2 Manufacturing of Aluminium Composite Materials: a Review
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On Mechanical Properties of Aluminum Alloys
Technical Journal, University of Engineering and Technology (UET) Taxila, Pakistan Vol. 25 No. 1-2020 ISSN:1813-1786 (Print) 2313-7770 (Online) The Effect of Filler Materials (Al 4047 and Al 5356) on Mechanical Properties of Aluminum Alloys (AA6061-O and Heat-Treated AA7075-T6) in Tungsten Inert Gas (TIG) Dissimilar Metal Welding A.Batool1, N.A.Anjum2, H.Jawaid3 1,2,3Department of Mechanical Engineering, University of Engineering & Technology, Taxila, Pakistan 2 [email protected] Abstract- The purpose of the current work is to any other Alloy. investigate the combined effect of thickness and the As compared to other alloys of aluminum, the 6061 mechanical properties of dissimilar aluminum alloys series Al-alloys have been examined broadly due to annealed AA6061-O and heat-treated AA7075-T6 on their attributes like medium strength, better weld- the tensile strength of the joint. The joint is made by ability, formability, good corrosion resistance and Tungsten Inert Gas (TIG) welding using suitable fillers reduced cost of Aluminum alloy 6061 is one of the most Al 4047 and Al 5356. Different samples i.e. Welded utilized of the 6000 series aluminum alloys [2]. It is a Over-Nugget Sample (WOS), Welded Ground Sample versatile heat treatable alloy with intermediate to (WGS) and Base Material (BM) were investigated advanced strength capabilities [3]. The 6061 under tensile loading. In order to avoid failure, the Aluminum alloys are extensively used in the thickness of weak strength AA6061-O must be greater fabrication of several Aircraft and aerospace as compared to the thickness of AA7075 comprising components, transport and bicycle frames, marine high strength in order to balance stresses on both sides. -
The Study of Hems Based on the Mechanically Activated Intermetallic Al12mg17 Powder
molecules Article The Study of HEMs Based on the Mechanically Activated Intermetallic Al12Mg17 Powder Sergei Sokolov * , Alexander Vorozhtsov, Vladimir Arkhipov and Ilya Zhukov Laboratory of Metallurgy Nanotechnologies, National Research Tomsk State University, Lenin Avenue, 36, 634050 Tomsk, Russia; [email protected] (A.V.); [email protected] (V.A.); [email protected] (I.Z.) * Correspondence: [email protected]; Tel.: +7-923-406-77-01 Academic Editor: Svatopluk Zeman Received: 30 May 2020; Accepted: 19 July 2020; Published: 5 August 2020 Abstract: In this work, Al–Mg intermetallic powders were characterized and obtained by melting, casting into a steel chill and subsequent mechanical activation in a planetary mill. The method for producing Al12Mg17 intermetallic powder is presented. The dispersity, morphology, chemical composition, and phase composition of the obtained powder materials were investigated. Certain thermodynamic properties of high-energy materials containing the Al-Mg powder after mechanical activation of various durations were investigated. The addition of the Al-Mg powders to the high-energy composition (synthetic rubber SKDM-80 + ammonium perchlorate AP + boron B) can significantly increase the burning rate by approximately 47% and the combustion heat by approximately 23% compared with the high-energy compositions without the Al-Mg powder. The addition of the Al12Mg17 powder obtained after 6 h of mechanical activation provides an increase in the burning rate by 8% (2.5 0.1 mm/s for the mechanically activated Al Mg powder and ± 12 17 2.3 0.1 mm/s for the commercially available powder) and an increase in the combustion heat by 3% ± (7.4 0.2 MJ/kg for the mechanically activated Al-Mg powder and 7.1 0.2 MJ/kg for the commercially ± ± available powder). -
A Study of Process Parameters of Friction Stir Welded Aa 6061 Aluminum Alloy
ISSN: 2319-8753 International Journal of Innovative Research in Science, Engineering and Technology Vol. 2, Issue 6, June 2013 A STUDY OF PROCESS PARAMETERS OF FRICTION STIR WELDED AA 6061 ALUMINUM ALLOY Prashant Prakash1, Sanjay Kumar Jha2, Shree Prakash Lal3 Department of Production Engineering, B.I.T Mesra , Patna Campus, India 1 ,3 Department of Production Engineering, B.I.T Mesra , Ranchi , India 2 Abstract: Friction stir welding (FSW) is a relatively new solid-state joining process. This joining technique is energy efficient, environment friendly, and versatile. The principal advantages are low distortion, absence of melt related defects and high joint strength. In FSW parameters play an important role like tool design and material, tool rotational speed, welding speed and axial force. The paper focuses on process parameters that in required for producing effective friction stir welding joint. Keywords: Friction Stir welding, 6061 aluminum alloy, tool rotational speed, welding speed, tensile strength. I. INTRODUCTION Aluminium alloys with a wide range of properties. Among all aluminum alloys, AA 6061 alloy plays major role in the aerospace industry in which magnesium and silicon (0.3-1.5 w%, Si, Mg) are the principal alloying elements [9]. It is widely used in the aerospace applications because it has good formability, weldability, machinabilty, corrosion resistance, and good strength compared to other aluminum alloys. Aluminum alloys are generally classified as non-weldable because of the poor solidification microstructure and porosity in the fusion zone. Also, the loss in mechanical properties as compared to the base material is very significant. These factors make the joining of these alloys by conventional welding processes unattractive. -
