Journal of Minerals and Materials Characterization and Engineering

Volume 5, Issue 4 (July 2017)

ISSN Print: 2327-4077   ISSN Online: 2327-4085

Google-based Impact Factor: 1  Citations  

The Effect of Atmospheric Plasma Paint Stripping on the Fatigue Crack Growth Properties of Aluminium Substrates

HTML  XML Download Download as PDF (Size: 2295KB)  PP. 161-173  
DOI: 10.4236/jmmce.2017.54014    1,322 Downloads   2,739 Views  Citations

ABSTRACT

Paint removal is a common maintenance requirement for aircraft as well as naval and land vehicles, since external paint gets damaged and loses much of its corrosion protection effectiveness with time. Paint removal is also conducted when metallic aircraft structures are inspected periodically for fatigue cracks and corrosion. The conventional methods of removing paint employed throughout the Canadian Forces mainly include chemical stripping and abrasive media blasting. Chemical stripping involves the use of hazardous chemicals, which are high in Volatile Organic Compounds (VOC) and Hazardous Air Pollutants (HAP). Abrasive media blasting typically results in a substantial quantity of solid waste consisting of paint and blast residues. Such waste is subject to control under increasingly stringent environmental and safety regulations and its disposal is costly. The new Atmospheric Plasma (AP) paint removal process purports to be a high chemical energy, low thermal energy (cold plasma process), that should not damage temperature sensitive substructures, such as heat treated aerospace aluminium alloys. Fatigue strength is one of the key properties in aircraft structures. In order for AP paint stripping to be accepted as an aerospace industry standard paint removal process, it must be thoroughly tested to demonstrate that it does not adversely affect the fatigue properties of the substrate. This paper investigates effect of the paint removal process on fatigue crack growth of 7075-T6 and 2024-T3 aluminium panels.

Share and Cite:

Merati, A. , Yanishevsky, M. , Despinic, T. and Lo, P. (2017) The Effect of Atmospheric Plasma Paint Stripping on the Fatigue Crack Growth Properties of Aluminium Substrates. Journal of Minerals and Materials Characterization and Engineering, 5, 161-173. doi: 10.4236/jmmce.2017.54014.

Cited by

[1] Removal Mechanisms and Microstructure Characteristics of Laser Paint Stripping on Aircraft Skin Surface
Photonics, 2023
[2] The investigation of paint removal by atmospheric pressure plasma jet
Plasma Science and Technology, 2023
[3] Laser Ablation of Paint from 2024-T3 Alclad Aluminum-Numerical Simulation and Experimental Characterization
2022
[4] Experimental and numerical simulation analysis of laser paint removal of aluminum alloy
Journal of Laser …, 2022
[5] Effects of laser paint stripping on oxide film damage of 2024 aluminium alloy aircraft skin
Optics …, 2021
[6] Effect of Alternative Paint Stripping Processes on the Fatigue Performance of Aluminium Alloys-Atmospheric Plasma De-painting
2019
[7] Effect of Atmospheric Plasma Paint Removal on the Fatigue Performance of 2024-T3 Aluminium Alloy Sheet
2017

Copyright © 2024 by authors and Scientific Research Publishing Inc.

Creative Commons License

This work and the related PDF file are licensed under a Creative Commons Attribution 4.0 International License.