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    Transient liquid phase bonding of FSX-414 superalloy at the standard heat treatment condition

    , Article Materials Characterization ; Volume 66 , 2012 , Pages 38-45 ; 10445803 (ISSN) Bakhtiari, R ; Ekrami, A ; Sharif University of Technology
    2012
    Abstract
    The as-cast samples of FSX-414 Co-based superalloy were heat treated at the standard solution and aging heat treatment cycles. Specimens for joining were cut from the as-cast ingot. Transient liquid phase (TLP) bonding was carried out at the standard solution cycle, using MBF-30 interlayer. Also, bonded specimens were homogenized at the standard aging condition. The microstructure of the as-cast, heat treated and TLP bonded specimens were studied. These studies showed that the non-uniform distributed carbides of the as-cast specimen were replaced by uniform ones during the heat treatment. Eutectic M 23C 6 carbides were observed in all specimens. Due to the complete isothermal solidification,... 

    An investigation on the precipitation hardening of an ultrafine grained Al6063-Al2O3 nanocomposite

    , Article Proceedings of the International Euro Powder Metallurgy Congress and Exhibition, Euro PM 2012 ; Volume 1 , 2012 ; 9781899072361 (ISBN) Asgharzadeh, H ; Bayazid, M ; Simchi, A ; Sharif University of Technology
    2012
    Abstract
    In this work, age hardening behavior of an ultrafine-grained (UFG) Al6063-0.8 vol.% Al2O3 nanocomposite produced via reactive mechanical alloying followed by hot extrusion method by means of T6 heat treatment was studied. The temperature and time of solutionizing and aging were optimized by the Taguchi method. The optimal heat treatment condition was found to be solutionizing at 510 °C for 1.5 h and aging at 170 °C for 8 h. The signal-to-noise (S/N) ratio and analysis of variance (ANOVA) revealed that the solutionizing temperature was the most significant factor. A novel cyclic solution treatment was developed for age hardening of Al6063-Al2O3 nanocomposite. The results showed a considerable... 

    Microstructural changes of FSX-414 superalloy during TLP bonding

    , Article Defect and Diffusion Forum ; Volume 312-315 , 2011 , Pages 399-404 ; 10120386 (ISSN) ; 9783037851173 (ISBN) Bakhtiari, R ; Ekrami, A ; Sharif University of Technology
    Abstract
    The as-cast FSX-414 Co-based superalloy samples were solution treated at 1150°C for 4h and then aged at 980°C for 4h. Specimens for joining were cut from the as-cast ingot and TLP bonding carried out at the same conditions as for the solution and solution+aging treatment, using MBF-30 interlayer. Microstructures were studied for as-cast, heat treated and TLP bonded specimens. These studies showed that the ununiform distributed carbides of MC type in the as-cast specimens replaced by M23C6 type carbides with uniform distribution in the heat treated microstructure. Due to complete isothermal solidification, no eutectic structure in the bond region were wasobserved, but some intermetallics in... 

    Aging behavior of a 2024 Al alloy-SiCp composite

    , Article Materials and Design ; Volume 31, Issue 5 , May , 2010 , Pages 2368-2374 ; 02641275 (ISSN) Mousavi Abarghouie, S. M. R ; Seyed Reihani, S.M ; Sharif University of Technology
    2010
    Abstract
    In the present research work the 2024 aluminum alloy was reinforced with SiC particles via powder metallurgy method. The effect of heat treatment conditions on artificial aging kinetics was investigated. The solution treatment of the composite sample and the unreinforced alloy was carried out at 495 °C for 1, 2 and 3 h followed by aging at 191 °C for various aging times between 1 and 10 h. The existence of SiC particles led to increasing the peak hardness of the alloy. The peak hardness of the composite sample took place at shorter times than that of the unreinforced alloy for the samples solution treated for 2 and 3 h, but took place at longer times for the samples solution treated for 1 h.... 

    Effect of predeformation and heat treatment conditions in the SIMA process on microstructural and mechanical properties of A319 aluminum alloy

    , Article Journal of Alloys and Compounds ; Volume 468, Issue 1-2 , 2009 , Pages 130-135 ; 09258388 (ISSN) Arami, H ; Khalifehzadeh, R ; Keyvan, H ; Khomamizadeh, F ; Sharif University of Technology
    2009
    Abstract
    In this study the influences of predeformation and heat treatment conditions on stress-induced melt activating process (SIMA) of A319 aluminum alloy were investigated. At 30% of predeformation a dominant globular structure of grains was obtained. However, further increasing of the predeformation rate considerably reduced the shape factor. The holding time of 10-15 min at semi-solid temperature of 580 °C was suggested in order to prevent grain growth. Coarsening of the grains by excess time or temperature of heat treatment reduced the tensile strength of the alloy. © 2008 Elsevier B.V. All rights reserved  

    Low temperature nanostructured zinc titanate by an aqueous particulate sol-gel route: Optimisation of heat treatment condition based on Zn:Ti molar ratio

    , Article Journal of the European Ceramic Society ; Volume 30, Issue 4 , 2010 , Pages 947-961 ; 09552219 (ISSN) Mohammadi, M. R ; Fray, D. J ; Sharif University of Technology
    2010
    Abstract
    Nanocrystalline zinc titanate (ZnTiO3) thin films and powders with purity of 94% were produced at the low sintering temperature of 500 °C and the short sintering time of 1 h by a straightforward aqueous particulate sol-gel route. The effect of Zn:Ti molar ratio was studied on the crystallisation behaviour of zinc titanates. The prepared sols showed a narrow particle size distribution in the range 17-19 nm. X-ray diffraction (XRD) and Fourier transform infrared spectroscopy (FTIR) revealed that the powders contained mixtures of the rhombohedral-ZnTiO3, cubic-ZnO, cubic-Zn2TiO4 phases, as well as the anatase-TiO2 and the rutile-TiO2 depending on the sintering temperature and Zn:Ti molar ratio....