Constitutive Model of 6063 Aluminum Alloy Under the Ultrasonic Vibration Upsetting Based on Johnson-Cook Model

Total Page:16

File Type:pdf, Size:1020Kb

Constitutive Model of 6063 Aluminum Alloy Under the Ultrasonic Vibration Upsetting Based on Johnson-Cook Model Ultrasonics 96 (2019) 1–9 Contents lists available at ScienceDirect Ultrasonics journal homepage: www.elsevier.com/locate/ultras Constitutive model of 6063 aluminum alloy under the ultrasonic vibration upsetting based on Johnson-Cook model T ⁎ Zhendong Xie, Yanjin Guan , Jun Lin, Jiqiang Zhai, Lihua Zhu Key Laboratory for Liquid-Solid Structural Evolution and Processing of Materials (Ministry of Education), Shandong University, Jinan 250061, China ARTICLE INFO ABSTRACT Keywords: Establishing an accurate constitutive relation in ultrasonic vibration assisted metal forming, can provides a Ultrasonic vibration reliable theoretical basis for analyzing the mechanism of the ultrasonic vibration on materials. A constitutive Johnson-Cook model model of 6063 aluminum alloy under the ultrasonic vibration upsetting at room temperature was constructed Strain rate based on Johnson-Cook Model and experimental results. The influence of amplitude and frequency on the yield Acoustic softening strength, hardening coefficient and exponent were analyzed quantitatively. Results showed that the yield Hardening strength was reduced due to the softening effect induced by the ultrasonic vibration. The maximum decreasing amount was 68.8% when imposing the maximum ultrasonic energy in this study. The hardening coefficient and exponent increased by 10.9% and 16.6% in maximum, respectively. However, the ultrasonic vibration has little impact on the strain rate hardening. The modified Johnson-Cook constitutive model under the ultrasonic vi- bration upsetting was established and was in good agreement with the experimental results. 1. Introduction ultrasonic intensity. Based on elastic-viscoplastic constitutive relation, He et al. [11] studied the variation of the uniaxial tensile stress and Considerable efforts are being devoted to the investigation of the strain under the vibration condition. A one-dimensional mechanical ultrasonic vibration assisted metal plastic forming and its acting me- model was established to describe the volume effect of low and medium chanism on materials in recent decades [1–3], and these developed frequency vibrations. They found that the vibrational tensile stress forming processes, including ultrasonic drawing, ultrasonic extrusion depends on the strain rate and strain history. According to the super- and ultrasonic upsetting [4–6], has been widely used in practice. position principle and the strain variation assumption proposed by Earlier studies [7–9] have shown that the influence of ultrasonic Kirchner, He et al. [12] also expressed a mathematical description of vibration on material properties mainly include two aspects: (1) the the volume effect, and they denoted that the physical nature of the volume effect which can reduce the flow stress, and (2) the surface volume effect was the decrease of the average stress. The influence of effect which affects the friction status between the die and the work- ultrasonic vibration on uniaxial tensile process depended on the fre- piece. Focusing on these two effects, many scholars have conducted quency, amplitude and deformation velocity. Zheng et al. [13] studied various studies. However, the influence and acting mechanism of ul- the special behavior of metals under super-frequency vibration, and trasonic vibration on metals and theirs plastic behaviors are still un- established the elastic constitutive equation of metals and emphasized clear and the quantitative description model has not been established. that the effect of microstructures should be taken into account. Ac- Therefore, many efforts have been devoted to construct theoretical cording to the vibration assisted tensile experiments with applying low models that can quantitatively describe the effect of ultrasonic vibra- frequency vibration, Cai et al. [14] constructed a one-dimensional tion on the plastic deformation behaviors of metals based on certain visco-elastoplastic model based on the Kirchner‘ assumption, and stu- assumptions and simplification. died the mechanism of volume effect. Atanasiu [10] systematically and quantitatively estimated the re- The above mentioned theoretical models only can reveal the influ- lation between the ultrasonic field and material properties, described ence of ultrasonic vibration on material behavior qualitatively and can’t the metal