Please use this identifier to cite or link to this item:
Title: Solid state power controller
Authors: Ng, Tze Wei
Keywords: Engineering::Electrical and electronic engineering
Issue Date: 2021
Publisher: Nanyang Technological University
Source: Ng, T. W. (2021). Solid state power controller. Final Year Project (FYP), Nanyang Technological University, Singapore.
Project: B1077-201
Abstract: The advancement of technology in the field of electrical and electronics engineering has introduced a concept and developing pattern for All-Electric and More-Electric Aircraft (MEA/AEA) system and design. A MEA has significant advantages over a conventional mechanical system in its weight, cost, and space. This will essentially allow the replacement of the non-electrical systems on a conventional aircraft such as the hydraulic and pneumatic system with an electrical system. The changes to an electrical system from a mechanical system will result in a rise of voltage level in the aircraft. Hence, constant monitoring for the electrical fault signals will be required to prevent the aircraft from damage. Thus, there is a need to replace the conventional protection devices with a Solid-StatePower Controller (SSPC). SSPC can provide a constant flow of current during the normal conditions and have a faster reaction time. This report will demonstrate the design, testing,and development of the SSPC.
Fulltext Permission: restricted
Fulltext Availability: With Fulltext
Appears in Collections:EEE Student Reports (FYP/IA/PA/PI)

Files in This Item:
File Description SizeFormat 
  Restricted Access
2.76 MBAdobe PDFView/Open

Page view(s)

Updated on May 15, 2022


Updated on May 15, 2022

Google ScholarTM


Items in DR-NTU are protected by copyright, with all rights reserved, unless otherwise indicated.