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Damage Tolerance Behaviour of Integral Aircraft Structures Obtained by Stationary Shoulder Friction Stir Welding
Damage Tolerance Behaviour of Integral Aircraft Structures Obtained by Stationary Shoulder Friction Stir Welding Vom Promotionsausschuss der Technischen Universität Hamburg zur Erlangung des akademischen Grades Doktor-Ingenieur (Dr.-Ing.) genehmigte Dissertation von Alessandro Barbini aus Pisa (Italien) 2021 1. Gutachter: Prof. Dr.-Ing. Norbert Huber 2. Gutachter: Prof. Dr.-Ing Xiang Zhang Vorsitzende: Prof. Dr. Erica Lilleodden Mündliche Prüfung: 3. Juli 2020 Abstract Research focusing on new ways to achieve weight reduction without sacrificing the safety performances of an aircraft is the subject of a constant push in the aeronautical industry. The use of riveting to join skin and stringer is highly optimised but in order to reduce structural weight, aside from the continuous development of new materials, it is important to use the already available materials in an efficient way. For this reason, friction stir welding (FSW) was looked at for many years as a suitable replacement alternative for riveting but the focus of the research was mostly driven with a material science point of view. Therefore, the development of a new solid-state welding technology ensuring good material properties and, at the same time, being investigated as a structural joint is still a necessity. The present-study addresses the development of a new procedure for joining skin and stringers made of dissimilar aluminium alloys by stationary shoulder friction stir welding (SSFSW), which is to be applied in primary aircraft structures. Three different joint configurations were developed, and their performances were compared. At first, a fundamental analysis of the correlation between the two main process parameters, welding speed and rotational speed on heat development and joint formation, was conducted. -
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. -
This Item Is Held in Loughborough University's Institutional Repository
This item is held in Loughborough University’s Institutional Repository (https://dspace.lboro.ac.uk/) and was harvested from the British Library’s EThOS service (http://www.ethos.bl.uk/). It is made available under the following Creative Commons Licence conditions. For the full text of this licence, please go to: http://creativecommons.org/licenses/by-nc-nd/2.5/ MODELLING OF GRAIN BOUNDARY SEGREGATION, PRECIPITATION AND PRECIPITATE-FREE ZONES OF HIGH STRENGTH ALUMINIUM ALLOYS by Hong JIANG A Doctoral Thesis Submitted in partial fulfilment of the requirements for the award of Doctor of Philosophy of the Loughborough University of Technology March 1994 r-'7- 77'--", -- 0 by H. Jiang, 1994 Acknowledgments The work described in this thesis could not have been carried out without the help of others, whose support I gratefully acknowledge. In particular, sincere thanks must go to my supervisor, Professor Roy Faulkner of Loughborough University for his help, advice and encouragement throughout the duration of this work. Also I am deeply indebted to Mr John Bates, the Senior Laboratory Officer at IPTME for his advice, general instruction and guidance in the techniques for the experimental work and, thanks to Mr Shenghau Song, the Research Student at HYME for his kindly assistancein the experimental work. For financial support I am indebted to Loughborough University of Technology for their award of a Overseas Research Student Award and to Alcan International, Ban bury Laboratory for their supplementationof a ResearchStudentship. - III Abstract Aluminium alloys of the 7000 series with their high strength to weight ratio characteristics have been considered as a excellent choice in airftwne structure manufacturing. -
Aluminium 7020 Alloy and Its Welding Fatigue Behaviour