Alcotec Aluminum Technical Guide
AlcoTec Aluminum Technical Guide Contents AlcoTec Aluminum Wire & Equipment Technical Guide Table of Contents AlcoTec Aluminum Wire & Equipment Technical Guide ......................................................................................................... 1 Table of Contents ................................................................................................................................................................ 1 Environmental Health and Safety ......................................................................................................................................... 3 Technical Services Heat Treatable & Non-Heat Treatable Base & Fillers ............................................................................................................. 6 Filler Alloys: Chemical Composition Limits & Physical Properties ......................................................................................... 7 Conversion Factors ............................................................................................................................................................ 7 Welded Joint Strength ......................................................................................................................................................... 8 Typical Tensile Properties - Groove Welds ............................................................................................................................ 9 Weld Profiles ..................................................................................................................................................................... -
Studies on Properties of Al–Sic Metal Matrix Composite Material for Making IC Engine Valves
Proceedings of the World Congress on Engineering 2018 Vol II WCE 2018, July 4-6, 2018, London, U.K. Studies on Properties of Al–SiC Metal Matrix Composite Material for Making IC Engine Valves Nilamkumar S. Patel, Ashwin D. Patel, Ritesh Kumar Ranjan, Vikas Rai Abstract-Automobile industries are using material substitution the matrix also helps to transfer load among the composite for to build lighter weight, and fuel efficient engines, offering is compound material which differs from alloy due to fact better properties materials of engine components, including that all the individual component retain its characteristic. engine poppet valves and valve seats. Valves and valve seats are very important components that are used at high operating II. EXPERIMENTAL SET-UP temperature to control the flow and volumetric efficient at desired level of engine performance. The present work Stir casting process is liquid state processing. It is simple describes that Al-SiC composite as possible alternate materials and flexible process. In this process, there is mixing of with its unique capacity to give required properties for engine matrix and reinforcement. poppet valves and valve seats. Al-SiC MMC is prepared by In this process, reinforcement particles are added into the powder metallurgy and various casting techniques. In the research a composite is developed by stir casting process by molten matrix metal. And then the proper mixture is done using aluminium alloy with silicon carbide Nano particles and by hand stirring as well as Mechanical stirring. And then substitute sintering operation at 600oC temperature for one this mixture is allowed to pour into the mould shape. -
A Review on Comparison of Aluminium Alloy LM-25 with Al/Sic
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 01 | Jan-2018 www.irjet.net p-ISSN: 2395-0072 A review on comparison of Aluminium alloy LM-25 with Al/Sic Rahul Ushir1 , Kunal Gandhi2, Gaurav Dahe3, Vijay Bidgar4, Prof. Vishal Thakre5. 