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Parshwamani Metals
+91-8048554624 Parshwamani Metals https://www.indiamart.com/parshwamanimetals/ Parshwamani Metals is one of the leading manufacturers, supplier and traders of Industrial Metal Tube, Beryllium Product, Shim Sheet, SS Round And Square Bar, Aluminium Products, Aluminum Bronze Products etc. About Us Parshwamani Metals was established in the year 2015 as a professionally managed Manufacturer, Trader and Wholesaler specialized in providing premium grade Copper and Brass Metals Products. Today, we endeavor to revolutionize the industry by fabricating a wide gamut of quality products, which includes Brass Products, Copper Products and Copper Alloy. Our claim to success is hallmarked by the offered quality products that gained us huge recognizance for its high strength, wear and tear resistance, accurate dimensions, flexibility and durable finish. Our products find their wide applications in architectural fittings, hardware and telecommunication. Owing to swift delivery schedules, easy payment modes and overt business practices, we have been successful in earning huge client base. We deal in Jindal Brand. Our efforts are determined with the objective of industrial leadership that equips our team members to manufacture customized products. And, to achieve this, we have developed modernized R&D centers and cutting edge manufacturing facilities. Furthermore, the facility is divided into various functional units like procurement, engineering, production, research & development, quality-testing, warehousing & packaging etc. Our organization is backed -
The Processing and Characterisation of Recycled Ndfeb Based Magnets
The Processing and Characterisation of Recycled NdFeB based Magnets By Salahadin Muhammed Ali Adrwish A thesis submitted to the University of Birmingham for the degree of Doctor of Philosphy Supervisors Prof. I.R. Harris Dr. A.J. Williams School of Metallurgy and materials University of Birmingham B15 2TT University of Birmingham Research Archive e-theses repository This unpublished thesis/dissertation is copyright of the author and/or third parties. The intellectual property rights of the author or third parties in respect of this work are as defined by The Copyright Designs and Patents Act 1988 or as modified by any successor legislation. Any use made of information contained in this thesis/dissertation must be in accordance with that legislation and must be properly acknowledged. Further distribution or reproduction in any format is prohibited without the permission of the copyright holder. CONTENTS Acknowledgement List of abbreviations Synopsis Chapter One 1.0 Aims of the Project 1 Chapter Two 2.0 Commercial use of NdFeB magnets 5 2.1 Development of NdFeB-type magnets 5 2. 2 Global NdFeB market 6 2.3 Major NdFeB producers 8 2.4 Applications 12 2.5 Factors affecting NdFeB supply and demand 14 2.5.1 IT sector 14 2.5.2 Global price of Dy and Nd 16 2.5.3 Environmental considerations 18 Chapter Three 3.0 Detailed aspects of NdFeB-type magnets recycling 22 3.1 Introduction 22 3.2 Introduction 22 3.3 Processing of recycled NdFeB over the years 25 3.3.1 Recycling of NdFeB magnets 26 3.3.2 Recycling of machine (internal) waste (sludge) 27 -
Planning for Seafood Freezing
TTTTTTTTTTT Planning for Seafood Freezing Edward KOLBE Donald KRAMER MAB-60 2007 Alaska Sea Grant College Program University of Alaska Fairbanks Fairbanks, Alaska 99775-5040 (888) 789-0090 Fax (907) 474-6285 www.alaskaseagrant.org TTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTT Elmer E. Rasmuson Library Cataloging-in-Publication Data: Kolbe, Edward. Planning for seafood freezing ⁄ Edward Kolbe and Donald Kramer. – Fairbanks, Alaska : Alaska Sea Grant College Program, University of Alaska Fairbanks, 2007 126 p. : 51 ill. ; cm. (Alaska Sea Grant College Program, University of Alaska Fairbanks ; MAB-60) Includes bibliographical references and index. 1. Frozen seafood—Preservation—Handbooks, manuals, etc. 2. Seafood— Preservation—Handbooks, manuals, etc. 3. Cold storage—Planning—Handbooks, manuals, etc. 4. Fishery management—Handbooks, manuals, etc. 5. Refrigeration and refrigeration machinery—Handbooks, manuals, etc. 6. Frozen fishery products—Handbooks, manuals, etc. I. Title. II. Kramer, Donald E. III. Series: Alaska Sea Grant College Program ; MAB-60. SH336.F7 K65 2007 ISBN 1-56612-119-1 Credits The work for this book was funded in part by the NOAA Office of Sea Grant, U.S. Department of Commerce, under grants NA76RG0476 (OSU), NA86RG0050 (UAF), and NA76RG0119 (UW); projects A/ESG-3 (OSU), A/151-01 (UAF), and A/FP-7 (UW), and by appropriations made by the Oregon, Alaska, and Washington state legislatures. Publishing is supported by grant NA06OAR4170013, project A/161-01. Sea Grant is a unique partnership with public and private sectors, combining research, education, and technology transfer for public service. This national network of universities meets the changing environmental and economic needs of people in our coastal, ocean, and Great Lakes regions. -