6 Aluminium 7020 Alloy and Its Welding Fatigue Behaviour Carlos Bloem1, Maria Salvador2, Vicente Amigó2 and Mary Vergara1 1Universidad de Los Andes 2Universidad Politécnica de Valencia 1Venezuela 2España 1. Introduction Since Alfred Wilm discovered the aluminium alloys hardening precipitation phenomena at the begining of the last century (Polmear 1996), the use of aluminium alloys has increased, owing their advantages against corrosion and good strength weight ratio. The Aluminium Zinc Magnesium ternary alloys are getting more relevance every day. These alloys are commonly called Al-Zn-Mg. In this family the most used are the AA7005 and AA 7020, which are nearly the same alloys. Although the most remarkable difference between them is the slightly better mechanical behaviour of the 7020 one after welding. The ageing development of these alloys follows a simple precipitation phenomena summarized as: αss→α1+GP→α2+η’→αeq+η Some investigators propose a transitional step on the Guinier Preston (GPs) evolution that gives the response to the natural ageing as: αss→α1+GPround→α2+GPordered →α3+η’→α4+η→α4+T The calorimetric study of the natural ageing evolution shows that there is no difference on the heat exchange of η’ and η. So, the GPs evolution is the responsible of strengthening of the alloy. The mechanical properties of AA7020 are evaluated and the exponential evolution is advisable, due to natural ageing. The fatigue behaviour of AA7020 natural aged shows a typical Aluminium Wohler pattern. From this curve a mathematical model is proposed. Welded aluminium: Riveted and welded aluminium structures are getting more relevance every day. -
Metallurgical Abstracts (General and Non-Ferrous)
METALLURGICAL ABSTRACTS (GENERAL AND NON-FERROUS) Yolume 3 DEGEMBER 1936 Part 12 I.—PROPERTIES OF METALS (Continued from pp. ‘139-449.) ♦Tensile Properties of Single Crystal and Polyerystalline Aluminium. G. Welter and T. Mojmir (Wiadomości Instytutu Metalurgji i Metaloznawstwa (Warszawa), 1936, 3, (3), 130-136).—[In Polish, with German summary.] In the preparation of large single crystals of aluminium from the polyerystalline metal by recrystallization the orientation and shape of the single crystals depend on the purity of the metal, e.g. with 99-8% aluminium tho crystal boundaries are always perpendicular to the axis of the rod, whereas with 99-5% metal the crystal boundaries are practieally always parallel to this axis. With rods consisting of two large crystals the relative elongation at the grain boundary is the smallest. The naturę of the fracture of the specimen and the reduction in area depend on tho crystal structure. Determinations of the elastic limits (0-001,0-002,0-01, and 0-2% permanent deformation) show that there is a sudden transition from purely elastic to plastic deformation so that the load-elongation curve bends sharply at right angles. The highest elastic modulus was obtained with single crystal 99-8% aluminium (7150 kg./ mm.3), while the average valuo for polyerystalline aluminium is 6500 kg./mm.2. The elastic limit (0-001% elongation) yaries from 0-75 to 1-6 kg./mm.2; the tensile strength of single crystal aluminium is 4-5 kg./mm.2 and the elongation 50-100%. With inereasing grain-size the tensile strength of aluminium decreases rapidly at first, then more slowly—A. -
Determination of Kinetic Parameters from Calorimetric Study of Solid State Reactions in 7150 AlZnMg Alloy
Determination of kinetic parameters from calorimetric study of solid state reactions in 7150 AlZnMg alloy K. S. GHOSH1 , N. GAO 2 1. Department of Metallurgical and Materials Engineering, National Institute of Technology, Durgapur 713 209, India; 2. Materials Research Group, School of Engineering Science, University of Southampton, Southampton, SO17 1BJ, UK Received 4 August 2010; accepted 19 November 2010 Abstract: Differential scanning calorimetric (DSC) study was carried out at different heating rates to examine the solid state reactions in a 7150 AlZnMg alloy in waterquenched (WQ) state, naturally and artificially aged tempers. The exothermic and endothermic peaks of the thermograms indicating the solid state reaction sequence were identified. The shift of peak temperatures to higher temperatures with increasing heating rates suggests that the solid state