Development of solid-state power controller for aerospace applications
There is a developing pattern towards progressively more electric aircraft (MEA) design and system with an expanded number of converters/inverters and electronic circuits. As the electronic system has a favourable position over the conventional mechanical system, the pressure-driven system as far as...
Saved in:
Main Author: | |
---|---|
Other Authors: | |
Format: | Final Year Project |
Language: | English |
Published: |
Nanyang Technological University
2020
|
Subjects: | |
Online Access: | https://hdl.handle.net/10356/139776 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Institution: | Nanyang Technological University |
Language: | English |
id |
sg-ntu-dr.10356-139776 |
---|---|
record_format |
dspace |
spelling |
sg-ntu-dr.10356-1397762023-07-07T18:30:07Z Development of solid-state power controller for aerospace applications Low, Adrian Wei Chuan Su Rong School of Electrical and Electronic Engineering RSu@ntu.edu.sg Engineering::Electrical and electronic engineering There is a developing pattern towards progressively more electric aircraft (MEA) design and system with an expanded number of converters/inverters and electronic circuits. As the electronic system has a favourable position over the conventional mechanical system, the pressure-driven system as far as weight, cost, space, and productivity. An aeroplane joint strike contender (JSP) which enhances progressively on electronic innovation and a 270 VDC appropriation transport, is an exemplary case of MEA. Since in the semi-conductor region are improving thus, granting more opportunities for electronic designs and system, which are called Solid-state power controller (SSPC). Contrasted with customary electromechanical devices, SSPCs generally give quicker reaction time and greater power conversion capability. The establishment of MOSFETs/IGBTs in SSPC that can inexact the conduct of a perfect switch. SSPC includes a wide scope of circuit parts and various sorts of protections. This project habitat a fragment of an entire SSPC which is used to perceive arc faults in the system Bachelor of Engineering (Electrical and Electronic Engineering) 2020-05-21T07:43:19Z 2020-05-21T07:43:19Z 2020 Final Year Project (FYP) https://hdl.handle.net/10356/139776 en application/pdf Nanyang Technological University |
institution |
Nanyang Technological University |
building |
NTU Library |
continent |
Asia |
country |
Singapore Singapore |
content_provider |
NTU Library |
collection |
DR-NTU |
language |
English |
topic |
Engineering::Electrical and electronic engineering |
spellingShingle |
Engineering::Electrical and electronic engineering Low, Adrian Wei Chuan Development of solid-state power controller for aerospace applications |
description |
There is a developing pattern towards progressively more electric aircraft (MEA) design and system with an expanded number of converters/inverters and electronic circuits. As the electronic system has a favourable position over the conventional mechanical system, the pressure-driven system as far as weight, cost, space, and productivity. An aeroplane joint strike contender (JSP) which enhances progressively on electronic innovation and a 270 VDC appropriation transport, is an exemplary case of MEA. Since in the semi-conductor region are improving thus, granting more opportunities for electronic designs and system, which are called Solid-state power controller (SSPC). Contrasted with customary electromechanical devices, SSPCs generally give quicker reaction time and greater power conversion capability. The establishment of MOSFETs/IGBTs in SSPC that can inexact the conduct of a perfect switch. SSPC includes a wide scope of circuit parts and various sorts of protections. This project habitat a fragment of an entire SSPC which is used to perceive arc faults in the system |
author2 |
Su Rong |
author_facet |
Su Rong Low, Adrian Wei Chuan |
format |
Final Year Project |
author |
Low, Adrian Wei Chuan |
author_sort |
Low, Adrian Wei Chuan |
title |
Development of solid-state power controller for aerospace applications |
title_short |
Development of solid-state power controller for aerospace applications |
title_full |
Development of solid-state power controller for aerospace applications |
title_fullStr |
Development of solid-state power controller for aerospace applications |
title_full_unstemmed |
Development of solid-state power controller for aerospace applications |
title_sort |
development of solid-state power controller for aerospace applications |
publisher |
Nanyang Technological University |
publishDate |
2020 |
url |
https://hdl.handle.net/10356/139776 |
_version_ |
1772828016928358400 |