Adhesion and characterization of the interface between aerospace standard primer and anodized aluminium alloy

In aerospace industry, aluminum alloys have been the material of choice when it comes to building the fuselage, wing and supporting structure of modern passenger aircraft, military cargo and transport since 1930 [1]. Aluminum alloys are chosen due to their well-known performance characteristics, kno...

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Main Author: Toh, Xin Hui
Other Authors: Li Hua
Format: Final Year Project
Language:English
Published: 2015
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Online Access:http://hdl.handle.net/10356/64057
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-640572023-03-04T18:24:55Z Adhesion and characterization of the interface between aerospace standard primer and anodized aluminium alloy Toh, Xin Hui Li Hua School of Mechanical and Aerospace Engineering A*STAR Singapore Institute of Manufacturing Technology DRNTU::Engineering::Aeronautical engineering::Aircraft In aerospace industry, aluminum alloys have been the material of choice when it comes to building the fuselage, wing and supporting structure of modern passenger aircraft, military cargo and transport since 1930 [1]. Aluminum alloys are chosen due to their well-known performance characteristics, known fabrication costs, design experience, resistance to corrosion and high strength to weight ratio that will increase payload and save in fuel consumption. They usually undergo anodizing as a surface treatment to further enhance their protection against corrosion and to increase adhesion to paint. However, it has been understood that most paint adhesion problems are mainly due to delamination between the primer and the sealed anodic surface. Therefore, in this project, AA2024 specimens will be anodized under MIL-A-8625F Type II to understand the adhesion and characterization of the interface between the anodized aluminum alloy surface and two standard commercial aerospace primers A) with chromate, and B) chromate free. Three intrinsic factors have been designed to be taken into consideration for our experiments. They are the temperature used during the experiment, the presence of nickel incorporated in the sealing process and the presence of chromate in the primer. Two factors have been identified to be significant. The presence of nickel in the sealing process and chromate in the primer has shown to be more beneficial to adhesion. As such, it is vital to locate nickel further in the anodized oxide layer as the results from Scanning Electron Microscope (SEM) are not able to detect the nickel in the top sample surface as the total average over the surface is lower than 5 atomic percent. Bachelor of Engineering (Mechanical Engineering) 2015-05-22T07:30:21Z 2015-05-22T07:30:21Z 2015 2015 Final Year Project (FYP) http://hdl.handle.net/10356/64057 en Nanyang Technological University 46 p. application/pdf
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic DRNTU::Engineering::Aeronautical engineering::Aircraft
spellingShingle DRNTU::Engineering::Aeronautical engineering::Aircraft
Toh, Xin Hui
Adhesion and characterization of the interface between aerospace standard primer and anodized aluminium alloy
description In aerospace industry, aluminum alloys have been the material of choice when it comes to building the fuselage, wing and supporting structure of modern passenger aircraft, military cargo and transport since 1930 [1]. Aluminum alloys are chosen due to their well-known performance characteristics, known fabrication costs, design experience, resistance to corrosion and high strength to weight ratio that will increase payload and save in fuel consumption. They usually undergo anodizing as a surface treatment to further enhance their protection against corrosion and to increase adhesion to paint. However, it has been understood that most paint adhesion problems are mainly due to delamination between the primer and the sealed anodic surface. Therefore, in this project, AA2024 specimens will be anodized under MIL-A-8625F Type II to understand the adhesion and characterization of the interface between the anodized aluminum alloy surface and two standard commercial aerospace primers A) with chromate, and B) chromate free. Three intrinsic factors have been designed to be taken into consideration for our experiments. They are the temperature used during the experiment, the presence of nickel incorporated in the sealing process and the presence of chromate in the primer. Two factors have been identified to be significant. The presence of nickel in the sealing process and chromate in the primer has shown to be more beneficial to adhesion. As such, it is vital to locate nickel further in the anodized oxide layer as the results from Scanning Electron Microscope (SEM) are not able to detect the nickel in the top sample surface as the total average over the surface is lower than 5 atomic percent.
author2 Li Hua
author_facet Li Hua
Toh, Xin Hui
format Final Year Project
author Toh, Xin Hui
author_sort Toh, Xin Hui
title Adhesion and characterization of the interface between aerospace standard primer and anodized aluminium alloy
title_short Adhesion and characterization of the interface between aerospace standard primer and anodized aluminium alloy
title_full Adhesion and characterization of the interface between aerospace standard primer and anodized aluminium alloy
title_fullStr Adhesion and characterization of the interface between aerospace standard primer and anodized aluminium alloy
title_full_unstemmed Adhesion and characterization of the interface between aerospace standard primer and anodized aluminium alloy
title_sort adhesion and characterization of the interface between aerospace standard primer and anodized aluminium alloy
publishDate 2015
url http://hdl.handle.net/10356/64057
_version_ 1759858058183311360