Review on Friction Stir Processed TIG and Friction Stir Welded Dissimilar Alloy Joints S
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Experimental Study of Mechanical Properties of 5083 Aluminium Alloy Using Gas Tungsten Arc Welding
ISSN(Online) : 2319-8753 ISSN (Print) : 2347-6710 International Journal of Innovative Research in Science, Engineering and Technology (An ISO 3297: 2007 Certified Organization) Vol. 5, Issue 5, May 2016 Experimental Study of Mechanical Properties of 5083 Aluminium Alloy Using Gas Tungsten Arc Welding M.Srivatsava 1 , Gopal Vanga 2, G. Narendra Santosh Kumar3 Assistant Professor, Dept. of Mechanical Engg., Guru Nanak Institutions Technical Campus, Hyderabad, India1 Associate Professor, Dept. of Mechanical Engg., Guru Nanak Institutions Technical Campus, Hyderabad, India 2 Assistant Professor, Dept. of Mechanical Engg., Guru Nanak Institutions Technical Campus, Hyderabad, India 3 ABSTRACT: The aluminium and its alloys are widely used in marine applications such as ship hulls and its components due to its light weight and corrosion resistance. The aluminium alloy require special tool and skill to weld due to high thermal conductivity Aluminum Alloy 5083 [AA 5083] considered as a one of the best weldable aluminum alloys and exhibits a slight reduction of the strength of the Heat Affected Zone [HAZ], comparatively to the most of other aluminum alloys. This alloy is commonly used in the manufacturing of pressure vessels, marine vessels, armored vehicles, aircraft cryogenics, drilling rigs, structures and even in missile components etc. Aluminium alloy 5083 contains Mg-Mn-Cr, in the tempered condition, it is strong and retaining good formability due to excellent ductility.5083 has high resistance to corrosion and used in marine applications. This report also investigates the weld quality through NDT and also study mechanical properties like UTS,0.2% YS and % of elongation and micro hardness using Gas Tungsten Arc welding (GTAW) with non-pulsed current and pulsed current at different process like 2Hz, 4Hz and 6Hz were studied and also to find the weld joint efficiency. -
Tensile Behavior of Aluminium Alloy 6063 - T6 in Sea Water
International Journal of Engineering Research and Development e-ISSN: 2278-067X, p-ISSN: 2278-800X, www.ijerd.com Volume 10, Issue 5 (May 2014), PP.68-74 Tensile Behavior of Aluminium Alloy 6063 - T6 In Sea Water P.John Maclins RVS Educational Trust’s Group of Institutions, Asst. Professor, Department of Aeronautical Engineering, Dindigul, Tamilnadu, India. Abstract:- Sea water, by virtue of its chloride content, is a most efficient electrolyte. The Omni-presence of oxygen in marine atmospheres, sea spray increases the aggressiveness of salt attack. The differential concentration of oxygen dissolved in a droplet of salt spray creates a cell in which attack is concentrated where the oxygen concentration is lowest. The sea environment is the most structurally hostile environment within which aircraft operate. The structural components are being exposed to salt spray continuously during its operation and it experiences heavy loading during landing. Corrosion also leads to crack propagation when subjected to loading. Corrosion along with damage leads to the failure of structural components prematurely and presents a serious problem in the aging aircraft. This requires a different approach to the maintenance of structural components subjected to corrosion and repetitive loads. This paper studies the effect of corrosion and low impact damage on aluminium alloy 6063- T6. The 6063 aluminium alloy that was used for the study was heat treated and soaked in seawater prepared per ASTM D1141 for different intervals of time between 0hours and 1000hours. Corroded specimens were subjected to low impact damage. The result shows a gradual degradation in mechanical properties of the alloy due to corrosion and damage. -
MATRIX Al-ALLOYS for SILICON CARBIDE REINFORCED METAL MATRIX COMPOSITES
IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 INFLUENCE OF VOLUME FRACTION, SIZE, CRACKING, CLUSTERING OF PARTICULATES AND POROSITY ON THE STRENGTH AND STIFFNESS OF 6063/SICP METAL MATRIX COMPOSITES A. Chennakesava Reddy1 1Professor, Department of Mechanical Engineering, JNTUH College of Engineering, Kukatpally, Hyderabad – 500 085, Telangana, India Abstract The objective of this study is to examine the influence of volume fraction, size of particulates, formation of precipitates at the matrix/particle interface, particle cracking, voids/porosity, and clustering of particulates on the strength and stiffness of 6063/SiCp metal matrix composites. Tensile strength and stiffness increase with an increase in the volume fraction of SiC particulates. The tensile strength and stiffness decrease with increase in size of the particulates, presence of porosity, clustering, and particle cracking. Formation of particulate clusters is more prominent in the composites having very small-reinforced particulates. Mg2Si compound is likely to precipitate at the matrix/particle interfaces of 6063/SiC composite. Keywords: 6063, SiC, clustering, cracking, porosity, clustering --------------------------------------------------------------------***------------------------------------------------------------------ 1. INTRODUCTION matrix composite have become of principal importance for the manufacturer to make a quality product as per the Consolidation of a high strength ceramic particulate in a soft designer specifications. The objective of this work is to metal matrix is the technological renovation in the domain study the influence of the volume fraction and particle size of composites for the designer to assure high specific elastic of SiCp, clustering and cracking of particulates, modulus, strength-to-weight ratio, fatigue durability, and voids/porosity, and formation of precipitates at the wear resistance in the fields of aerospace and automotive particle/matrix interface on the tensile strength and stiffness applications. -
Multi-Response Optimization of Process Parameters by Taguchi Grey Relational Analysis for Dissimilar Thickness Friction Stir Process Corner Weld Aa5086 Alloy
Journal of Engineering Science and Technology Vol. 13, No. 10 (2018) 3297 - 3312 © School of Engineering, Taylor’s University MULTI-RESPONSE OPTIMIZATION OF PROCESS PARAMETERS BY TAGUCHI GREY RELATIONAL ANALYSIS FOR DISSIMILAR THICKNESS FRICTION STIR PROCESS CORNER WELD AA5086 ALLOY MANIGANDAN KRISHNAN*, SENTHILKUMAR SUBRAMANIAM School of Mechanical Engineering, VIT University, Vellore, India *Corresponding Author: [email protected] Abstract This paper presents the multi-response optimization of friction stir corner welding process for dissimilar thickness AA5086 aluminium alloy plates. The corner joint of AA5086 aluminium alloy plates of thicknesses of 6 mm and 4 mm was welded by Friction Stir Welding (FSW) process. The FSW experiments were conducted agreeing to the L9 orthogonal array. Three FSW process parameters: tool traverse speed (100, 150 and 190 mm/min), rotational speed (900, 1000 and 1100 rev/min), and plunge depth (0.1, 0.2, and 0.3 mm) were related with weld tensile strength and hardness. The Analysis of Variance (ANOVA) was used to determine the percentage contribution of each input parameter on the weld quality. Taguchi Grey Relational Analysis is used to optimize and order the FSW process parameters. Conferring to the results of the analyses, the optimal welding condition was determined as 1000 rev/min for tool rotational speed, 150 mm/min for traverse speed and 0.1 mm for tool plunge depth. The percentage contribution of the traverse speed (54%) revealed a significant influence compared to tool rotational speed (21%) and plunge depth (13%). The microstructures of various zones were observed and analysed. Tensile tests were conducted and the fracture was observed at heat affected zones for all the joints. -
Aluminium Alloys Chemical Composition Pdf
Aluminium alloys chemical composition pdf Continue Alloy in which aluminum is the predominant lye frame of aluminum welded aluminium alloy, manufactured in 1990. Aluminum alloys (or aluminium alloys; see spelling differences) are alloys in which aluminium (Al) is the predominant metal. Typical alloy elements are copper, magnesium, manganese, silicon, tin and zinc. There are two main classifications, namely casting alloys and forged alloys, both further subdivided into heat-treatable and heat-free categories. Approximately 85% of aluminium is used for forged products, e.g. laminated plates, foils and extrusions. Aluminum cast alloys produce cost-effective products due to their low melting point, although they generally have lower tensile strength than forged alloys. The most important cast aluminium alloy system is Al–Si, where high silicon levels (4.0–13%) contributes to giving good casting features. Aluminum alloys are widely used in engineering structures and components where a low weight or corrosion resistance is required. [1] Alloys composed mostly of aluminium have been very important in aerospace production since the introduction of metal leather aircraft. Aluminum-magnesium alloys are both lighter than other aluminium alloys and much less flammable than other alloys containing a very high percentage of magnesium. [2] Aluminum alloy surfaces will develop a white layer, protective of aluminum oxide, if not protected by proper anodization and/or dyeing procedures. In a wet environment, galvanic corrosion can occur when an aluminum alloy is placed in electrical contact with other metals with a more positive corrosion potential than aluminum, and an electrolyte is present that allows the exchange of ions. -