deformation behaviors in the process of ultrasonic assisted describe the stress-strain relationship under the ultrasonic vibration forming based on rigid-viscoplastic model and concluded that the yield condition quantificationally and accurately. Especially, the influence of strength of the material reduced exponentially with the increase of the the frequency and amplitude can’t be included into these theoretical ⁎ Corresponding author. E-mail address: [email protected] (Y. Guan). https://doi.org/10.1016/j.ultras.2019.03.017 Received 19 June 2018; Received in revised form 28 November 2018; Accepted 20 March 2019 Available online 21 March 2019 0041-624X/ © 2019 Elsevier B.V. All rights reserved. Z. Xie, et al. Ultrasonics 96 (2019) 1–9 models. Thus, based on Arrhennius thermal activation model and dis- strain hardening behavior of materials. C3 is the coefficient of strain- location evolution theory [15], Yao [16] proposed an acoustic softening rate hardening, reflecting the sensitivity of material to strain rate. m is model and an acoustic residual hardening model respectively. Upsetting the thermal softening exponent, meaning the softening effect of mate- tests assisted by high frequency vibration were conducted to construct rials subjected to thermal loading. Because all of the experiments in our the constitutive model of which the results showed a good agreement work were carried out at room temperature, T = Tr. Meanwhile, the with the experimental results. Wang [17] divided the softening effect of factors of strain, strain-rate and temperature that in the JC model are ultrasonic vibration into two aspects: acoustic softening and stress su- independent of each other. Thus, the effect of the temperature can be perposition, and then calculated the proportion of the stress reduction ignored and then the JC model can be simplified as induced by acoustic softening effect. Prabhakar et al. [18] also pro- posed a theoretical model based on the dislocation dynamics, which can n ⎡ ε̇⎤ σ =+()1(lnCCε12+ C 3 ) express the effect of strain, strain rate and amplitude on the stress. ⎣⎢ εṙ⎦⎥ (4) However, there are too many parameters that are hard to obtain In order to determine the parameters in (4), the upsetting tests through the experiments in these models. Therefore, it is necessary to under the reference strain-rate were performed firstly. When εε̇= , Eq.̇ construct a relatively convenient and accurate theoretical model to r (4) can be simplified as reflect the stress-strain relationship of the material deformed under the n ultrasonic vibration condition. σ =+()CCε12 (5) In general, an ideal model should be able to describe the materials’ plastic behaviors, such as strain-rate dependence, temperature depen- The value of C1 is determined as the yield stress σs at the strain of dence, strain and strain-rate history dependence, work-hardening or 0.2% at the reference strain-rate. In this study, the reference strain rate -3 −1 strain-hardening behaviors. However, it is extremely difficult and even εṙis 3.33 × 10 s . impossible to completely describe all these phenomena. Therefore, By rearranging Eq. (5) and taking natural logarithm on both sides of many scholars introduced necessary assumptions and tried to describe Eq. (5), it could be transformed into the following form: the deformation behavior in a wide range of strain rate and temperature ln(σσ−=s ) nε ln + ln C2 (6) as accurately as possible. At present, many phenomenological con- stitutive models are proposed which can well represent the materials’ Then, using the true stress-strain data under reference strain-rate plastic deformation behaviors in a certain range, such as Johnson-Cook condition, the relationship between lnε and ln(()σσ− s ) is determined. (JC) model [19], Zerilli-Armstrong model [20], Bodner-Partom model The values of n and C2 can be obtained as the slope and intercept of the [21], and Khan-Huang model [22]. Especially, the JC constitutive fitting line. model has been applied widely because of its simplicity and uni- After that, several upsetting tests under a list of strain rates should – versality [23 25]. be performed to obtain the unknown C3. Therefore, in this paper, the conventional upsetting (C-upsetting) It is found from Eq. (4) that the relationship between σ and ln(εε/̇ṙ) and ultrasonic vibration assisted upsetting (UV-upsetting) of 6063 Al can be decided by flow stresses under different strain rates. The value of ff n alloy under di erent strain rates were conducted, and the parameters in C3 can be calculated from the slope CC31·(+ Cε 2 ) of the fitting line of the JC model were estimated based on the experimental results. The σ-σ0.2. influence of the frequency and amplitude on material’s parameters was analyzed. Consequently, the modified JC model which couples with the 3. Ultrasonic vibration assisted upsetting ultrasonic vibration parameters was established, which can reflect the influence of ultrasonic vibration on the stress-strain relation of 6063 Al 3.1. Establishment of ultrasonic vibration assisted upsetting system alloy. This model provides a reliable theoretical basis for the analysis of the effect of ultrasonic vibration on the material deformation behaviors. The experimental system consists of a universal
