Structural Life Enhancement on Friction Stir Welded AA6061 with Optimized Process and HFMI/PIT Parameters

Total Page:16

File Type:pdf, Size:1020Kb

Structural Life Enhancement on Friction Stir Welded AA6061 with Optimized Process and HFMI/PIT Parameters See discussions, stats, and author profiles for this publication at: https://www.researchgate.net/publication/309960723 Structural life enhancement on friction stir welded AA6061 with optimized process and HFMI/PIT parameters Article in The International Journal of Advanced Manufacturing Technology · June 2017 DOI: 10.1007/s00170-016-9697-7 CITATIONS READS 4 43 3 authors, including: Yupiter HP Manurung Mohamed Ackiel Universiti Teknologi MARA Serba Dinamik Group Berhad 78 PUBLICATIONS 453 CITATIONS 16 PUBLICATIONS 66 CITATIONS SEE PROFILE SEE PROFILE Some of the authors of this publication are also working on these related projects: Spot weld View project All content following this page was uploaded by Mohamed Ackiel on 22 June 2018. The user has requested enhancement of the downloaded file. Structural life enhancement on friction stir welded AA6061 with optimized process and HFMI/PIT parameters Yupiter H. P. Manurung, Mohamed Ackiel Mohamed & Azrriq Zainul Abidin The International Journal of Advanced Manufacturing Technology ISSN 0268-3768 Int J Adv Manuf Technol DOI 10.1007/s00170-016-9697-7 1 23 Your article is protected by copyright and all rights are held exclusively by Springer- Verlag London. This e-offprint is for personal use only and shall not be self-archived in electronic repositories. If you wish to self-archive your article, please use the accepted manuscript version for posting on your own website. You may further deposit the accepted manuscript version in any repository, provided it is only made publicly available 12 months after official publication or later and provided acknowledgement is given to the original source of publication and a link is inserted to the published article on Springer's website. The link must be accompanied by the following text: "The final publication is available at link.springer.com”. 1 23 Author's personal copy Int J Adv Manuf Technol DOI 10.1007/s00170-016-9697-7 ORIGINAL ARTICLE Structural life enhancement on friction stir welded AA6061 with optimized process and HFMI/PIT parameters Yupiter H. P. Manurung1 & Mohamed Ackiel Mohamed2 & Azrriq Zainul Abidin3 Received: 5 September 2016 /Accepted: 3 November 2016 # Springer-Verlag London 2016 Abstract This novel study presents an unconventional ap- 65, 25 and 10% for air pressure, impact frequency and indent- proach to find the best governing process parameters of high er diameter, respectively. Secondly, using subsequent post- frequency mechanical impact technique based on multi- weld mechanical treatment, the life cycle number can be ex- objective optimization method. In this investigation, the tended up to 12 times on friction-stirred weld. Finally, based post-weld mechanical treatment is aimed to enhance fatigue on the experimental confirmation test, the proposed method resistance of structural friction-stirred weld subjected to fluc- can effectively estimate the structural life and surface hardness tuating loads by obtaining nominal sub-surface hardness. The within the acceptable range of relative error. experimental study was conducted on aluminium alloy AA 6061 with thickness of 6 mm under varied parameters centred Keywords Fatigue life . Friction stir welding (FSW) . High on indenter diameter, air pressure and impact frequency. The frequency mechanical impact (HFMI) . Pneumatic impact investigation began with obtaining optimum parameters for treatment (PIT) . Optimization single response by using conventional Taguchi method with L9 orthogonal array. Next, advanced optimization approach by means of multi-objective Taguchi method attempts to con- 1 Introduction sider the multiple responses simultaneously which are sub- surface hardness and structural life. As the final results, the The friction stir welding (FSW) process is witnessing a optimum value was acquired by calculating the total normal- growth in a wide range of industrial applications due to the ized quality loss and multiple signal-to-noise ratios based on minimal governing parameters and many other advantages as unequal desirability. The significant level