reactions are thermally activated and kinetically controlled. The artificial aging behaviour of the alloy was assessed by measuring the variations of hardness with aging time. The fraction of transformation (Y), the rate of transformation (dY/dt), the transformation function f(Y), and the kinetic parameters such as activation energy (Q) and frequency factor (k0) of all the solid state reactions in the alloy were determined by analyzing the DSC data, i.e. heat flow involved with the corresponding DSC peaks. It was found that the kinetic parameters of the solid state reactions are in good agreement with the published data. Key words: 7150 AlZnMg alloy; DSC; aging behaviour; activation energy; transformation function method, i.e. susceptibility to errors and timeconsuming 1 Introduction technique, calorimetric method can conveniently be utilized to understand the kinetics of all types of Aluminium alloys of 7xxx series AlZnMg are precipitation and dissolution reactions in aluminium widely used in aircraft and aerovehicle structural alloys [12−13]. -
Precious Metals
V o l . 3 Part 12 The Monthly Journal of the INSTITUTE OF METALS ind METALLURGICAL ABSTRACTS CONTENTS PAGE Institute News and Announcements 617 Personal Notes 618 Local Sections News [politechnik;] 619 Meetings of O ther Societies 621 Notice to Authors of Papers 622 757. Creep of Lead and Lead Alloys. Part 1.—Creep of Virgin Lead. By J. McKeown 623 758. The Constitution of Silver-Rich Antimony-Silver Alloys. By P. W . Reynolds and W . Hume-Rothery 645 759. An Aluminium Statue of 1893 : Gilbert’s Eros. By R. S. Hutton and R. Sellgman 655 Metallurgical Abstracts 487-628 DECEMBER 1936 Copyright Entered at Stationers' Hall TRADE MARK THIS COPPER-SILICON-MANGANESE ALLOY IS NOW AVAILABLE AS A BRITISH PRODUCT • • • • " EVERDUR ” (i.c.i™Metds Ltd.) offers these outstanding advantages 9 Strength equal to that of steel 9 Remarkable corrosion resistance 9 High fatigue limit • Welds readily by all usual methods O Makes unusually sound castings 9 Excellent machining qualities • Easily worked hot or cold A Comparatively inexpensive The booklet “ Everdur,” in addition to giving further details of these properties, also contains valuable information relating to applications and physical characteristics. “ Everdur” is available as sheet, strip, tube, rod, plates, wire, in all sizes, and also in the form of casting ingots. PLEASE ADDRESS THE COUPON TO IMPERIAL CHEMICAL INDUSTRIES LTD. DEPT. M9, IMPERIAL CHEMICAL HOUSE, LONDON, S.W.I Please send a copy o f the “ Everdur ” booklet Nam e................................................................................................................................. ........ Address..................................................................................................................................... P r in t e d in G r e a t B r it a in b y R ic h a r d C la y a n d S o n s, L im it e d , B u n g a y , S u f f o l k . -
SPRAY CASTING (Derleme) Elmas SALAMCI SPREY
G.Ü. Fen Bilimleri Dergisi ISSN 1303-9709 G.U. Journal of Science 17(2): 155-173 (2004) 17(2):155-173 (2004) SPRAY CASTING (Derleme) Elmas SALAMCI Zonguldak Karaelmas Üniversitesi, Karabük Teknik Eğitim Fakültesi 78200, Karabük, TÜRKİYE [email protected] ABSTRACT This paper is designed to provide a basic review of spray casting. A brief overview of the historical development of spray casting and the description of plant and equipment have been given. Following metallurgical characteristics of spray formed alloys, process parameters and solidification mechanism of spray deposition have been discussed in detail. Finally, microstructure and mechanical properties of the selected spray cast Al-Zn-Mg-Cu alloys have been presented and compared with conventionally and powder metallurgy processed 7xxx aluminium alloys. Keywords: Spray casting, Osprey, LDC, Al-Zn-Mg-Cu SPREY DÖKÜM (Review) ÖZET Bu makalede sprey döküm yöntemi incelendi. Sprey dökümün özet olarak tarihsel gelişimi ve proses hakkında bilgi verildi. Daha sonra sprey dökümle üretilmiş alaşımların metalurjik özellikleri, proses