Recommended publications
  • Tensile Behavior of Aluminium Alloy 6063 - T6 in Sea Water
    International Journal of Engineering Research and Development e-ISSN: 2278-067X, p-ISSN: 2278-800X, www.ijerd.com Volume 10, Issue 5 (May 2014), PP.68-74 Tensile Behavior of Aluminium Alloy 6063 - T6 In Sea Water P.John Maclins RVS Educational Trust’s Group of Institutions, Asst. Professor, Department of Aeronautical Engineering, Dindigul, Tamilnadu, India. Abstract:- Sea water, by virtue of its chloride content, is a most efficient electrolyte. The Omni-presence of oxygen in marine atmospheres, sea spray increases the aggressiveness of salt attack. The differential concentration of oxygen dissolved in a droplet of salt spray creates a cell in which attack is concentrated where the oxygen concentration is lowest. The sea environment is the most structurally hostile environment within which aircraft operate. The structural components are being exposed to salt spray continuously during its operation and it experiences heavy loading during landing. Corrosion also leads to crack propagation when subjected to loading. Corrosion along with damage leads to the failure of structural components prematurely and presents a serious problem in the aging aircraft. This requires a different approach to the maintenance of structural components subjected to corrosion and repetitive loads. This paper studies the effect of corrosion and low impact damage on aluminium alloy 6063- T6. The 6063 aluminium alloy that was used for the study was heat treated and soaked in seawater prepared per ASTM D1141 for different intervals of time between 0hours and 1000hours. Corroded specimens were subjected to low impact damage. The result shows a gradual degradation in mechanical properties of the alloy due to corrosion and damage.
    [Show full text]
  • MATRIX Al-ALLOYS for SILICON CARBIDE REINFORCED METAL MATRIX COMPOSITES
    IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 INFLUENCE OF VOLUME FRACTION, SIZE, CRACKING, CLUSTERING OF PARTICULATES AND POROSITY ON THE STRENGTH AND STIFFNESS OF 6063/SICP METAL MATRIX COMPOSITES A. Chennakesava Reddy1 1Professor, Department of Mechanical Engineering, JNTUH College of Engineering, Kukatpally, Hyderabad – 500 085, Telangana, India Abstract The objective of this study is to examine the influence of volume fraction, size of particulates, formation of precipitates at the matrix/particle interface, particle cracking, voids/porosity, and clustering of particulates on the strength and stiffness of 6063/SiCp metal matrix composites. Tensile strength and stiffness increase with an increase in the volume fraction of SiC particulates. The tensile strength and stiffness decrease with increase in size of the particulates, presence of porosity, clustering, and particle cracking. Formation of particulate clusters is more prominent in the composites having very small-reinforced particulates. Mg2Si compound is likely to precipitate at the matrix/particle interfaces of 6063/SiC composite. Keywords: 6063, SiC, clustering, cracking, porosity, clustering --------------------------------------------------------------------***------------------------------------------------------------------ 1. INTRODUCTION matrix composite have become of principal importance for the manufacturer to make a quality product as per the Consolidation of a high strength ceramic particulate in a soft designer specifications. The objective of this work is to metal matrix is the technological renovation in the domain study the influence of the volume fraction and particle size of composites for the designer to assure high specific elastic of SiCp, clustering and cracking of particulates, modulus, strength-to-weight ratio, fatigue durability, and voids/porosity, and formation of precipitates at the wear resistance in the fields of aerospace and automotive particle/matrix interface on the tensile strength and stiffness applications.
