Relevant bibliographies by topics / Solutionizing

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  1. Journal articles
  2. Dissertations / Theses
  3. Book chapters
  4. Conference papers

Academic literature on the topic 'Solutionizing'

Author: Grafiati
Published: 4 June 2021
Last updated: 12 June 2025

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Journal articles on the topic "Solutionizing"

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Tomaszewska, Agnieszka, Rafał Michalik, and Magdalena Jabłońska. "Influence of Solutionizing Parameters on the Structure and Corrosion Resistance of the ZnAl40Cu3 Alloy." Solid State Phenomena 246 (February 2016): 123–26. http://dx.doi.org/10.4028/www.scientific.net/ssp.246.123.

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The purpose of carried out examination was to determine the effect of solution heat treatment on the structure and corrosion resistance of the ZnAl40Cu3 alloy in the "acid rain" environment. The scope of the test included Brinell hardness tests, structural tests and galvanostatic and potentiodynamic tests. The examination showed that the maximum hardness of the sample after solution heat treatment obtain after 10 h of solutionizing. It has been shown that the solutionizing increases the corrosion resistance. The corrosion resistance was greater, when the longer was the time of solutionizing.
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Rajesh Kannan, P., V. Muthupandi, B. Arivazhagan, and K. Devakumaran. "Microstructure and Mechanical Properties of Heat-treated T92 Martensitic Heat Resistant Steel." High Temperature Materials and Processes 36, no. 8 (2017): 771–78. http://dx.doi.org/10.1515/htmp-2016-0030.

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AbstractT92 samples were solutionized at 1,050 °C, 1,100 °C and 1,150 °C for 20 min and then tempered at 730 °C, 745 °C and 760 °C for 60 min. Optical microscopy studies were carried out to understand the microstructural evolution due to heat treatment. These heat-treated samples comprised of lath martensite microstructure in all the cases. Prior austenite grain size of the heat-treated samples increased with solutionizing temperature. Tensile properties were evaluated using micro-tensile samples. Hardness values of the heat-treated samples were estimated using Vickers hardness tester. Interestingly, for all the given tempering condition, the hardness values showed an increasing trend with solutionizing temperature while their tensile strength values tend to decrease. Fractograph analysis depicted that increasing the solutionizing temperature led to grain boundary decohesion.
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Kulkarni, Rahul Ramesh, Nityanand Prabhu, Peter D. Hodgson та Bhagwati Prasad Kashyap. "Kinetics of γ-Mg17Al12 Phase Dissolution and its Effect on Room Temperature Tensile Properties in As-Cast AZ80 Magnesium Alloy". Solid State Phenomena 209 (листопад 2013): 207–11. http://dx.doi.org/10.4028/www.scientific.net/ssp.209.207.

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As-cast AZ80 magnesium alloy consists of α-Mg, eutectic product of α-Mg and γ-Mg17Al12, with the latter present in the form of partially and fully divorce eutectic. There occurs dissolution of harder γ-Mg17Al12 phase during homogenization treatment at 400 ᵒ and 439 ᵒC. The proportion of the α-Mg and γ-Mg17Al12 phase was varied by solutionizing the alloy for various lengths of time at these temperatures, in order to investigate the kinetics of phase transformation and to evaluate the effect of phase proportion, size and morphology on room temperature tensile properties. It was found that the yield strength decreases with the increase in solutionizing temperature from 400ᵒ to 439 ᵒC and at the same time, ductility in general increases with the increasing solutionizing temperature. The variation in tensile properties and the nature of fractographs were analyzed in terms of the effects of microstructure
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Tang, Yun Yi, Heng Cheng Liao, and Ye Liu. "Precipitation of ScAl3 Phase during Solutionizing and Ageing of Hypoeutectic Al-Sc Alloys and its Impact to Mechanical Properties." Materials Science Forum 877 (November 2016): 581–86. http://dx.doi.org/10.4028/www.scientific.net/msf.877.581.