of the parameters a solid state welding compared to the commonly used fusion was evaluated by using analysis of variance. Furthermore, welding process. However, tensile residual stress remains to the second-order model for predicting the objectives was de- be significant concern due to its extensive clamping and stir- rived by applying response surface methodology. It can be ring process which can lead to lower fatigue resistance partic- summarized that, first, the affecting parameters to obtain su- ularly in structures subjected to fluctuating loads triggering a perior structural life can be ordered at significant level of ca. need for improvement [1–3]. The enhancement of the fatigue resistance of welded joints is becoming increasingly significant in many areas such as the * Yupiter H. P. Manurung railway, aerospace and automotive industries. A recent meth- [email protected] od of enhancing the fatigue resistance of welded aluminium alloy (AA) structures is to use modern post-weld treatment 1 Faculty of Mechanical Engineering, Universiti Teknologi MARA processes. Improving the fatigue resistance of welded joints (UiTM), Shah Alam, Malaysia by conventional improvement methods such as grinding, shot 2 Universiti Kuala Lumpur Malaysia France Insitute (UNIKLMFI), peening, air hammer peening or tungsten inert gas (TIG) Kuala Lumpur, Malaysia dressing are well established. However, these techniques are 3 Technogerma Engineering & Consultancy, Mont Kiara, Kuala inconsistent, not always efficient, have limited application Lumpur, Malaysia areas and can cause other related problems. The relatively Author's personal copy Int J Adv Manuf Technol new technique of high frequency mechanical impact (HFMI) most possible minimum value of process performance at the peening of weld toes as well as heat affected zones offers a optimum point of process parameters. Numerous researches favourable alternative for weld improvement. HFMI is termed involving the optimization of process parameters for FSW as a method in which a hardened steel pin impact on the surface well as other welding processes had been carried out previ- of the metal to be treated at a required frequency and pressure ously to obtain the optimal point of governing parameters by magnitude in accordance to specifications. employing the multi-objective Taguchi method (MTM) and There are a quite number of research conducted using con- response surface methodology (RSM). A mathematical model ventional and HFMI methods in the past decades. Rodopoulos was successfully developed for quality features of resistance et al. [3] investigated through experimental study the effects of spot welding [10]. A hybrid TM using the Taguchi quality loss ultrasonic impact treatment (UIT) on the fatigue resistance of function and RSM was employed for the multi-response opti- friction stir welded AA panels. The effects of laser and shot mization of a laser beam cutting process [11]. TM has been peening on the mechanical properties with iso-stress assump- successfully applied to determine the optimal FSW process tion were studied by O. Hatemleh [4] to calculate local stress– parameter combination that would maximize the tensile strain curves of friction stir welded 2195 AA joints. A signif- strength, notch tensile strength and the weld sub-surface hard- icant improvement in the fatigue resistance of friction stir ness of the AA6061 joints by Periyasamy et al. [12]. TM was welded AA7075 by applying ultrasonic peening (UP) was also effectively used to optimize the process parameters of reported out by Qiulin et al. [5] using a self-made device with FSWAA6061 in an attempt to minimize the heat affected zone a stress ratio of R = 0.5. The strengthened layer caused by the (HAZ) distance to the weld line [13]. The prediction of the plastic variation, surface hardening and consistency of tissue, optimum tensile strength by varying process parameters for as well as compressive transversal residual stress induced by joining of a butt joint dissimilar Al–Cu alloy AA2219 and UP were found to be the main reasons for the increased life AA5083 plates using TM technique was investigated by cycle. Microstructural and fatigue properties of FSW made of Koilraj et al. [14]. AA2043 with controlled shot peening was examined by Ali Based on past researches, it is