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Characterization Studies on Graphene-Aluminium Nano Composites for Aerospace Launch Vehicle External Fuel Tank Structural Application

From the aspect of exploring the alternative lightweight composite material for the aerospace launch vehicle external fuel tank structural components, the current research work studies three different grades of Aluminium alloy reinforced with varying graphene weight percentages that are processed th...

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Autores principales: Jayaseelan, Joel, Pazhani, Ashwath, Michael, Anthony Xavior, Paulchamy, Jeyapandiarajan, Batako, Andre, Hosamane Guruswamy, Prashantha Kumar
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2022
Materias:
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9456592/
https://www.ncbi.nlm.nih.gov/pubmed/36079286
http://dx.doi.org/10.3390/ma15175907
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author Jayaseelan, Joel
Pazhani, Ashwath
Michael, Anthony Xavior
Paulchamy, Jeyapandiarajan
Batako, Andre
Hosamane Guruswamy, Prashantha Kumar
author_facet Jayaseelan, Joel
Pazhani, Ashwath
Michael, Anthony Xavior
Paulchamy, Jeyapandiarajan
Batako, Andre
Hosamane Guruswamy, Prashantha Kumar
author_sort Jayaseelan, Joel
collection PubMed
description From the aspect of exploring the alternative lightweight composite material for the aerospace launch vehicle external fuel tank structural components, the current research work studies three different grades of Aluminium alloy reinforced with varying graphene weight percentages that are processed through powder metallurgy (P/M) route. The prepared green compacts composite ingots are subjected to microwave processing (Sintering), hot extruded, and solution treated (T6). The developed Nano-graphene reinforced composite is studied further for the strength–microstructural integrity. The nature of the graphene reinforcement and its chemical existence within the composite is further studied, and it is found that hot extruded solution treated (HEST) composite exhibited low levels of carbide (Al(4)C(3)) formations, as composites processed by microwaves. Further, the samples of different grades reinforced with varying graphene percentages are subjected to mechanical characterisation tests such as the tensile test and hardness. It is found that 2 wt% graphene reinforced composites exhibited enhanced yield strength and ultimate tensile strength. Microstructural studies and fracture morphology are studied, and it is proven that composite processed via the microwave method has exhibited good ductile behaviour and promising failure mechanisms at higher load levels.
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spelling pubmed-94565922022-09-09 Characterization Studies on Graphene-Aluminium Nano Composites for Aerospace Launch Vehicle External Fuel Tank Structural Application Jayaseelan, Joel Pazhani, Ashwath Michael, Anthony Xavior Paulchamy, Jeyapandiarajan Batako, Andre Hosamane Guruswamy, Prashantha Kumar Materials (Basel) Article From the aspect of exploring the alternative lightweight composite material for the aerospace launch vehicle external fuel tank structural components, the current research work studies three different grades of Aluminium alloy reinforced with varying graphene weight percentages that are processed through powder metallurgy (P/M) route. The prepared green compacts composite ingots are subjected to microwave processing (Sintering), hot extruded, and solution treated (T6). The developed Nano-graphene reinforced composite is studied further for the strength–microstructural integrity. The nature of the graphene reinforcement and its chemical existence within the composite is further studied, and it is found that hot extruded solution treated (HEST) composite exhibited low levels of carbide (Al(4)C(3)) formations, as composites processed by microwaves. Further, the samples of different grades reinforced with varying graphene percentages are subjected to mechanical characterisation tests such as the tensile test and hardness. It is found that 2 wt% graphene reinforced composites exhibited enhanced yield strength and ultimate tensile strength. Microstructural studies and fracture morphology are studied, and it is proven that composite processed via the microwave method has exhibited good ductile behaviour and promising failure mechanisms at higher load levels. MDPI 2022-08-26 /pmc/articles/PMC9456592/ /pubmed/36079286 http://dx.doi.org/10.3390/ma15175907 Text en © 2022 by the authors. https://creativecommons.org/licenses/by/4.0/Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (https://creativecommons.org/licenses/by/4.0/).
spellingShingle Article
Jayaseelan, Joel
Pazhani, Ashwath
Michael, Anthony Xavior
Paulchamy, Jeyapandiarajan
Batako, Andre
Hosamane Guruswamy, Prashantha Kumar
Characterization Studies on Graphene-Aluminium Nano Composites for Aerospace Launch Vehicle External Fuel Tank Structural Application
title Characterization Studies on Graphene-Aluminium Nano Composites for Aerospace Launch Vehicle External Fuel Tank Structural Application
title_full Characterization Studies on Graphene-Aluminium Nano Composites for Aerospace Launch Vehicle External Fuel Tank Structural Application
title_fullStr Characterization Studies on Graphene-Aluminium Nano Composites for Aerospace Launch Vehicle External Fuel Tank Structural Application
title_full_unstemmed Characterization Studies on Graphene-Aluminium Nano Composites for Aerospace Launch Vehicle External Fuel Tank Structural Application
title_short Characterization Studies on Graphene-Aluminium Nano Composites for Aerospace Launch Vehicle External Fuel Tank Structural Application
title_sort characterization studies on graphene-aluminium nano composites for aerospace launch vehicle external fuel tank structural application
topic Article
url https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9456592/
https://www.ncbi.nlm.nih.gov/pubmed/36079286
http://dx.doi.org/10.3390/ma15175907
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