1,2,3,4 BE student Mechanical, SND COE & RC, YEOLA, Maharashtra, India 5Prof. Mechanical, SND COE & RC, YEOLA, Maharashtra, India ---------------------------------------------------------------------***--------------------------------------------------------------------- Abstract- Many industries suffered a great loss of materials and procedures to decrease the wear of devices manufacturing process due to collapse of manufacturing and designing segments. These incorporate change of mass machines due to wear and fail of lubrication. Friction is main properties of the materials, surface medications and cause of wear and energy dissipation. Improving friction can utilization of covering, and so on. In the course of the most make substantial saving. It is obvious that enormous amount recent couple of years, numerous endeavors have been made of the worlds resources are used to overcome friction in the to comprehend the wear conduct of the surfaces in sliding form or another. Lubrication is an effective means of contact and the instrument, which prompts wear. The controlling wear and reducing friction. Hence, for the survival applications of aluminium and its alloys for the machine of machine wear and friction must be decreased parts are increasing day to day in the industry. However, and/controlled carefully. little has been reported on the wear behaviour of aluminium and its alloys with the addition of grain refiner and modifier. Key words: Silicon Carbide(Sic) , aluminium LM25,scanning electron microscope ( SEM ) , metal PROBLEM DEFINITION: matrix composite ( MMCs) . -
Maec.19 70 (University of London) London
COMPLEX & INCREMENTAL STRESS CREEP OF A HIGH STRENGTH ALUMINIUM ALLOY AT ELEVATED TEMPERATURES (ALLOY: HIDUMINIUM RR58 SPECIFICATION DTD 731) by SURINDAR BAHADUR MATHUR Thesis presented in the Department of Mechanical Engineering for the Award of the Doctor of Philosphy in Mechanical Engineering of the University of London. Mechanical Engineering Department Imperial College of Science and Technology mAec.19 70 (University of London) London. ABSTRACT A theory for creep rates under complex and incremental stresses is deduced from experimental data concerning complex creep at elevated temperatures for the test material HIDUMINIUM RR 58 - Specification DID 731. The most important results are for tubular specimens tested at 150°C and 250°C under incremental loads. The analysis of results relates to steady state creep only. Modified relationships in stress equivalence and strain equivalence are proposed to account for thermal softening, polygonization, recrystallization and the resulting exaggerated flow in the direction of the applied shear. (The original equations are based on the hypothesis of Von Mises). A further relationship is suggested between the immediate total energy of distortion and the subsequent creep work rate. Results of the static tests and the results of the tests for creep behaviour under complex loading are presented and compared with the results of static torsion and simple incremental torsion creep tests on the basis of the proposed equations. An appendix describes the complex creep testing machine, furnace, extensometers -
The Effect of Cooling Rate on the Microstructure of A356 Aluminium Alloy
SVOA MATERIALS SCIENCE & TECHNOLOGY (ISSN: 2634-5331) Research https://sciencevolks.com/materials-science/ Volume 2 Issue 4 The Effect of Cooling Rate on the Microstructure of A356 Aluminium Alloy Maftah H. Alkathafi1*, Abdalfattah A. Khalil2, Ayad O. Abdalla3 Affiliations: 1Mechanical Engineering Department, Faculty of Engineering, Sirte University, Libya 2Materials Science Department, Faculty of Engineering, Omer Al-Mukhtar University, Libya. 3College of Mechanical Engineering Technology, Benghazi-Libya. *Corresponding author: Maftah H. Alkathafi* Mechanical Engineering Department, Faculty of Engineering, Sirte University, Libya Received: December 10, 2020 Published: December 31, 2020 Abstract: In this study a fast-cooling technology is employed for a cast iron mould to prepare cast A356 aluminium alloy by solidifica- tion of the molten metal. The cooling rate is achieved by pouring the molten alloy into a preheating permanent mould at different temperatures (25, 100, 200, 300 and 4000C) for cast samples with 40 mm inside diameter and 200 mm height. The samples considered are analyzed by optical microscopy, scanning electron microscopy (SEM), and EDS X-ray analysis (EDS). The effects of cooling rate on the morphology of α – aluminum and eutectic silicon of A356 alloy have been studied. The results showed that the dendritic structure of α-phase was broken and converted into a somewhat globular grain structure and the coarse acicular eutectic silicon trend to be broken and converted into short sticks or small rounded in other cases. Keywords: A356 Aluminum alloy, Grain refinement, Cooling rate, SEM, EDS, Microstructure. 1. Introduction Aluminium alloys have attractive physical and mechanical properties. They are lightweight, low costs production, easy to machine and have good recycling possibilities up to 95 % [1]. -
Aluminium Alloy - 6262 - T6 Extrusions