DEVELOPMENT and CHARACTERIZATION of Al-3.7%Cu-1.4%Mg ALLOY/PERIWINKLE ASH (Turritella Communis) PARTICULATE COMPOSITES
DEVELOPMENT AND CHARACTERIZATION OF Al-3.7%Cu-1.4%Mg ALLOY/PERIWINKLE ASH (Turritella communis) PARTICULATE COMPOSITES BY MICHEAL NEBOLISA NWABUFOH THE DEPARTMENT OF METALLURGICAL AND MATERIALS ENGINEERING AHMADU BELLO UNIVERSITY, ZARIA JUNE, 2015. DEVELOPMENT AND CHARACTERIZATION OF Al-3.7%Cu-1.4%Mg ALLOY/PERIWINKLE ASH (Turritella communis) PARTICULATE COMPOSITES BY Michael Nebolisa NWABUFOH, B. Eng (Met), E.S.U.T M.Sc/Eng/01731/2010-2011 A THESIS SUBMITTED TO THE SCHOOL OF POSTGRADUATE STUDIES, AHMADU BELLO UNIVERSITY, ZARIA. IN PARTIAL FULFILLMENT OF THE REQUIREMENTS FOR THE AWARD OF A MASTER DEGREE IN METALLURGICAL AND MATERIALS ENGINEERING. DEPARTMENT OF METALLURGICAL AND MATERIALS ENGINEERING, FACULTY OF ENGINEERING AHMADU BELLO UNIVERSITY, ZARIA. NIGERIA. JUNE, 2015 ii Declaration I hereby declare that, this research work titled "Development and Characterization of Al-3.7%Cu-1.4%Mg Alloy/Periwinkle Shell (Turritella communis) Ash Particulate Composites" was carried out by me, and the results of this research were obtained by tests carried out in the laboratory and all quotations are indicated by references. Name of Student Signature Date iii Certification This research work titled "Development and Characterization of Al-3.7%Cu- 1.4%Mg/Periwinkle (Turritella communis) Shell Ash Particulate Composites" by Nwabufoh M. Nebolisa with Registration Number M.Sc/Eng/01731/2010-2011 meets the regulations guiding the Award of Master degree in Metallurgical and Materials Engineering at Ahmadu Bello University, Zaria. ____________________ ________________ Prof. S.B. Hassan Date Chairman, Supervisor committee ____________________ _______________ Prof. G.B. Nyior Date Member, Supervisor committee ____________________ _______________ Prof. S.A. Yaro Date Head of Department _____________________ ________________ Prof. -
Review on Thermal Analysis of Friction Stir Welding of Aluminium 5083 Alloy
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 12 | Dec 2018 www.irjet.net p-ISSN: 2395-0072 Review on Thermal Analysis of Friction Stir Welding of Aluminium 5083 Alloy M. Shiva Chander1, Dr. M. Rama Krishna2, Dr. B. Durgaprasad3 1Research Scholar, Department of Mechanical Engineering, JNTU Anantapur, Anantapuramu, A.P. 2Professor&Principal, Department of Mechanical Engineering, A M Reddy College of Engineering, Narsaraopeta, Guntur, A.P. 3Professor, Department of Mechanical Engineering, JNTU Anantapur, Anantapuramu, A.P. -------------------------------------------------------------------------***------------------------------------------------------------------------ Abstract - Friction Stir Welding (FSW), invented by Wayne Keywords: Friction stir welding, tool pin profile, FSW Thomas at TWI Ltd in 1991 overcomes many of the parameters, mechanical properties, microstructure analysis, problems associated with traditional joining techniques. 5083 Aluminium alloy, Tool geometry, SEM analysis, FSW is a solid-state process which produces welds of high temperature distribution, thermal analysis. quality in difficult-to-weld materials such as aluminium, and is fast becoming the process of choice for manufacturing I. INTRODUCTION lightweight transport structures such as boats, trains and Aluminum is the most prominent material to meet the aeroplanes. Aluminium alloys are lightweight materials challenges of future automotive regarding high strength to relatively used in automotive industries. In FSW, the welding weight ratio, corrosion resistance, emissions, safety and tool motion induces frictional heating and severe plastic sustainability. The welding of aluminum and its alloy is deformation and metal joining process is done in solid state difficult by fusion welding and resistance spot welding due results, which results in defect free welds with good to high thermal and electrical conductivity. -
ISSN: 2320-5407 Int. J. Adv. Res. 7(9), 779-794
