance of fuel cell powered UAV / Mohd Hafiz Hussim
description	The primary objective of the study is to integrate a fuel cell, hydrogen tanks, brushless DC motor and other equipments. The invention of the fuel cell has brought new clean energy to industries, transportation and electrical appliances around the world, the problem are the past fuel cell system have had a low power to weight ratio. System integration is the bringing together of the component subsystems into one system and ensuring that the subsystems function together as a system. Every component like the hydrogen tank, the fuel cell, the brushless DC motor and the servos must be placed on the suitable place to ensure the space inside the structure to be completely occupied and the weight distribution for the whole UAV is right. Every component's weight must be measured first before it is placed on the UAV. For this semester, the other focus was fabricating the airframe of the UAV. As the fabrication goes on, the countermass balance of the UAV is also determined. The calculation was done by considering the Center of Pressure, Center of Gravity, the weight and length of the whole structure and some other parameters.
format	Thesis
qualification_level	Bachelor degree
author	Hussim, Mohd Hafiz
author_facet	Hussim, Mohd Hafiz
author_sort	Hussim, Mohd Hafiz
title	System integration and counter-mass balance of fuel cell powered UAV / Mohd Hafiz Hussim
title_short	System integration and counter-mass balance of fuel cell powered UAV / Mohd Hafiz Hussim
title_full	System integration and counter-mass balance of fuel cell powered UAV / Mohd Hafiz Hussim
title_fullStr	System integration and counter-mass balance of fuel cell powered UAV / Mohd Hafiz Hussim
title_full_unstemmed	System integration and counter-mass balance of fuel cell powered UAV / Mohd Hafiz Hussim
title_sort	system integration and counter-mass balance of fuel cell powered uav / mohd hafiz hussim
granting_institution	Universiti Teknologi MARA
granting_department	Faculty of Mechanical Engineering
publishDate	2009
url	https://ir.uitm.edu.my/id/eprint/36519/1/36519.pdf
_version_	1783734343143784448

System integration and counter-mass balance of fuel cell powered UAV / Mohd Hafiz Hussim

Similar Items