Aluminium Level 2 2019 CES Edupack
Level 2 Age-hardening wrought Al-alloys The 2000 and 7000 series age -hardening aluminum alloys are the backbone of the aerospace industry. The 6000 series has lower strength but is more easily extruded: it is used for marine and ground transport systems. THE MATERIAL The high -strength aluminum alloys rely on age -hardening: a sequence of heat treatment steps that causes the precipitation of a nano-scale dispersion of intermetallics that impede dislocation motion and impart strength. This can be as high as 700 MPa giving them a strength-to-weight ratio exceeding even that of the strongest steels. This record describes for the series of wrought Al alloys that rely on age-hardening requiring a solution heat treatment followed by quenching and ageing. This is recorded by adding TX to the series number, where X is a number between 0 and 8 that records the state of heat treatment. They are listed below using the IADS designations (see Technical notes for details).2000 series: Al with 2 to 6% Cu -- the oldest and most widely used aerospace series.6000 series: Al with up to 1.2% Mg and 1.3% Si -- medium strength extrusions and forgings.7000 series: Al with up to 8% Zn and 3% Mg -- the Hercules of aluminum alloys, used for high strength aircraft structures, forgings and sheet. Certain special alloys also contain silver. So this record, like that for the non-age hardening alloys, is broad, encompassing all of these. COMPOSITION 2000 series: Al + 2 to 6% Cu + Fe, Mn, Zn and sometimes Zr 6000 series: Al + up to 1.2%Mg + 0.25% Zn + Si, Fe a nd Mn 7000 series: Al + 4 to 9 % Zn + 1 to 3% Mg + Si, Fe, Cu and occasionally Zr and Ag GENERAL PROPERTIES Density 2500 - 2900 kg/m^3 Price *1. -
Ferrous Friction Stir Weld Physical Simulation A
FERROUS FRICTION STIR WELD PHYSICAL SIMULATION A Dissertation Presented in Partial Fulfillment of the Requirements for the Degree Doctor of Philosophy in the Graduate School of The Ohio State University By Seth Jason Norton, M.S. ******** The Ohio State University 2006 Dissertation Committee: Approved by Dr. John Lippold, Adviser Dr. David Dickinson Adviser Dr. Charles Albright Welding Engineering Graduate Program ii ABSTRACT Traditional fusion welding processes have several drawbacks associated with the melting and solidification of metal. Weld defects associated with the solidification of molten metal may act as initiation sites for cracks. Segregation of alloying elements during solidification may cause local changes in resistance to corrosion. The high amount of heat required to produce the molten metal in the weld can produce distortion from the intended position on cooling. The heat from the electric arc commonly used to melt metal in fusion welds may also produce metal fumes which are a potential health hazard. Friction stir welding is one application which has the potential to make full thickness welds in a single pass, while eliminating fume, reducing distortion, and eliminating solidification defects. Currently the friction stir welding process is used in the aerospace industry on aluminum alloys. Interest in the process by industries which rely on iron and its alloys for structural material is increasing. While friction stir welding has been shown to be feasible with iron alloys, the understanding of friction stir welding process effects on these materials is in its infancy. This project was aimed to better that understanding by developing a procedure for physical simulation of friction stir welding. -
Specifications of 2 Kelvin J-T Heat Exchanger