Aluminium Alloy - 6262 - T6 Extrusions SPECIFICATIONS CHEMICAL COMPOSITION Commercial 6262 BS EN 573-3:2009 Alloy 6262 EN 6262 Element % Present Magnesium (Mg) 0.80 - 1.20 Aluminium alloy 6262 is a heat treatable alloy with Copper (Cu) 0.15 - 1.40 very good corrosion resistance and strength. Additions of bismuth to the alloy mean that 6262 has excellent Silicon (Si) 0.40 - 0.80 machinability and surface finish. Lead (Pb) 0.40 - 0.70 High-speed steel or carbide tooling can be used to obtain smooth finishes. Heavy cutting requires oil Bismuth (Bi) 0.40 - 0.70 lubricant but light cutting can be done dry. Iron (Fe) 0.0 - 0.70 Alloy 6262 can be used in place of 2011 when higher corrosion resistance and better anodising response is Zinc (Zn) 0.0 - 0.25 required. Chromium (Cr) 0.04 - 0.14 Applications Titanium (Ti) 0.0 - 0.15 6262 is commonly used in the manufacture of: Manganese (Mn) 0.0 - 0.15 Screw machine products Camera parts Others (Total) 0.0 - 0.15 Nuts Other (Each) 0.0 - 0.05 Couplings Aluminium (Al) Balance Marine fittings Decorative hardware and appliance fittings Hinge pins Oil line fittings ALLOY DESIGNATIONS Valves and valve parts Aluminium alloy 6262 also corresponds to the following standard designations and specifications but may not PLEASE NOTE: Due to European Environmental be a direct equivalent: Protection Directives: AA6262 # 2000/53/CE-ELV – For the automotive sector Al 1.0Mg 0.6Si Pb # 2002/95/CE-RoHS – For the electrical and A96262 electronics sector This alloy has been replaced by Alloy 6026 which has a PLEASE NOTE: Due to European Environmental lower Lead content. -
Annual Report of the Director of the Mint
- S. Luriºus vsº ANNUAL REPORT Of the Director of the N/int for the fiscal year ended June 30, 1970. ANNUAL REPORT of the Director of the Mint for the fiscal year ended June 30 1970 DEPARTMENT OF THE TREASURY DOCUMENT NO. 3253 Director of the Mint U.S. GOVERNMENT PRINTING OFFICE WASHINGTON : 1971 For sale by the Superintendent of Documents, U.S. Government Printing Office Washington, D.C. 20402 - Price $1 (paper cover) Stock Number 4805–0009 LETTER OF TRANSMITTAL DEPARTMENT OF THE TREASURY, BUREAU OF THE MINT, Washington, D.C., April 29, 1971. SIR: I have the honor to submit the Ninety-eighth Annual Report of the Director of the Mint, since the Mint became a Bureau within the Department of the Treasury in 1873. Annual reports of Mint activities have been made to the Secretary of the Treasury since 1835, pursuant to the act of March 3, 1835 (4 Stat. 774). Annual reports of the Mint have been made since it was established in 1792. This report is submitted in compliance with Section 345 of the Revised Statutes of the United States, 2d Edition (1878), 31 U.S.C. 253. It includes a review of the operations of the mints, assay offices, and the bullion depositories for the fiscal year ended June 30, 1970. Also contained in this edition are reports for the calendar year 1969 on U.S. gold, silver, and coinage metal production and the world's monetary stocks of gold, silver, and coins. MARY BROOKs, Director of the Mint. Hon. JoHN B. Con NALLY, Secretary of the Treasury. -
Effect of Volume Fraction (Al2o3) on Tensile Strength of Aluminium 6061 by Varying Stir Casting Furnace Parameters: a Review
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 10 | Oct -2017 www.irjet.net p-ISSN: 2395-0072 Effect of volume fraction (Al2O3) on tensile strength of Aluminium 6061 by varying stir casting furnace parameters: A Review Yogesh Prabhavalkar1, Prof.Dr.A.N.Chapgaon 2 1M.E. Student, Ashokrao Mane Group of Institution Vathar-416112, Maharashtra, India 2Professor, Department of Mechanical Engineering, Ashokrao Mane Group of Institution Vathar-416112, Maharashtra, India ---------------------------------------------------------------------***------------------------------------------------------------------- Abstract - Aluminium metal matrix composites (AMMCs) are potential materials for various applications due to their good physical and mechanical properties. The addition of reinforcements into it improves the stiffness, specific strength, wear, creep and fatigue properties compared to the conventional engineering materials and It was revealed that aluminium with reinforcement of Al2O3 composites have a higher tensile strength than 6061 aluminium alloy with reduced ductility. Fabrication of this metal matrix is done by stir casting technique which is one of the prominent and economical techniques for development and processing of the same. It has been found that with the increase in weight percentage of reinforcement particles in the aluminium metal matrix, the new material exhibits lower wear rate against abrasive wearing. This article is just an assessment of effect of reinforcement (Al2O3)on AMC’s mechanical properties with various process parameters of stir casting process, such as stirrer design and it’s speed, stirring temperature, stirring time (holding time) and concentration of Al2O3 . Keywords - Aluminum metal matrix composites, Stir casting process, 6061 Aluminium alloy; Al2O3 composites; Tensile strength. 1. INTRODUCTION: Metal matrix composites are metals reinforced with other metal, ceramic or organic compounds. -
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.