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In this paper, precipitation of ScAl3 phase during solutionizing and ageing and its impact to mechanical properties of hypoeutectic Al-Sc alloy and effect of Sc addition amount were investigated by TEM and SEM microstructure observation and mechanical property testing. During solutionizing at 640oC for 24h, for Al-0.2wt.%Sc and Al-0.4wt.%Sc alloy, ScAl3 particles formed in the course of solidification become smaller, indicating, as a whole, Sc is partially dissolved into Al solution. Simultaneously, precipitation of two types of ScAl3 particles are observed by TEM. One has a size of 200~300nm, and the other is much small, 5~20nm in size. Though re-dissolution of Sc solute into Al solution and precipitation of large and fine ScAl3 particles occur in the solutionizing course, but the strength and hardness are decreased. The key reason for it is thought to be the softening effect of high level of vacancies in matrix lattice from the high solutionizing temperature. After further aging at 300oC for 3h, a great number of fine ScAl3 particles are precipitated in the Al matrix, which leads to a considerable precipitation hardening effect, thus the strength and hardness are increased obviously. Increasing the Sc content in the alloy results in a considerable rise in as-cast and as-aged strength and hardness, due to the solution strengthening and precipitation hardening respectively.
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Wongbunyakul, Piyanut, Patama Visuttipitukkul, Panyawat Wangyao, Gobboon Lothongkum, and Prasonk Sricharoenchai. "Effect of Reheat Treatment on Microstructural Refurbishment and Hardness of the As-cast Inconel 738." High Temperature Materials and Processes 33, no. 5 (2014): 453–61. http://dx.doi.org/10.1515/htmp-2013-0065.

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AbstractThis work investigates the effect of rejuvenation heat treatment conditions for refurbishment of the long-term serviced gas turbine blades, which were made of as-cast nickel base superalloy grade, Inconel 738. The reheat treatment conditions consist of solutionizing treatments at temperatures of 1,438, 1,458 and 1,478 K for 14.4 ks and aging treatments at temperatures of 1,133, 1,148 and 1,163 K for 43.2, 86.4, 129.6 and 172.8 ks. The results show that increase in aging times results in continuous increase of size and area fraction of gamma prime (γ′) particles. The higher solutionizing temperature leads to the lower area fraction and smaller size of gamma prime particles. Regarding the microstructure characteristics, the most proper reheat treatment condition should be solutionizing at temperature of 1,438 K for 14.4 ks and aging at temperature of 1,133 K for 172.8 ks, which provides the highest area fraction of gamma prime particles in proper size.
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Khorshidi, R., A. Honarbakhsh Raouf, M. Emamy, and H. R. Jafari Nodooshan. "The Evolution of Heat Treatment on the Tensile Properties of Na-Modified Al-Mg2Si In Situ Composite." Advanced Materials Research 311-313 (August 2011): 283–86. http://dx.doi.org/10.4028/www.scientific.net/amr.311-313.283.

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The effect of different solution temperatures has been investigated on the tensile properties of Na-modified Al-Mg2Si in situ composite specimens which were subjected to solutionizing at different temperatures of 480 °C, 500 °C and 520 °C for holding time of 4 h followed by quenching. Tensile test results indicated that elongation value gradually increases upon solution treatment whereas ultimate tensile strength (UTS) reduces. The results of solution treatment also showed that the highest quality index is achieved in 500 °C (354 MPa) and so it is revealed optimum solutionizing temperature level (500 °C) for improving tensile properties.
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Apelian, D., and S. K. Chaudhury. "Fluidized bed heat treatment of aluminum cast components." Journal de Physique IV 120 (December 2004): 555–62. http://dx.doi.org/10.1051/jp4:2004120064.

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Heat Treatment and post casting treatments of cast components has always been an important step in the control of microstructure, and resultant properties. In the past, the solutionizing, quenching and ageing process steps may have “required” in total over 20 hours of processing time. With the advent of fluidized bed reactors (FB), processing time has been dramatically reduced. For example, instead of 8-10 hours solutionizing time in a conventional furnace, the time required in FB is less than an hour. Experiments with Al-Si-Mg alloy, (both modified with Sr, and unmodified) were performed, having different diffusion distances (different DAS), and for different reaction times and temperatures. Both the model and the experimental results are presented and discussed.
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OHNISHI, Nobuaki, Tetsuya TAKAAI, Yoshihiro NAKAYAMA, and Masahiro OHMORI. "High temperature solutionizing of AC4CH aluminum casting alloy." Journal of Japan Institute of Light Metals 45, no. 8 (1995): 447–52. http://dx.doi.org/10.2464/jilm.45.447.