obvious that fatigue strength et al. [6] and stated that the compressive residual stress intro- of material can be improved significantly with the help of duced by the peening process attributed to an increment in the various methods including HFMI and process parameter op- low cycle region. In an attempt to restore the degraded fatigue timization is an important criterion prior to the application of performance due to FSW, laser peening without coating welding and cutting process. However, no attempt has been (LPwC) was applied to FSW AA6061 joints by Sano et al. made yet to employ multi-objective parameter optimization [7] and obtained an increment of 30 MPa from an as-welded for FSW with subsequent post-weld treatment especially value of 90 MPa. It was pointed that a higher fatigue perfor- using the recently innovated pneumatic impact treatment mance can be expected if the processing parameters in LPwC (PIT) which also falls under the generic term of HFMI method were optimized. The effect of HFMI on butt welds, T-joints as mentioned in [15 ]. As first hypothesis in achieving opti- and longitudinal attachments for mild construction steel mum
Recommended publications
  • Table of Contents
    Table of Contents Committees Preface Symposium A: Invited Lectures New Perspectives for Wrought Magnesium Alloys J. Bohlen, D. Letzig and K.U. Kainer 1 Automotive Mg Research and Development in North America J.A. Carpenter, J. Jackman, N.Y. Li, R.J. Osborne, B.R. Powell and P.S. Sklad 11 State of the Art in the Refining and Recycling of Magnesium L.F. Zhang and T. Dupont 25 Research and Development of Processing Technologies for Wrought Magnesium Alloys F.S. Pan, M.B. Yang, Y.L. Ma and G.S. Cole 37 Overview of CAST and Australian Magnesium Research D.H. StJohn 49 Development of Magnesium Alloys with High Performance S. Kamado and Y. Kojima 55 Symposium B: Cast Magnesium Alloys and Foundry Technologies Effects of Microstructure and Partial Melting on Tensile Properties of AZ91 Magnesium Cast Alloy T.P. Zhu, Z.W. Chen and W. Gao 65 Effect of Heat Treatment on the Microstructure and Creep Behavior of Mg-Sn-Ca Alloys T.A. Leil, Y.D. Huang, H. Dieringa, N. Hort, K.U. Kainer, J. Buršík, Y. Jirásková and K.P. Rao 69 Creep Behaviour and Microstructure of Magnesium Die Cast Alloys AZ91 and AE42 K. Wei, L.Y. Wei and R. Warren 73 Growth Rate of Small Fatigue Cracks of Cast Magnesium Alloy at Different Conditions X.S. Wang and J.H. Fan 77 A Cyclic Stress-Strain Constitutive Model for Polycrystalline Magnesium Alloy and its Application X.G. Zeng, Q.Y. Wang, J.H. Fan, Z.H. Gao and X.H. Peng 81 Dynamic Stress-Strain Behavior of AZ91 Alloy at High-Strain Rate G.Y.
    [Show full text]
  • 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.
    [Show full text]
  • Aste Bolaffi Auto Classiche
    ASTE BOLAFFI AUTO CLASSICHE Milano, 24 maggio 2019 STAFF OPERATIVO | OPERATIONAL TEAM Amministrazione e finanza Accounting and finance Simone Manenti [email protected] Maria Luisa Caliendo [email protected] Serena Giancale [email protected] Comunicazione Communication Silvia Lusetti [email protected] Ufficio stampa Press-office Margherita Criscuolo [email protected] Gestione organizzativa Organization Management Chiara Pogliano [email protected] Laura Cerruti [email protected] Christina Penza [email protected] Irene Toscana [email protected] Logistica Logistics Michele Sciascia [email protected] Ezio Chiantello [email protected] Elisabetta Deaglio [email protected] Simone Gennero [email protected] Fulvio Giannese [email protected] Roberto Massa Micon [email protected] Servizio clienti Customer service Filippo Guidotti [email protected] Erika Bonetto [email protected] Giuseppe Ibba [email protected] Amministratore sistema informatico lotto | lot 18 System administrator Maurizio Tuninetti [email protected] consulente | consultant lotti | lots 52-53 AUTO CLASSICHE Classic motor vehicles ASTA | AUCTION Venerdì 24 maggio 2019 Friday 24 May 2019 Lainate, Milano ore 15.00 | 3.00 pm lotti 1-56 | lots 1-56 ESPOSIZIONE | VIEWING da martedì 21 a venerdì 24 maggio 2019 from Tuesday 21 to Friday 24 May 2019 ore 11.00-19.00 | 11.00 am-7.00 pm La Pista via Manuel Fangio, Lainate, Milano INFORMAZIONI | ENQUIRIES tel +39 011-0199101
    [Show full text]
  • 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.