    [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]
  • ISSN: 2320-5407 Int. J. Adv. Res. 7(9), 779-794
    ISSN: 2320-5407 Int. J. Adv. Res. 7(9), 779-794 Journal Homepage: - www.journalijar.com Article DOI: 10.21474/IJAR01/9728 DOI URL: http://dx.doi.org/10.21474/IJAR01/9728 RESEARCH ARTICLE TAFEL POLARIZATION AND IMPEDANCE STUDIES OF AL-7075 ALLOY AND ITS COMPOSITES IN DIFFERENT MEDIUM. Sravanthi.M1, Dr.K.G.Manjunatha2, Dr.Saifulla Khan3 and Sunitha N4 1. Assistant professor, Department of Chemistry,AMC Engineeing College, Banneerghatta Main Road, Bangalore,Karnataka-560083, India. 2. Prof. and HOD R&D Centre, Department of Engineering Chemistry, Ghousia College of Engineering, Ramanagaram, Bangalore, Karnataka-56215, India. 3. Assistant professor, Department of Chemistry, Ghousia college of Engineering, B.M Road, Ramanagaram – Bangalore, Karnataka-562159, India. 4. Assistant Professor, Department of Chemistry, City Engineering College, Kanakapura Road, Bangalore, Karnataka-560083, India. …………………………………………………………………………………………………….... Manuscript Info Abstract ……………………. ……………………………………………………………… Manuscript History Aluminum metal matrix composites because of their high potential in Received: 09 July 2019 satisfying the recent demands have a wide variety of applications in Final Accepted: 12 August 2019 aviation, defense system, and automobile industries. It has been noticed Published: September 2019 in research that the properties of composites can be enhanced by the addition of ceramic particles like SiC and graphite to metal matrix Key words:- Al7075, OCP, Tafel polarization, EIS composites. This paper attempts on corrosion studies of Al 7075 base and SEM. alloy/SiC/graphite based composites in different inorganic acid mediums (0.1M HCl,0.1M H2SO4 medium) and neutral chloride medium (3.5% NaCl medium) by making use of Tafel Polarization Technique and Electrochemical Impedance Spectroscopy Technique. Test samples were casted by taking the various percent of SiC/graphite by stir casting method as per ASTM standards.
    [Show full text]
  • Comparison of Aluminum Alloys from Aircraft of Four Nations Involved in the WWII Conflict Using Multiscale Analyses and Archival Study
    heritage Article Comparison of Aluminum Alloys from Aircraft of Four Nations Involved in the WWII Conflict Using Multiscale Analyses and Archival Study Toufa Ouissi 1,2,*, Gilles Collaveri 3, Philippe Sciau 1, Jean-Marc Olivier 2 and Magali Brunet 1,* 1 CEMES, UPR 8011 CNRS, 31055 Toulouse, France; [email protected] 2 FRAMESPA, UMR 5136, University of Toulouse Jean-Jaurès, 31058 Toulouse, France; [email protected] 3 Aerocherche, 31700 Blagnac, France; [email protected] * Correspondence: [email protected] (T.O.); [email protected] (M.B.) Received: 30 September 2019; Accepted: 14 November 2019; Published: 22 November 2019 Abstract: Aluminum alloys are very interesting witnesses of industrial and technical development. The first ever developed was Duralumin, a light metal with good mechanical properties. In the 1930s, the rise of nationalism stimulated research and development, generating various aluminum alloys. This work reports the comparison of two versions of aluminum alloys, which were found in collected parts of WWII crashed aircraft from four nations: a Messerschmitt Bf 109 (DE), a Dewoitine D.520 (FR), and a P-51 Mustang (USA) and an Avro Lancaster (United Kingdom). The first version of alloy with magnesium content below or equal to 1 wt.% and the second version with higher magnesium content (1.5 wt.%), were identified as respectively AlCuMg1, AlCuMg2 in Germany; Duralumin, Duralumin F.R. in France; Hiduminium DU Brand, Hiduminium 72 in the UK and 17S, 24S in the USA. This study uses a multiscale approach based on historical research complimented by laboratory analyses of materials directly collected on the crashed aircraft.