ISSN: 2320-5407 Int. J. Adv. Res. 7(9), 779-794 Journal Homepage: - www.journalijar.com Article DOI: 10.21474/IJAR01/9728 DOI URL: http://dx.doi.org/10.21474/IJAR01/9728 RESEARCH ARTICLE TAFEL POLARIZATION AND IMPEDANCE STUDIES OF AL-7075 ALLOY AND ITS COMPOSITES IN DIFFERENT MEDIUM. Sravanthi.M1, Dr.K.G.Manjunatha2, Dr.Saifulla Khan3 and Sunitha N4 1. Assistant professor, Department of Chemistry,AMC Engineeing College, Banneerghatta Main Road, Bangalore,Karnataka-560083, India. 2. Prof. and HOD R&D Centre, Department of Engineering Chemistry, Ghousia College of Engineering, Ramanagaram, Bangalore, Karnataka-56215, India. 3. Assistant professor, Department of Chemistry, Ghousia college of Engineering, B.M Road, Ramanagaram – Bangalore, Karnataka-562159, India. 4. Assistant Professor, Department of Chemistry, City Engineering College, Kanakapura Road, Bangalore, Karnataka-560083, India. …………………………………………………………………………………………………….... Manuscript Info Abstract ……………………. ……………………………………………………………… Manuscript History Aluminum metal matrix composites because of their high potential in Received: 09 July 2019 satisfying the recent demands have a wide variety of applications in Final Accepted: 12 August 2019 aviation, defense system, and automobile industries. It has been noticed Published: September 2019 in research that the properties of composites can be enhanced by the addition of ceramic particles like SiC and graphite to metal matrix Key words:- Al7075, OCP, Tafel polarization, EIS composites. This paper attempts on corrosion studies of Al 7075 base and SEM. alloy/SiC/graphite based composites in different inorganic acid mediums (0.1M HCl,0.1M H2SO4 medium) and neutral chloride medium (3.5% NaCl medium) by making use of Tafel Polarization Technique and Electrochemical Impedance Spectroscopy Technique. Test samples were casted by taking the various percent of SiC/graphite by stir casting method as per ASTM standards. -
Conversion Coatings for Aluminium Alloys: a Surface Investigation for Corrosion Mechanisms
Conversion coatings for aluminium alloys: a surface investigation for corrosion mechanisms. by Rossana Grilli Submitted for the Degree of Doctor of Philosophy March 2010 The Surface Analysis Laboratory Surrey Materials Institute and Faculty of Engineering & Physical Sciences University of Surrey Guildford Surrey GU2 7XH UK Abstract Abstract Cr(VI) based conversion coatings are currently the treatments of choice for aluminium alloys to prevent corrosion, and are widely used in the aerospace industry also because of their good electrical conductivity and because they are good primers for paints and adhesives. Hexavalent chromium though is harmful for humans and for the environment, thus it needs to be replaced with more environmentally friendly materials. In this work three alternative pre-treatments for aluminium alloys were proposed and their properties were investigated and compared with the performance of a Cr(VI) based treatment. The selected “green” alternatives are based on titanium and zirconium compounds and they were applied to three different aluminium alloys relevant for spacecraft applications: Al2219, Al7075 and Al5083. After the characterization of the chosen materials by means of SEM, AES, XPS, EDX and SAM, some of their surface properties were explored: the adsorption of an epoxy acrylate resin used for UV-cured coatings, and the stability under UV and thermal exposure. The outcome of this preliminary investigation provided the basis for a further selection of materials to use in a corrosion study, and Al2219 was chosen as a substrate, together with an hybrid (organic/inorganic) coating, Nabutan STI/310. Alodine 1200S was proposed as chromate treatment and used as reference. A comparison of the behaviour during the exposure to a corrosive environment, as a NaCl solution, was made between the untreated Al2219 alloy, and the alloy treated with Nabutan STI/310 and Alodine 1200S. -
Characterisation of Tool Geometries for Friction Stir
COPYRIGHT AND CITATION CONSIDERATIONS FOR THIS THESIS/ DISSERTATION o Attribution — You must give appropriate credit, provide a link to the license, and indicate if changes were made. You may do so in any reasonable manner, but not in any way that suggests the licensor endorses you or your use. o NonCommercial — You may not use the material for commercial purposes. o ShareAlike — If you remix, transform, or build upon the material, you must distribute your contributions under the same license as the original. How to cite this thesis Surname, Initial(s). (2012) Title of the thesis or dissertation. PhD. (Chemistry)/ M.Sc. (Physics)/ M.A. (Philosophy)/M.Com. (Finance) etc. [Unpublished]: University of Johannesburg. Retrieved from: https://ujcontent.uj.ac.za/vital/access/manager/Index?site_name=Research%20Output (Accessed: Date). CHARACTERISATION OF TOOL GEOMETRIES FOR FRICTION STIR LAP WELDS OF ALUMINIUM AND COPPER TITLE PAGE By EWUOLA, OLUWATOYIN