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Kakazey, Mykola, Marina Vlasova, Pedro Antonio Márquez Aguilar, Olexandr Bykov, Volodymyr Stetsenko, and Andriy Ragulya. "Laser Surface Solutionizing and Crystallization of Al2O3-Cr2O3." International Journal of Applied Ceramic Technology 6, no. 2 (2009): 335–43. http://dx.doi.org/10.1111/j.1744-7402.2008.02280.x.

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MANICKAM, Dhanashekar, and Senthil Kumar VELUKKUDI SANTHANAM. "Effect of Solution Heat Treatment and Artificial Aging on Compression Behaviour of A356 Alloy." Materials Science 25, no. 3 (2019): 281–85. http://dx.doi.org/10.5755/j01.ms.25.3.20442.

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Aluminium alloys are subjected to heat treatment to increase the strength and corrosion properties. This paper aims to study the effect of heat treatment on the compression behaviour of A356 alloy under quasi static condition and barreling effect. The various heat treatments are: (i) solution heat treatment of 1 h at 540 °C + natural aging 0 h + artificial aging at 180 °C up to 5.5 h, (ii) solution heat treatment of 3 h at 540 °C + natural aging for 20 h + artificial aging at 180 °C up to 5.5 h, and (iii) solution heat treatment of 6 h at 540 °C + natural aging for 20 h + artificial aging at 180 °C up to 5.5 h. Specially to understand the influence of artificial aging at every 0.5 h up to 5.5 h, the specimens were heat treated. From the results, solutionizing for 1 hr have a better compression strength irrespective of the artificial aging. Natural aging had decreased the ductility but increased the strength property. Artificial aging had a significant effect on the compressive strength and peak strength were obtained at 4 h irrespective of solutionizing heat treatment. Compressive strength increased by 33 % for 1 h of solutionizing and 4 h of artificial aged specimen when compared to non-heat treated alloy. Two mathematical relations discussed in literature were used for calculating the radius of the barreled surface followed by validation. DOI: http://dx.doi.org/10.5755/j01.ms.25.3.20442
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Dissertations / Theses on the topic "Solutionizing"

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Kulpinski, Kyle E. "The Effect of Solutionizing Heat Up Rate and Quench Rate on the Grain Size and Fracture Mode of a 6061 Alloy Pressure Vessel." Case Western Reserve University School of Graduate Studies / OhioLINK, 2012. http://rave.ohiolink.edu/etdc/view?acc_num=case1334239996.

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Gowreesan, Vamadevan. "Rapid Infrared Thermal Processing of AA 2618 and AA 6061 Forgings." Ohio University / OhioLINK, 2008. http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1225849023.

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Goel, Sneha. "Post-treatment of Alloy 718 produced by electron beam melting." Licentiate thesis, Högskolan Väst, Avdelningen för avverkande och additativa tillverkningsprocesser (AAT), 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:hv:diva-13547.

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Electron beam melting (EBM), a metal additive manufacturing (AM) process, has received considerable industrial attention for near net shape manufacture of complex geometries with traditionally difficult-to-machine materials. This has fuelled considerable academic interest in investigating EBM of Alloy 718, a nickel ironbased superalloy possessing an exciting combination of good mechanical behaviour and cost effectiveness. EBM production of Alloy 718 is particularly promising for aerospace and other sectors which value rapid production of components with large scope for design flexibility. The EBM builds are characterized by presence of inevitable defects and, anisotropy within a build is also a concern. Consequently, as-built Alloy 718 has to be subjected to post-build thermal-treatments (post-treatments) to ensure that the parts eventually meet the critical service requirements. Not withstanding the above, limited knowledge is available about optimal post-treatments for EBM-built Alloy 718. Therefore, the main focus of the work presented in this thesis was to systematically investigate the response of EBM-built material to post-treatments, which include hotisostatic pressing (HIPing), solution treatment (ST), and aging. HIPing of EBM-built Alloy 718 led to more than an order of magnitude reduction in defect content, which was reduced from as high as 17% to &lt; 0.2% in samples built with intentionally introduced porosity to investigate limits of defect closure achievable through HIPing. In addition, HIPing also caused complete dissolution of δ and γ" phases present in the as-built condition, with the latter causing dropin hardness of the material. HIPing had no effect on the carbides and inclusions such as TiN, Al2O3 present in the built material. The evolution of microstructure during ST and aging was systematically investigated. Growth of potentially beneficial grain boundary δ phase precipitates was found to cease after a certain duration of ST, with samples subjected to prior-HIPing exhibiting lesser precipitation of the δ phase during ST. While the specimen hardness increased onaging, it was observed to plateau after a duration significantly shorted than the specified ASTM 'standard' aging cycle. Therefore, prima facie there are promising prospects for shortening the overall heat treatment duration. A combination of HIPing, ST, and aging treatments in a single uninterrupted cycle was also explored. Future work involving incorporation of a shortened heat treatment schedule in a combined cycle can have significant industrial implications.<br><p>Articles submitted to journals and unpublished manuscripts are not included in this registration</p>
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Book chapters on the topic "Solutionizing"

