Icaciem2017057 by ASDF Administartor

International Conference on Advances & Challenges in Interdisciplinary Engineering and Management

International Conference on Advances & Challenges in Interdisciplinary Engineering and Management 2017 [ICACIEM 2017]

ISBN Website Received Article ID

978-81-933235-1-9 icaciem.org 10 – January – 2017 ICACIEM057

VOL eMail Accepted eAID

01 icaciem@asdf.res.in 28 - January – 2017 ICACIEM.2017.057

Microstructure and Mechanical Properties of Aluminium Alloy 6061 Reinforced Glass 1,2,3,4,5

E Poovarasan1, M Ramesh2, S Ranjith3, G Santhoshkumar4, S Sarathkumar5 U.G Scholars, Dept. of Mechanical Engineering, Vidyaa Vikas College of Engineering and Technology, Tiruchengode, India

Abstract: Aluminium matrix composites (AMCs) refer to the category of luminosity heaviness elevated routine aluminium centric material systems. The reinforcement in AMCs might be in the appearance of incessant/irregular fibres, whisker or particulates, in volume fractions. Properties of AMCs be able to be tailored to the demands of different industrial applications by appropriate addition of matrix, reinforcement and processing route. This work focuses on the fabrication of aluminium alloy (6061) matrix composites (AMCs) reinforced with 5 to 14 wt% glass particulates of 70µm, 80µm, 100µm and 240µm using stir casting route. The microstructure and mechanical properties of the fabricate AMCs were analysed. The mechanical properties like rigidity and tensile strength of the unreinforced alloy and composites had been calculated. The mechanical properties like hardness and tensile strength had improved with the enlarge in weight percentage of glass particulates in the aluminium matrix.

ISBN Website Received Article ID

978-81-933235-1-9 icaciem.org 10 – January – 2017 ICACIEM058

VOL eMail Accepted eAID

01 icaciem@asdf.res.in 28 - January – 2017 ICACIEM.2017.058

Analysis of Carbon-Epoxy Composite in Aircraft Application 1

D Suman kotekar1 Assistant Professors, Dept. of Mechanical Engineering, Vidyaa Vikas College of Engineering and Technology, Tiruchengode, India

Abstract: The aerospace industry is one of the major fast growing fields and has a major contribution toward the development of a country by contributing to trade, freight and defence. The major concerns in this field are regarding the weight of the aircraft, performance and capacity. Regarding the weight of the aircraft, it has a major role in the functioning and performance of an aircraft. Starting from wood, metal, etc. there has been a continuous development in parts of an aircraft. Recent trend is that the metal has been replaced by composite materials, which are lighter in weight and have more strength and increased performance than their counterparts. Regarding the composites the have two major parts namely fibre and matrix. The proportion of this two has a major influence on the properties of the composite. The carbon epoxy composites are being used in major parts of an aircraft and their porosity level makes a major contribution to their performance. This composite is manufactured by variety of methods majorly by autoclave method. These composites are tested for their optimum porosity level as high porosity leads to the decrease in the strength of the part and hence leads to failure, which may cause damage at a large extent. Hence this project will be helpful to identify the optimum porosity level at which the part shows high strength and performance for the ideal functioning of the part. This paper is prepared exclusively for International Conference on Advances & Challenges in Interdisciplinary Engineering and Management 2017 [ICACIEM 2017] which is published by ASDF International, Registered in London, United Kingdom under the directions of the Editor-in-Chief Dr K Samidurai and Editors Dr. Daniel James, Dr. Kokula Krishna Hari Kunasekaran and Dr. Saikishore Elangovan. Permission to make digital or hard copies of part or all of this work for personal or classroom use is granted without fee provided that copies are not made or distributed for profit or commercial advantage, and that copies bear this notice and the full citation on the first page. Copyrights for third-party components of this work must be honoured. For all other uses, contact the owner/author(s). Copyright Holder can be reached at copy@asdf.international for distribution.