Specification of Brazed aluminium plate fin heat exchanger A. Scope of Supply (Qty-1 No.) Fabrication and supply of brazed aluminium plate fin heat exchanger as per parameters described in Table-1. B. Bidder Qualification Criteria 1. Original Manufacturer must have enough experience and knowledge of complete manufacturing cycle of brazed plate fin heat exchanger. He must have experience in supplying brazed plate fin heat exchanger. The supplier shall submit/upload supporting documents (scan copy of purchase order) for the same along with bid. 2. If the bidder is not the original manufacturer then he must submit the details of original manufacturer/fabricator. And quotation will be accepted only when the original manufacturer/fabricator qualify the above mentioned criteria. C. Design Details and Requirements 1. The manufacturer will prepare all the fabrication drawings according to the details mentioned in Table 1, with necessary flow distributor,headers and nozzles for passage of low pressure and high pressure stream. It is manufacturer’s responsibility to prepare final fabrication drawings of complete unit with all necessary details and get written approval from purchaser before commencing the fabrication. 2. The heat exchanger shall be made as per the standard tolerances given in ALPEMA code for the external dimensions of brazed Aluminium plate-fin heat exchangers. Table 1. Details of various parameters of plate fin heat exchanger Parameters Details Working Fluid (hot and cold side) Helium Heat Exchanger core Material ASTM 3003 Aluminium alloy Headers and Nozzle Material ASTM 5083/5454 Aluminium alloy Mass flow rate 6 g/s Operating pressure 6 bara maximum for hot side 16 mbara for cold side Fin type Offset Serrated Fin Fin density 14 fins/inch (551 fins/m) +0.2mm Fin height for hot side 3.8mm−0mm Fin height for cold side +0.2mm 6.5mm−0mm Fin Flow length Minimum 3mm and Maximum 5 mm Fin Thickness 0.2 mm Parting sheet thickness 0.8 mm Side bar thickness 8 mm No. -
Machining of Aluminum and Aluminum Alloys / 763
ASM Handbook, Volume 16: Machining Copyright © 1989 ASM International® ASM Handbook Committee, p 761-804 All rights reserved. DOI: 10.1361/asmhba0002184 www.asminternational.org MachJning of Aluminum and AlumJnum Alloys ALUMINUM ALLOYS can be ma- -r.. _ . lul Tools with small rake angles can normally chined rapidly and economically. Because be used with little danger of burring the part ," ,' ,,'7.,','_ ' , '~: £,~ " ~ ! f / "' " of their complex metallurgical structure, or of developing buildup on the cutting their machining characteristics are superior ,, A edges of tools. Alloys having silicon as the to those of pure aluminum. major alloying element require tools with The microconstituents present in alumi- larger rake angles, and they are more eco- num alloys have important effects on ma- nomically machined at lower speeds and chining characteristics. Nonabrasive con- feeds. stituents have a beneficial effect, and ,o IIR Wrought Alloys. Most wrought alumi- insoluble abrasive constituents exert a det- num alloys have excellent machining char- rimental effect on tool life and surface qual- acteristics; several are well suited to multi- ity. Constituents that are insoluble but soft B pie-operation machining. A thorough and nonabrasive are beneficial because they e,,{' , understanding of tool designs and machin- assist in chip breakage; such constituents s,~ ,.t ing practices is essential for full utilization are purposely added in formulating high- of the free-machining qualities of aluminum strength free-cutting alloys for processing in alloys. high-speed automatic bar and chucking ma- Strain-hardenable alloys (including chines. " ~ ~p /"~ commercially pure aluminum) contain no In general, the softer ailoys~and, to a alloying elements that would render them lesser extent, some of the harder al- c • o c hardenable by solution heat treatment and ,p loys--are likely to form a built-up edge on precipitation, but they can be strengthened the cutting lip of the tool. -
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. -
Aluminum Alloy Weldability: Identification of Weld Solidification Cracking Mechanisms Through Novel Experimental Technique and Model Development
Dipl.-Ing. Nicolas Coniglio Aluminum Alloy Weldability: Identifi cation of Weld Solidifi cation Cracking Mechanisms through Novel Experimental Technique and Model Development BAM-Dissertationsreihe • Band 40 Berlin 2008 Die vorliegende Arbeit entstand an der BAM Bundesanstalt für Materialforschung und -prüfung. Impressum Aluminum Alloy Weldability: Identifi cation of Weld Solidifi cation Cracking Mechanisms through Novel Experimental Technique and Model Development 2008 Herausgeber: BAM Bundesanstalt für Materialforschung und -prüfung Unter den Eichen 87 12205 Berlin Telefon: +49 30 8104-0 Telefax: +49 30 8112029 E-Mail: [email protected] Internet: www.bam.de Copyright © 2008 by BAM Bundesanstalt für Materialforschung und -prüfung Layout: BAM-Arbeitsgruppe Z.64 ISSN 1613-4249 ISBN 978-3-9812354-3-2 Aluminum Alloy Weldability: Identification of Weld Solidification Cracking Mechanisms through Novel Experimental Technique and Model Development Dissertation zur Erlangung des akademischen Grades Doktor-Ingenieur (Dr.-Ing.) genehmigt durch die Fakultät für Maschinenbau der Otto-von-Guericke-Universität Madgeburg am 02.06.08 vorgelegte Dissertation von Dipl.