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Gouma, P. I., J. E. Kertz, and R. G. Buchheit. "Localized Corrosion Mechanisms of Al-Li-Cu Alloy AF/C458 after Interrupted Quenching from Solutionizing Temperatures." In Lightweight Alloys for Aerospace Application. John Wiley & Sons, Inc., 2013. http://dx.doi.org/10.1002/9781118787922.ch11.

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Varma, S. K. "Effect of Solutionizing Time on Age Hardening Characteristics and Corrosive Wear Behavior of Age Hardenable Al Alloy Composites." In Advanced Light Alloys and Composites. Springer Netherlands, 1998. http://dx.doi.org/10.1007/978-94-015-9068-6_2.

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Quan, G., L. Ren, and M. Zhou. "2.13 Solutionizing and Age Hardening of Aluminum Alloys." In Comprehensive Materials Finishing. Elsevier, 2017. http://dx.doi.org/10.1016/b978-0-12-803581-8.09195-5.

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Simencio Otero, Rosa L., Patricia M. Kavalco, Lauralice C. F. Canale, George E. Totten, and Lemmy Meekisho. "Quench Factor Analysis." In Encyclopedia of Aluminum and Its Alloys. CRC Press, 2019. http://dx.doi.org/10.1201/9781351045636-140000233.

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One of the steps of the heat treatment process of age-hardenable aluminum alloys is the quenching process in which the alloy is cooled from the solutionizing temperature. The objective is to quench sufficiently fast to avoid undesirable concentration of alloying elements in the defect and grain boundary structure while at the same time not quenching faster than necessary to minimize residual stresses, which may lead to excessive distortion, or cracking. Various studies have been conducted to predict the relative quench rate sensitivity to yield different properties for age-hardenable alloys. Of these different predictive methods, the one that showed the more realistic results is quench factor analysis (QFA) since it involves a correlation of the cooling curve (time–temperature curve) of the cooling process throughout the quenching cycle for the desired cross-section size of interest with a C-curve (Time–Temperature–Property Curve) for the specific alloy of interest. The QFA numerical procedure has evolved since its original introduction. A review of the basic assumptions of the classical QFA model will be provided here, which will include discussion of the various improvements to the classical model that have been proposed over the intervening years since its introduction.
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Conference papers on the topic "Solutionizing"

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Kumari, Geeta, Carl Boehlert, S. Sankaran, and M. Sundararaman. "The Effects of Solutionizing and Aging temperature on the Microstructure of Allvac 718plus." In HT2019. ASM International, 2019. http://dx.doi.org/10.31399/asm.cp.ht2019p0096.

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Abstract A study on the microstructural evolution of a Ni-based superalloy, Allvac 718Plus, in the forged condition, was performed by varying the solutionizing temperature. Different solutionizing temperatures were chosen to obtain different fractions of the gamma prime (Ni3(Al,Ti,Nb), γ’) and delta (Ni3Nb, δ) phase precipitates. The solutionizing temperatures ranged between 945°C to 1100°C. After solutionizing, the samples were subjected to a standard two-step aging treatment (788°C for 8h followed by 704°C for 8h). The 954°C solutionizing treatment resulted in incomplete dissolution of the γ’ phase and a relatively high volume fraction of the δ phase, which formed preferentially at grain boundaries. The γ’ phase was completely dissolved during each of the other three solutionizing treatments (1000°C, 1050°C, and 1100°C), while the fraction of the δ phase decreased with increasing solutionizing temperature. The 1100°C solutionizing treatment led to significant growth of the matrix grains (Ni (FCC), γ).
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Velukkudi Santhanam, Senthil Kumar, and Dhanashekar Manickam. "Effect of Artificial Aging on Mechanical Properties and Corrosion Behaviour of A356 Alloy." In ASME 2017 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2017. http://dx.doi.org/10.1115/imece2017-72562.