    [Show full text]
  • Evaluación De La Resistencia a La Fatiga De La Aleación De Aluminio Aa-6061 Tratada Térmicamente Mediante Un Proceso De Envej
    UNIVERSIDAD DE CARABOBO FACULTAD DE INGENIERÍA ESCUELA DE INGENIERÍA MECÁNICA EVALUACIÓN DE LA RESISTENCIA A LA FATIGA DE LA ALEACIÓN DE ALUMINIO AA-6061 TRATADA TÉRMICAMENTE MEDIANTE UN PROCESO DE ENVEJECIMIENTO ARTIFICIAL CON PERÍODOS DE 8 Y 10 HORAS. AUTORES: Martínez Motamayor, Javier Enrique Pérez Ramos, Nestor Osue TUTOR: Díaz, Eleazar Valencia, Noviembre del 2008 DEDICATORIA El presente trabajo especial de grado está dedicado primero que nada, a Dios por darme la oportunidad de llegar a donde he llegado y por ser siempre mi fortaleza en momentos de debilidad. En segundo lugar, a toda mi gran familia, pero en especial a mis padres Rubén José Martínez Pisani y Clara Cecilia Motamayor de Martínez, quienes me han enseñado grandes cosas a lo largo de mi vida, haciendo énfasis en los valores y el trabajo duro para alcanzar todas las metas propuestas. También quisiera dedicarlo a mi hermana Valeria Valentina Martínez Motamayor, por su cariño y apoyo incondicional. Por último, pero no menos importante, se lo dedico a mi Alma Mater la Universidad de Carabobo y a mi querido país Venezuela, de los cuales me siento orgulloso de provenir y que por ellos pienso luchar y trabajar para ayudar a que se desarrollen y progresen cada día más. Javier Enrique Martínez Motamayor DEDICATORIA No quiero que culmine mi carrera sin antes dar gracias a dios por darme la fuerza y su eterna compañía en los momentos difíciles de mi carrera. A mis padres que han sido, son y seguirán siendo mi apoyo incondicional cuando necesité un consejo a lo largo de toda mi vida.
    [Show full text]
  • Tensile Fractography of Artificially Aged Al6061-B4c Composites
    Proceedings of 3rd International Conference on Mechanical and Aeronautical Engineering Held on 18th- 19th January 2017, in Bangkok, Thailand. ISBN: 9788193137390 TENSILE FRACTOGRAPHY OF ARTIFICIALLY AGED AL6061-B4C COMPOSITES Gowri Shankar Achutha Kini Department of Mechanical and Manufacturing Department of Mechanical and Manufacturing Engineering, Manipal UniversityManipal Engineering, Manipal UniversityManipal Institute of Technology,Manipal, Institute of Technology,Manipal Karnataka State, India Karnataka State, India S S Sharma Department of Mechanical and Manufacturing Engineering, Manipal UniversityManipal Institute of Technology,Manipal Karnataka State, India Abstract— Presence of B4C reinforced particles in I. INTRODUCTION Al6061 alloy and various weight percentages of (2, Aluminum- magnesium-silicon alloys (Al-Mg-Si; also 4 and 6) on the hardness and tensile behaviour is denoted as 6xxx series), are medium strength, heat studied in the present work. Under different aging treatable alloys with good formability and corrosion temperatures the influence of artificial aging on the resistance. The 6061Al alloy has been studied mechanical properties was also assessed. Brinell extensively because of their technological importance macro hardness and mechanism of tensile fracture and farther increase in strength obtained by behavior have been discussed. Failure mode of precipitation hardening [1]. Aluminium matrix fracture surface is studied to determine the composites reinforced with ceramic particles such as parameters which influence the crack growth SiC, B4C, Al2O3 and TiC are the most commonly used characteristics. Lower temperature aging and materials in automobile and marine industries, have addition of B4C particles shows improvement in been paid more consideration because of high strength, hardness by 170% and tensile strength by 90% due high modulus and low density.