parametreleri ve sprey döküm yönteminin katılaşma mekanizması detaylı olarak tartışıldı. Son olarak bazı sprey dökülmüş Al-Zn-Mg-Cu alaşımlarının mikroyapı ve mekanik özellikleri verildi ve bu sonuçlar geleneksel döküm yöntemi ve toz metalurjisiyle üretilmiş 7xxx serisi alüminyum alaşımlarının özellikleri ile kıyaslandı. Anahtar Kelimeler: Sprey döküm, Osprey, LDC, Al-Zn-Mg-Cu 1. GİRİŞ 1. INTRODUCTION Hızlı katılaşma yoluyla direk olarak eriyikten alaşım ve Spray forming, spray casting and spray deposition are kompozit malzemelerin üretildiği prosese sprey şekil terms used to describe a process that produces rapidly verme, sprey döküm veya sprey biriktirme yöntemi denir. solidified alloys and composite materials directly from the Bu yöntemde ergimiş metalin atomizasyonu ile üretilen melt. -
Compression Test of Aluminium Alloy at Different Strain Rate
1 COMPRESSION TEST OF ALUMINIUM ALLOY AT DIFFERENT STRAIN RATE A THESIS SUBMITTED IN PARTIAL FULFILMENT OF THE REQUIREMENTS FOR THE DEGREE OF Bachelor of Technology In Mechanical Engineering By RAHUL RAJ 109ME0407 Under the Guidance of Prof. S.K.SAHOO Department of Mechanical Engineering National Institute of Technology ROURKELA 2 National Institute of Technology ROURKELA CERTIFICATE This is to certify that thesis entitled, “COMPRESSION TEST OF ALUMINIUM ALLOY AT DIFFERENT STRAIN RATE” submitted by RAHUL RAJ in partial fulfilment of the requirements for the award of Bachelor of Technology Degree in Mechanical Engineering at National Institute of Technology Rourkela is an authentic work carried out by him under my Supervision and guidance. To the best of my knowledge, the matter included in this thesis has not been submitted to any other university or institute for award of any Degree. Date: 10th may, 2013 Prof. S.K.SAHOO Dept. of Mechanical Engineering National Institute of Technology Rourkela- 769008 3 ACKNOWLEDGEMENT I express my deep sense of gratitude and indebtedness to my project guide Prof S.K.Sahoo, Department of Mechanical Engineering, NIT Rourkela for introducing the topic and for his best guidance, consistent encouragement and constant supervision throughout the course of this work. I would like to give special thanks to Mr. srikar, PG scholar in mechanical engineering who gave his valuable time and support for this project work. I also express my sincere gratitude to Mr. Susant Sahu PG Scholars in Mechanical Engineering for giving their valuable time. I am grateful to Prof. K.P.Maity, Head of the Department of Mechanical Engineering for providing me the necessary facilities in the department. -
Friction Stir Welding of 38 Mm OD 6082-T6 Aluminium Tubes
University of Plymouth PEARL https://pearl.plymouth.ac.uk 01 University of Plymouth Research Outputs University of Plymouth Research Outputs 2016-12 Semiautomatic friction stir welding of 38 mm OD 6082-T6 aluminium tubes Hattingh, DG http://hdl.handle.net/10026.1/5455 10.1016/j.jmatprotec.2016.07.027 JOURNAL OF MATERIALS PROCESSING TECHNOLOGY All content in PEARL is protected by copyright law. Author manuscripts are made available in accordance with publisher policies. Please cite only the published version using the details provided on the item record or document. In the absence of an open licence (e.g. Creative Commons), permissions for further reuse of content should be sought from the publisher or author. Friction Stir Welding of 38 mm OD 6082-T6 Aluminium Tubes – Process Development and Microstructure D. G. Hattingh1 , L. G. von Welligh1 , D. Bernard1, L. Susmel2 , R. Tovo3, and M. N. James1, 4 1 Department of Mechanical Engineering, Nelson Mandela Metropolitan University, Port Elizabeth (South Africa) 2 Department of Civil & Structural Engineering, University of Sheffield, Sheffield (UK) 3 Department of Engineering, University of Ferrara, Ferrara (Italy) 4 School of Marine Science & Engineering, University of Plymouth, Plymouth (UK) e-mail: [email protected]; [email protected] Keywords: Friction stir welding; 6082 aluminium alloy; small diameter tube; electron back-scatter diffraction; retracting pin tool Abstract This paper describes the development of a semi-automated friction stir welding (FSW) technique for joining 38 mm nominal outer diameter (OD) tubes of 6082-T6 aluminium alloy with 3.5 mm nominal wall thickness. Process development for this application of FSW required the integration of a rotational axis with the control system of the FSW machine as well as the development of a secondary human-machine interface (HMI) for this axis and also necessitated the design of a retracting tool pin in order to eliminate the exit hole of the pin. -