OLABISI A dissertation submitted to the FACULTY OF ENGINEERING AND THE BUILT ENVIRONMENT in fulfilment of the requirements for the degree of MASTERS OF PHILOSOPHY In MECHANICAL ENGINEERING At the UNIVERSITY OF JOHANNESBURG SUPERVISOR: PROF E. T. AKINLABI CO-SUPERVISOR: MR D. M. MADYIRA NOVEMBER 2015 DECLARATION I understand what plagiarism means. Where I have used the works of others, I have adequately referenced. I have not submitted this work for academic credit at any other institution. This research work is fully mine. _______________________ EWUOLA Oluwatoyin Olabisi 201338860 _______________________ _______________________ Prof AKINLABI Esther T. Mr MADYIRA Daniel M. Supervisor Co-supervisor ii | P a g e ABSTRACT The patenting of the Friction Stir Welding (FSW) process in 1991 opened up a process that was known within a relatively small circle of researchers to the entire research community. -
Comparison of Aluminum Alloys from Aircraft of Four Nations Involved in the WWII Conflict Using Multiscale Analyses and Archival Study
heritage Article Comparison of Aluminum Alloys from Aircraft of Four Nations Involved in the WWII Conflict Using Multiscale Analyses and Archival Study Toufa Ouissi 1,2,*, Gilles Collaveri 3, Philippe Sciau 1, Jean-Marc Olivier 2 and Magali Brunet 1,* 1 CEMES, UPR 8011 CNRS, 31055 Toulouse, France; [email protected] 2 FRAMESPA, UMR 5136, University of Toulouse Jean-Jaurès, 31058 Toulouse, France; [email protected] 3 Aerocherche, 31700 Blagnac, France; [email protected] * Correspondence: [email protected] (T.O.); [email protected] (M.B.) Received: 30 September 2019; Accepted: 14 November 2019; Published: 22 November 2019 Abstract: Aluminum alloys are very interesting witnesses of industrial and technical development. The first ever developed was Duralumin, a light metal with good mechanical properties. In the 1930s, the rise of nationalism stimulated research and development, generating various aluminum alloys. This work reports the comparison of two versions of aluminum alloys, which were found in collected parts of WWII crashed aircraft from four nations: a Messerschmitt Bf 109 (DE), a Dewoitine D.520 (FR), and a P-51 Mustang (USA) and an Avro Lancaster (United Kingdom). The first version of alloy with magnesium content below or equal to 1 wt.% and the second version with higher magnesium content (1.5 wt.%), were identified as respectively AlCuMg1, AlCuMg2 in Germany; Duralumin, Duralumin F.R. in France; Hiduminium DU Brand, Hiduminium 72 in the UK and 17S, 24S in the USA. This study uses a multiscale approach based on historical research complimented by laboratory analyses of materials directly collected on the crashed aircraft. -
Evaluation of Structural and Mechanical Properties of TIG Welded Aluminium Alloy AA-5083 Subjected to Post Cryogenic Treatment
Evaluation of Structural and Mechanical Properties of TIG Welded Aluminium Alloy AA-5083 Subjected to Post Cryogenic Treatment Sachin. L.S1, Mayur. S1*, Pavan. K.M1, Chandrashekar. A2 and B.S. Ajaykumar3 1Dept. of Mechanical Engg. Bangalore Institute of Technology, Bangalore - 560 004, India 2Asst. Professor, Dept. of Mechanical Engg. Bangalore Institute of Technology, Bangalore - 560 004, India 3Professor, Dept. of Mechanical Engg. Bangalore Institute of Technology, Bangalore - 560 004, India * correspondence author email: [email protected] Abstract - Cryogenic treatment is a low temperature achieved at -85°C. But when treated for a particular deep treatment process widely used in recent years to enhance the freeze time at -196oC there was a tremendous material properties without considerable sacrifice of other improvement in the above mentioned properties. “Cryo” properties at the same time. Cryogenic engineering is a means cold. Cryogeny means low temperature science[2]. branch of material handling process which has significant commercial applications. AA-5083 is very commonly used in The basic cryogenic treatment consists a gradual cooling the manufacture of welded pressure vessels, marine, auto of the specimen until the defined temperature, holding it aircraft cryogenics, transportation equipment such as for a given time (freezing time) and then progressively building of railroad cars, tip truck bodies, in missile leading it back to the room temperature[1]. Among the components. In this study, TIG welded Aluminium alloy AA- non-ferrous materials Aluminium and its alloys have 5083 plates were subjected to cryogenic treatment after been of interest in almost all the fields, due to their welding and their structural and mechanical properties were modest specific strength, ease of manufacture and low evaluated.