    [Show full text]
  • Experimental Studies on Grey Cast Iron Reinforced Aa6061 Composite
    EXPERIMENTAL STUDIES ON GREY CAST IRON REINFORCED AA6061 COMPOSITE 1SHIVAPRAKASH Y M, 2GOWRISHANKAR M C, 3SS SHARMA, 4K V SREENIVASA PRASAD 1MIT,Manipal,Karnataka,India; 2MIT,Manipal,Karnataka,India; 3MIT,Manipal,Karnataka,India; 4SJCE,Mysore,Karnataka,India E-mail: [email protected], [email protected], [email protected], [email protected] Abstract- Aluminium alloy composites are widely used because of their higher strength, stiffness and good wear resistance. In producing these composites the reinforcing materials used in common have been silicon carbide, aluminum oxide, boron carbide and graphite in the form of particles or whiskers. The ceramic particles reinforced aluminum composites are new generation materials which can be tailored for particular properties for specific application requirements. The particulates reinforced composite have best plastic forming ability than that of whisker or fiber counterpart and hence have emerged as most demanding reinforcements with great cost advantage. The particulate reinforced composites have been proved to be most suitable for heat and wear resistance applications. In the present study microstructure, hardness, tensile and impact properties of AA 6061based composite reinforced with Grey Cast Iron (GCI) is analyzed and presented. The presence of Grey Cast Iron resulted in improving the mechanical properties of their respective composites. The micrographs of the composites studied revealed the uniform distribution of the particles in the matrix system. Comparison of the characteristics study before and after heat treatment was done and it was found that there is an improvement in hardness, tensile strength and impact resistance of the composites as well as AA 6061 alloy after heat treatment. Index Terms- particulate, metal matrix composites, stir casting, heat treatment I.
    [Show full text]
  • Review on Friction Stir Processed TIG and Friction Stir Welded Dissimilar Alloy Joints S
    Preprints (www.preprints.org) | NOT PEER-REVIEWED | Posted: 25 October 2019 doi:10.20944/preprints201910.0226.v2 Peer-reviewed version available at Metals 2020, 10, 142; doi:10.3390/met10010142 “Review On Friction Stir Processed TIG And Friction Stir Welded Dissimilar Alloy Joints S. Mabuwa1*, V. Msomi1 1Cape Peninsula University of Technology, Faculty of Engineering and the Built Environment, P.O. Box 1906, Bellville, 7535, South Africa. *Corresponding author: [email protected];27219538778” Abstract “There is an increase towards reducing the weight of structures through the use of aluminium alloys in different industries like aerospace, automotive, etc. This growing interest would lead towards using dissimilar aluminium alloys which would require welding. TIG and friction stir welding are the well- known techniques that are currently suitable for joining dissimilar aluminium alloys. The welding of dissimilar alloys has its own dynamics which impact on the quality of the weld. This then suggests that there should be a process which can be used to improve the dissimilar alloys welds post their production. Friction stir processing is viewed as one of the techniques that could be used to improve the mechanical properties of the material. This paper reports on the status and the advancement of FSW, TIG and FSP technique. It further looks at the variation use of FSP on TIG and FSW welded joints with the purpose of identifying the knowledge gap.” KeyWords: Tensile analysis; Microhardness; Friction stir welding; TIG welding; Friction stir processing; Aluminium alloys; Microstructure. 1 Introduction “Aluminium alloys are known to be good candidates for different applications in various fields like aerospace, food packaging, automotive industries, etc.
    [Show full text]
  • Elevated Temperature Effects on the Mechanical Properties of Age Hardened 6Xxx Series Aluminum Alloy Extrusions
    Elevated Temperature Effects on the Mechanical Properties of Age Hardened 6xxx Series Aluminum Alloy Extrusions A Senior Project Presented to The Faculty of the Materials Engineering Department California State University, San Luis Obispo In Partial Fulfillment of the Requirements for the Degree: Bachelors of Science in Materials Engineering by Rachael Donovan Rose Fortune Robert Trout June 2015 0 Abstract The purpose of this project is to determine if over-aging of aluminum causes the yield or tensile strength to fall below the minimum strength values set by the aluminum industry. Extruded aluminum alloys, 6061-T6, 6063-T6, and two proprietary alloys, HS6X-T6 and RX82-T6, were exposed to reheating treatments at extended times and temperatures. The three temperatures were 350°F, 390°F, and 425°F. The times of reheat increased logarithmically from 30 minutes to 64 hours. The samples were tensile tested to determine the tensile strength and yield strength. Statistical methods helped model the behavior of yield and tensile strength as a function of alloy, time, and interaction of alloy and time for each temperature. This showed which alloy experienced a change in strength and at what time and temperature the strength fell below minimum acceptable values. The strongest to weakest untreated alloys respectively were HS6X, RX82, 6061, and 6063. As time progressed at each temperature, the strongest to weakest alloys changed to HS6X, 6061, RX82, and 6063 respectively. For the 6061 and 6063 alloys, the yield strength did not go below the lower bound value at 350°F, at 390°F it took 16 hours, and for 425°F it took 4 hours.