    [Show full text]
  • International Alloy Designations and Chemical Composition Limits for Wrought Aluminum and Wrought Aluminum Alloys
    International Alloy Designations and Chemical Composition Limits for Wrought Aluminum and Wrought Aluminum Alloys 1525 Wilson Boulevard, Arlington, VA 22209 www.aluminum.org With Support for On-line Access From: Aluminum Extruders Council Australian Aluminium Council Ltd. European Aluminium Association Japan Aluminium Association Alro S.A, R omania Revised: January 2015 Supersedes: February 2009 © Copyright 2015, The Aluminum Association, Inc. Unauthorized reproduction and sale by photocopy or any other method is illegal . Use of the Information The Aluminum Association has used its best efforts in compiling the information contained in this publication. Although the Association believes that its compilation procedures are reliable, it does not warrant, either expressly or impliedly, the accuracy or completeness of this information. The Aluminum Association assumes no responsibility or liability for the use of the information herein. All Aluminum Association published standards, data, specifications and other material are reviewed at least every five years and revised, reaffirmed or withdrawn. Users are advised to contact The Aluminum Association to ascertain whether the information in this publication has been superseded in the interim between publication and proposed use. CONTENTS Page FOREWORD ........................................................................................................... i SIGNATORIES TO THE DECLARATION OF ACCORD ..................................... ii-iii REGISTERED DESIGNATIONS AND CHEMICAL COMPOSITION
    [Show full text]
  • A Novel Brazing Technique for Aluminum
    WELDING RESEARCH SUPPLEMENT TO THE WELDING JOURNAL, JUNE 1994 Sponsored by the American Welding Society and Ihe Welding Research Council A Novel Brazing Technique for Aluminum A simplified and cost-effective method using an alloy powder mixture instead of a clad surface has been developed for brazing aluminum, copper and brass BY R. S. TIMSIT AND B. J. JANEWAY ABSTRACT. This paper describes a novel Introduction eutectic composition such as AA4045, brazing technique for aluminum, in AA4047 or AA4343 (Ref. 4). These alloys which at least one of the contacting alu­ The joining of metal parts by brazing contain 9 to 1 3 wt-% of Si and are char­ minum surfaces is coated with a powder- often involves the use of a filler metal acterized by a melting temperature (in a mixture consisting of silicon and a potas­ characterized by a liquidus temperature narrow range near 577°C) (Ref. 5) con­ sium fluoroaluminate flux. Brazing is above 450°C (842°F) but appreciably siderably lower than that of the core alloy carried out by heating the joint to ap­ below the solidus temperatures of the (~660°C). Joining is carried out at ap­ C proximately 600 C in nitrogen gas at core materials. On melting, the filler proximately 600°C (1112°F) in the pres­ near-atmospheric pressure over a time metal spreads between the closely fitted ence of a noncorrosive flux such as a flu­ interval of a few minutes. During heating, surfaces, forms a fillet around the joint oroaluminate salt (Refs. 1, 6) to remove the flux melts at 562°C and dissolves the and yields a metallurgical bond on cool­ native surface oxide films from the con­ surface oxide layers on the aluminum, ing.
    [Show full text]
  • Alloys for Aeronautic Applications: State of the Art and Perspectives
    metals Review Alloys for Aeronautic Applications: State of the Art and Perspectives Antonio Gloria 1, Roberto Montanari 2,*, Maria Richetta 2 and Alessandra Varone 2 1 Institute of Polymers, Composites and Biomaterials, National Research Council of Italy, V.le J.F. Kennedy 54-Mostra d’Oltremare Pad. 20, 80125 Naples, Italy; [email protected] 2 Department of Industrial Engineering, University of Rome “Tor Vergata”, 00133 Rome, Italy; [email protected] (M.R.); [email protected] (A.V.) * Correspondence: [email protected]; Tel.: +39-06-7259-7182 Received: 16 May 2019; Accepted: 4 June 2019; Published: 6 June 2019 Abstract: In recent years, a great effort has been devoted to developing a new generation of materials for aeronautic applications. The driving force behind this effort is the reduction of costs, by extending the service life of aircraft parts (structural and engine components) and increasing fuel efficiency, load capacity and flight range. The present paper examines the most important classes of metallic materials including Al alloys, Ti alloys, Mg alloys, steels, Ni superalloys and metal matrix composites (MMC), with the scope to provide an overview of recent advancements and to highlight current problems and perspectives related to metals for aeronautics. Keywords: alloys; aeronautic applications; mechanical properties; corrosion resistance 1. Introduction The strong competition in the industrial aeronautic sector pushes towards the production of aircrafts with reduced operating costs, namely, extended service life, better fuel efficiency, increased payload and flight range. From this perspective, the development of new materials and/or materials with improved characteristics is one of the key factors; the principal targets are weight reduction and service life extension of aircraft components and structures [1].