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Aluminium alloys used in automobile applications are generally heat treated to obtain a desired combination of strength and ductility. The knowledge in treatment temperature as well as the time of this process is essential for optimum results. In this paper A356 alloy is subjected to different heat treatment conditions and examined its effects on the mechanical properties and corrosion behaviour. The solutionizing temperature and time were 540°C and 1 hour respectively, followed by 24 hours of natural aging and the artificial aging temperature and time were 180°C and 0.5, 1, 1.5, 2, 2.5, 3, 3.5, 4, 4.5, 5, 5.5, 6 hours respectively. The standard T6 heat treatment process performed were used as reference in-order to compare the effect of artificial ageing. The solutionizing temperature for 1 hour and artificial ageing time of 4.5 hours produced peak compressive strength when compared to other aging times.
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Hegde, S. R., R. M. Kearsey, and J. Beddoes. "Design of Solutionizing Heat Treatments for an Experimental Single Crystal Superalloys." In Superalloys. TMS, 2008. http://dx.doi.org/10.7449/2008/superalloys_2008_301_310.

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Arhami, M., F. Sarioglu, and A. Kalkanli. "Effect of Heat-Treatment and Reinforcement With Silicon Carbide on the Microstructure and Mechanical Properties of AlFeVSi Alloy." In ASME 2007 International Mechanical Engineering Congress and Exposition. ASMEDC, 2007. http://dx.doi.org/10.1115/imece2007-42073.

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The aging response of Al-Fe-V-Si composite was compared with the un-reinforced alloy. The effects of solutionizing time, alloying element and SiC reinforcement on the age hardening response, microstructure and mechanical properties of these alloy and its composites was also investigated. The study was performed by T6 heat treatment at three different solutionizing times. Room temperature tensile testing was conducted for peak aged specimens to determine the effect of this heat treatment on the strength of squeezed cast un-reinforced and reinforced Al-Fe-V-Si alloy with SiC particles. The presence of SiC particles accelerated the aging kinetics of the composites compared to the unreinforced alloys. The time to reach peak age hardness was decreased by addition of SiCp. Mainly two different Fe-intermetallics; small α-Al7(Fe, V)3Si and large β-Al18Fe11Si phases were present in the system studied. The fracture surfaces of composites revealed decohesion of SiC particles from the matrix and cracking of needle like-β intermetallics was observed.
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Hirose, Akio, and Kojiro F. Kobayashi. "Laser surface solutionizing of inconel 718: Improvement of resistance to hydrogen embrittlement." In ICALEO® ‘98: Proceedings of the Laser Materials Processing Conference. Laser Institute of America, 1998. http://dx.doi.org/10.2351/1.5059129.

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Jan, James, and D. Scott MacKenzie. "On the Development of Parametrical Water Quenching Heat Transfer Model Using Quenchometer and Its Validation for All Boiling Regimes." In HT2019. ASM International, 2019. http://dx.doi.org/10.31399/asm.cp.ht2019p0279.

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Abstract In the water quenching process of Aluminum 319, temperature drops rapidly from solutionizing temperatures, around 500°C, to water pool temperature. In this temperature range, the quenching process goes through three boiling regimes: film boiling, transition boiling, and nucleate boiling, before reducing to convection heat transfer. Each boiling regime has unique heat transfer characteristics governed by different physics. A common method to analyze the heat transfer rate in liquid quenching is the cooling curve analysis by quenchometer. Among several methodologies to characterize heat transfer rate, we have found successes in adapting a heat transfer framework based on Leidenfrost point (LFP), minimum heat flux (MHF), and critical heat flux (CHF) to develop a CFD model for quenching process simulation. The CFD model then can be used to calculate temperature histories as well as temperature profiles and the simulation results can be sent to FEA to predict thermal residual stress and distortion. Although the LFP, MHF, and CHF framework has been proven useful for the numerical simulation of water quenching process, these parameters are not constant and they have to be calibrated through experiments for each quenching condition. The objective of this paper is to parameterize the boiling model by quenching conditions such as water pool temperature. Then the predictive model is validated by experimental data obtained by quenchometers.
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