Effect of Preheating Condition on Strength of AA6060 Aluminium Alloy for Extrusion
Effect of Preheating Condition on Strength of AA6060 Aluminium Alloy for Extrusion Cheng Meng A thesis submitted in partial fulfilment of the Master of Engineering School of Engineering Auckland University of Technology March 2010 Copyright © 2010 Cheng Meng All rights reserved ABSTRACT Fletcher Aluminium is a New Zealand company that manufactures aluminium extrusions for the building market. Their extrusion process involves using a hydraulic ram to force heated raw supplied material, in the form of large diameter cylindrical logs, through a die land that is the desired product shape. The final quality of the extruded product is influenced by the extrusion temperature, ram pressure and extrusion speed. The speed of extrusion at Fletcher Aluminium is limited by the extrusion ram pressure because the extrusion machine is operating at the pressure limit of the compressor. Currently the company requires an increase in the extrusion speed, while maintaining quality requirements where these improvements are desired without upgrading the compressor. The press pressure is required to overcome friction and the flow stress of the billet, which is dependent on the precipitates and solutes conditions and their strengthening effects in the billet. However, the preheating temperature and extrusion speeds need to be sufficiently low enough to avoid hot tearing. This research starts to increase the ram speed by decreasing the Mg2Si content for precipitation strengthening. Heat treatment may be used to dissolve Mg2Si content by billet preheat to a temperature at or exceeds solvus temperature (TSolvus). However, a higher (than TSolvus) billet temperature may have two conflicting effects. First, a higher temperature in general reduces the flow stress thus lowering the required pressure. -
Closed-Loop Recycling • Mexican Aluminum Industry • Service Center Metals Ten Years & Growing Al Casting Conidence
• Closed-Loop Recycling • Mexican Aluminum Industry • Service Center Metals Ten Years & Growing Al Casting Conidence Built on innovation and reined through experience, Wagstaff billet and ingot casting technologies are a gateway to proitability. Casthouses around the world rely on the history, experience, and service offered by Wagstaff to foster conidence within the casting operation. That conidence is valuable and necessary to safely cast aluminum and to ultimately maximize proits in the marketplace. The leader in Direct Chill Casting Technology › Casting Machines › Automation › Rolling Ingot Casting Systems › Metal Level Control › Billet Casting Systems › Worldwide Service and Support To ind out how your operation can increase casting conidence Call +1 509 922 1404 | www.wagstaff.com Directory of Secondary Aluminum Equipment Mfrs and Suppliers Index Page 71 Categories/Companies Page 72 Alphabetical Listing of Companies Page 76 DEPARTMENTS: Light Metal World ............................................................................ Page 80 New Equipment Spotlight ............................................................... Page 84 Reg. U.S. Trademark Secondary News ............................................................................. Page 87 “The International Magazine of the Light Metal Industry” Extruder News ................................................................................. Page 88 Contracts & Expansions.................................................................. Page 90 July/August 2013 • Volume