    [Show full text]
  • Aluminum Cast Alloys: Enabling Tools for Improved Performance
    Aluminum Cast Alloys: Enabling Tools for Improved Performance D. Apelian 2009 Although great care has been taken to provide accurate and current information, neither the author(s), nor the publisher, nor anyone else associated with this publication, shall be liable for any loss, damage or liability directly or indirectly caused or alleged to be caused by this book. The material contained herein is not intended to provide specific advice or recommendations for any specific situation. Any opinions expressed by the author(s) are not necessarily those of NADCA. Trademark notice: Product or corporate names may be trademarks or registered trademarks and are used only for identification and explanation without intent to infringe nor endorse the product or corporation. © 2009 by North American Die Casting Association, Wheeling, Illinois. All Rights Reserved. Neither this book nor any part may be reproduced or transmitted in any form or by any means, electronic or mechanical, including photocopying, microfilming, and recording, or by any information storage and retrieval system, without permission in writing from the publisher. Worldwide Report Aluminum Cast Alloys: Enabling Tools for Improved Performance By: D. Apelian NADCA 2009 Table of Contents 1. Introduction 1 2. Industry Needs 3 3. Aluminum Alloy – Fundamentals 5 3.1 Effects of Alloying Elements 6 3.2 General Applications of Alloy Families 14 4. Enabling Tools 19 4.1 Measurements 19 a) Chemistry Control 19 b) Castability 24 4.2 Predictive 32 a) Composition and Properties 32 b) Phase Transformations 35 c) Solidification 37 5. Case Studies 45 5.1 Optimization of 380 45 5.2 Thermal Management Alloys 47 5.3 Quench Sensitivity 48 5.4 High Integrity Casting – SSM 50 6.
    [Show full text]
  • Couplant Effect and Evaluation of FSW AA6061-T6 Butt Welded Joint
    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). Couplant Effect and Evaluation of FSW AA6061-T6 Butt Welded Joint By Itai Mumvenge 217093863 Submitted in partial fulfilment of the requirements for the degree of Master of Engineering in Mechanical Engineering In the Department of Mechanical Engineering Science Of the Faculty of Engineering and the Built Environment At the University of Johannesburg, South Africa Supervisor: Dr Stephen A. Akinlabi Co-Supervisor: Dr Peter M. Mashinini November, 2017 i 1. DEDICATION This dissertation is dedicated to my late grandmother Esnath Mvenge ii 2. COPYRIGHT STATEMENT The copyright of this dissertation is owned by the University of Johannesburg, South Africa. No information derived from this publication may be published without the author’s prior consent, unless correctly referenced. ………………………………….. 25 November 2017 Author’s Signature Date: iii 3. AUTHOR DECLARATION I, Mumvenge Itai hereby declare that the research work documented in this dissertation is my own, and no portion of the work has been submitted in support of an application for another degree or qualification at this or any other university or institute of learning.