    [Show full text]
  • MATRIX Al-ALLOYS for SILICON CARBIDE REINFORCED METAL MATRIX COMPOSITES
    IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 INFLUENCE OF VOLUME FRACTION, SIZE, CRACKING, CLUSTERING OF PARTICULATES AND POROSITY ON THE STRENGTH AND STIFFNESS OF 6063/SICP METAL MATRIX COMPOSITES A. Chennakesava Reddy1 1Professor, Department of Mechanical Engineering, JNTUH College of Engineering, Kukatpally, Hyderabad – 500 085, Telangana, India Abstract The objective of this study is to examine the influence of volume fraction, size of particulates, formation of precipitates at the matrix/particle interface, particle cracking, voids/porosity, and clustering of particulates on the strength and stiffness of 6063/SiCp metal matrix composites. Tensile strength and stiffness increase with an increase in the volume fraction of SiC particulates. The tensile strength and stiffness decrease with increase in size of the particulates, presence of porosity, clustering, and particle cracking. Formation of particulate clusters is more prominent in the composites having very small-reinforced particulates. Mg2Si compound is likely to precipitate at the matrix/particle interfaces of 6063/SiC composite. Keywords: 6063, SiC, clustering, cracking, porosity, clustering --------------------------------------------------------------------***------------------------------------------------------------------ 1. INTRODUCTION matrix composite have become of principal importance for the manufacturer to make a quality product as per the Consolidation of a high strength ceramic particulate in a soft designer specifications. The objective of this work is to metal matrix is the technological renovation in the domain study the influence of the volume fraction and particle size of composites for the designer to assure high specific elastic of SiCp, clustering and cracking of particulates, modulus, strength-to-weight ratio, fatigue durability, and voids/porosity, and formation of precipitates at the wear resistance in the fields of aerospace and automotive particle/matrix interface on the tensile strength and stiffness applications.
    [Show full text]
  • Tensile Shear Strength and Dynamic Mechanical Analysis of 6063 Aluminium Alloy and 304 Stainless Steel by Spot Welding S. A
    Tensile shear strength and dynamic mechanical analysis of 6063 aluminium alloy and 304 stainless steel by spot welding S. A. Razak School of Materials Engineering, Universiti Malaysia Perlis, 02600 Arau, Perlis, Malaysia Email: [email protected] Abstract: Mechanical properties of dissimilar metal of spot welding were tested and analyzed based on the variation in welding currents and welding times. From visual observation, the largest weld nugget recorded was 7.43 mm at 5 kA, meanwhile the smallest was 6.4 mm at 3 kA. It was found that weld nugget size increase with the increment of weld current and extension of weld time. Based on tensile result, the largest weld nugget size of 7.43 mm produced the highest tensile strength, 31.99 N/mm2 mean while the smallest weld nugget 6.4 mm produced 29.40 N/mm2. The results show that weld nugget size affect the tensile shear strength, and with the increment of weld current and extension of welding time, tensile shear strength increase. Dynamic mechanical properties defined the storage modulus, loss modulus and damping capacity of dissimilar metal spot welded. It was found that at 10 Hz frequency between 70°C to 350°C, with heating rate of 10°C/minute, the storage modulus increase with increment in weld current and the extension of weld time to 8 s. Meanwhile the loss modulus decrease with the increased of weld current and weld time. Same pattern happen to damping capacity, the value dropped with the increases of welding current and welding time. Keywords: spot welding, dissimilar metal, 6063 aluminium alloy, 304 stainless steel, dynamic mechanical analysis.
    [Show full text]