-Ing. Nicolas Coniglio Thesis Committee: Prof. Dr.-Ing. A. Bertram Prof. Dr.-Ing. T. Böllinghaus Prof. C.E. Cross Prof. S. Marya Date of Examination: 23 October 2008 Abstract Abstract The objective of the present thesis is to make advancements in understanding solidification crack formation in aluminum welds, by investigating in particular the aluminum 6060/4043 system. Alloy 6060 is typical of a family of Al-Mg-Si extrusion alloys, which are considered weldable only when using an appropriate filler alloy such as 4043 (Al-5Si). The effect of 4043 filler dilution (i.e. weld metal silicon content) on cracking sensitivity and solidification path of Alloy 6060 welds are investigated. -
Mechanical Milling of Co-Rich Melt-Spun Sm-Co Alloys
University of Nebraska - Lincoln DigitalCommons@University of Nebraska - Lincoln Mechanical & Materials Engineering, Engineering Mechanics Dissertations & Theses Department of Spring 5-2010 MECHANICAL MILLING OF CO-RICH MELT-SPUN SM-CO ALLOYS Farhad Reza Golkar-Fard University of Nebraska - Lincoln, [email protected] Follow this and additional works at: https://digitalcommons.unl.edu/engmechdiss Part of the Engineering Mechanics Commons, and the Mechanical Engineering Commons Golkar-Fard, Farhad Reza, "MECHANICAL MILLING OF CO-RICH MELT-SPUN SM-CO ALLOYS" (2010). Engineering Mechanics Dissertations & Theses. 6. https://digitalcommons.unl.edu/engmechdiss/6 This Article is brought to you for free and open access by the Mechanical & Materials Engineering, Department of at DigitalCommons@University of Nebraska - Lincoln. It has been accepted for inclusion in Engineering Mechanics Dissertations & Theses by an authorized administrator of DigitalCommons@University of Nebraska - Lincoln. MECHANICAL MILLING OF CO-RICH MELT-SPUN SM-CO ALLOYS by FARHAD REZA GOLKAR-FARD A THESIS Presented to the Faculty of The Graduate College at the University of Nebraska In Partial Fulfillment of Requirements For the Degree of Master Science Major: Engineering Mechanics Under the Supervision of Professor Jeffrey E. Shield Lincoln, Nebraska May, 2010 MECHANICAL MILLING OF CO-RICH MELT-SPUN SM-CO ALLOYS Farhad Reza Golkar-Fard, M.S UNIVERSITY OF NEBRASKA, 2010 Advisor: Jeffrey E. Shield Rare-earth, high-energy permanent magnets are currently the best performing permanent magnets used today. The discovery of single domain magnetism in 1950’s ultimately led to the development of nanocomposite magnets which had superior magnetic properties. Previous work has shown that mechanical milling (MM) effectively generates nanoscale structures in Sm-Co-based alloys. -
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. -
Microstructure and Mechanical Properties of the Annealed 6060 Aluminium Alloy Processed by ECAP Method
Volume 80 International Scientific Journal Issue 1 published monthly by the July 2016 World Academy of Materials Pages 31-36 and Manufacturing Engineering Microstructure and mechanical properties of the annealed 6060 aluminium alloy processed by ECAP method M. Karoń *, A. Kopyść, M. Adamiak, J. Konieczny Faculty of Mechanical Engineering, Silesian University of Technology, ul. Konarskiego 18a, 44-100 Gliwice, Poland * Corresponding e-mail address: [email protected] ABSTRACT Purpose: The main goal of this paper is to present the investigation results of microstructural evolution and mechanical properties changes in commercial EN AW 6060) aluminium alloy after intensive plastic deformation, obtained by equal channel angular pressing (ECAP) techniques in an annealed state. Design/methodology/approach: Annealing heat treatment was used to remove various types of internal stress in a commercially available alloy in order to increase workability of the material. The evolution of its properties and material behaviour was evaluated after 2,4,6,and 8 passes of the ECAP process. Findings: It was found that the mechanical properties and microstructure during intensive plastic deformation, such as that during the ECAP process, were changed. Plastic deformation refined grains in the aluminium alloy and increased its mechanical properties. Research limitations/implications: The presented study shows results of the investigated material in an annealed state. Practical implications: The applied processing route allows development of materials characterized by high strength and ultrafine grain microstructure compared to un-deformed annealed aluminium alloy. Originality/value: The work presents data about the influence of intensive plastic deformation on the microstructure and mechanical properties of 6060 aluminium alloy after annealing.