    [Show full text]
  • Aste Bolaffi Auto E Moto Classiche
    ASTE BOLAFFI AUTO E MOTO CLASSICHE Milano, 23 maggio 2018 ASTE BOLAFFI S.p.A. Società del Gruppo Bolaffi ESPERTI | SPECIALISTS Presidente e Amministratore Delegato Francobolli Orologi Chairman and C.E.O. Stamps Watches Giulio Filippo Bolaffi [email protected] [email protected] Consiglieri Matteo Armandi Aldo Aurili consulente | consultant Directors Giovanna Morando Enrico Aurili consulente | consultant Nicola Bolaffi Alberto Ponti Pietro Sangiorgio assistente | assistant Fabrizio Prete Monete, banconote e medaglie Arti del Novecento Business Development Coins, banknotes and medals 20th Century Art Cristiano Collari [email protected] [email protected] [email protected] Gabriele Tonello Cristiano Collari Carlo Barzan Francesca Benfante Operations Alberto Pettinaroli Tommaso Marchiaro Arredi, dipinti e oggetti d'arte [email protected] Manifesti Furniture, paintings and works of art Posters [email protected] [email protected] Cristiano Collari Torino Francesca Benfante Umberta Boetti Villanis Via Cavour 17 Armando Giuffrida Francesca Benfante 10123, Torino consulente | consultant Tel. +39 011-0199101 Auto e moto classiche Fax +39 011-5620456 Libri rari e autografi Classic motor vehicles Rare books and autographs [email protected] [email protected] Tommaso Marchiaro Cristiano Collari Ezio Chiantello Annette Pozzo Stefano Angelino consulente | consultant Massimo Delbò consulente | consultant Antonio Ghini consulente | consultant Grafica | Graphic design Vini e distillati Wines and spirits Pierangelo
    [Show full text]
  • T.C. ALTINBAŞ UNIVERSITY Institute of Graduate Studies Mechanical
    T.C. ALTINBAŞ UNIVERSITY Institute of Graduate Studies Mechanical Engineering A MODEL FOR THE DISTRIBUTION OF TEMPERATURE ON THE ALUMINUM ALLOY WHEN USING FRICTION WELDING Sewara Mohsin Mahealdeen SHEKHAN Master Thesis Supervisor Asst. Prof. Dr. Hakan KAYGUSUZ Istanbul, (2020) A MODEL FOR THE DISTRIBUTION OF TEMPERATURE ON THE ALUMINUM ALLOY WHEN USING FRICTION WELDING By Sewara Mohsin Mahealdeen SHEKHAN Mechanical Engineering Submitted to the Graduate School of Science and Engineering in partial fulfillment of the requirements for the degree of Master of Science ALTINBAŞ UNIVERSITY 2020 The thesis titled “A MODEL FOR THE DISTRIBUTION OF TEMPERATURE ON THE ALUMINUM ALLOY WHEN USING FRICTION WELDING” prepared and presented by SEWARA MOHSIN was accepted as a Master of Science Thesis in Mechanical Engineering. Asst. Prof. Dr. Hakan KAYGUSUZ Supervisor Thesis Defense Jury Member School of Engineering and Asst. Prof.Dr. Hakan Natural Sciences, KAYGUSUZ AltinbasUniversity __________________ School of Engineering and Asst. Prof.Dr. İbrahim KOÇ Natural Sciences, AltinbasUniversity __________________ Faculty of Engineering and Asst. Prof.Dr. Bengi ÖZUĞUR Natural Sciences Kadir Has UYSAL University __________________ I certify that this thesis satisfies all the requirements as a thesis for the degree of Master of Science. Approval Date of Institute of Graduate studies __/__/__ iii I hereby declare that all information in this document has been obtained and presented in accordance with academic rules and ethical conduct. I also declare that, as required by these rules and conduct, I have fully cited and referenced all material and results that are not original to this work. Sewara Mohsin Mahealdeen SHEKHAN iv DEDICATION I would like to dedicate this work to my first teacher, my mother, my first supporter and role model, my father and my companion throughout the journey.
    [Show full text]
  • Registered International Designation
    International Alloy Designations and Chemical Composition Limits for Wrought Aluminum and Wrought Aluminum Alloys 1400 Crystal Drive, Suite 430, Arlington, VA 22209 www.aluminum.org Revised: August 2018 Supersedes: January 2015 © Copyright 2018, The Aluminum Association, Inc. Unauthorized reproduction and sale by photocopy or any other method is illegal. ISSN: 2377-6692 Use of the Information The Aluminum Association has used its best efforts in compiling the information contained in this publication. Although the Association believes that its compilation procedures are reliable, it does not warrant, either expressly or impliedly, the accuracy or completeness of this information. The Aluminum Association assumes no responsibility or liability for the use of the information herein. All Aluminum Association published standards, data, specifications and other material are reviewed at least every five years and revised, reaffirmed or withdrawn. Users are advised to contact The Aluminum Association to ascertain whether the information in this publication has been superseded in the interim between publication and proposed use. CONTENTS Page FOREWORD ........................................................................................................... i SIGNATORIES TO THE DECLARATION OF ACCORD ..................................... ii-iii REGISTERED DESIGNATIONS AND CHEMICAL COMPOSITION LIMITS .... 1-17 Footnotes ........................................................................................................ 18 TABLE OF NOMINAL DENSITIES
    [Show full text]