Please use this identifier to cite or link to this item:
http://hdl.handle.net/123456789/10885
Title: | Design Optimisation Of Airbus A320 Nacelle Hinge Bracket |
Authors: | Mohamad Shukrie Bin Ab. Rashid |
Issue Date: | 15-Sep-2015 |
Abstract: | Researches have been conducted in order to reduce the weight of an aircraft. With the Additive Layer Manufacturing technology, it is a new and easier manufacturing process to produce parts of an aircraft. The design freedom of ALM ensures that the parts can be fully optimised before proceeding with the manufacturing. This research is meant to redesign the conventional nacelle hinge bracket by using Computer Aided Three-dimensional Interactive Application (CATIA) V5. It is to show that design improvements can contribute to weight saving while maintaining its strength and stiffness when performing similar tasks without fail. By optimising the design of the conventional nacelle hinge bracket, the total weight reduction managed was 20.20%. Through finite element analysis, the results obtained was promising which proved that the even though weight was reduced, the part can sustain the same load without fail. |
Description: | Bachelor of Aircraft Engineering Technology (Hons) Mechanical December 2014 |
URI: | http://localhost/xmlui/handle/123456789/10885 |
Appears in Collections: | Final Year Project - UniKL MIAT |
Files in This Item:
File | Description | Size | Format | |
---|---|---|---|---|
FYP FULL.pdf | 2.08 MB | Adobe PDF | View/Open Request a copy |
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.