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Relevant bibliographies by topics / Pure Aluminum

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Academic literature on the topic 'Pure Aluminum'

Author: Grafiati

Published: 4 June 2021

Last updated: 10 February 2022

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Journal articles on the topic "Pure Aluminum"

1

Wongpreedee, Kageeporn, Panphot Ruethaitananon, and Tawinun Isariyamateekun. "Interface Layers of Ag-Al Fusing Metals by Casting Processes." Advanced Materials Research 787 (September 2013): 341–45. http://dx.doi.org/10.4028/www.scientific.net/amr.787.341.

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The materials of fusing metals commercially used in the jewelry niche marketing is seen as precious metals. An innovation of fusing metals searched for new materials to differentiate from the markets for mass production. In this research, it studied the bonding processes of silver and aluminium metals by casting processes for mass productions. The studies had been varied parameters on the types of aluminium and process temperature controls. This research had used two types of aluminium which were pure aluminium 99.99% and aluminum 5083 alloys bonding with pure silver 99.99%. The temperatures had been specified for two factors including casting temperature at X1, X2 and flasking temperature at Y1, Y2. From the results, it was found that the casting temperature at 730°C and the flasking temperature at 230 °C of pure silver-aluminum 5083 alloys bonding had the thinnest average thickness of interface at 427.29 μm. The microstructure of pure silver-aluminum 5083 alloy bonding was revealed eutectic-like structures at the interfaces. The EDS analysis showed the results of compounds at interface layers of Ag sides giving Ag2Al intermetallics on pure silver-aluminum 5083 alloy bonding unlike pure silver-pure aluminium bonding giving Ag3Al intermetallics.

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Ichikawa, Junichi, Tatsuro Hayashida, and Shinsuke Suzuki. "Compressive Properties of Porous Aluminum Alloy Fabricated by Joining Pipes and Melt through Continuous Casting." Materials Science Forum 761 (July 2013): 151–55. http://dx.doi.org/10.4028/www.scientific.net/msf.761.151.

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A porous aluminum alloy was fabricated by joining pure aluminum pipes and Al-13mass% Si melt through continuous casting. Compressive tests were carried out with test specimens of the porous aluminum alloy fabricated by this method, non-porous aluminum alloy fabricated by continuous casting using Al-Si melt, and porous aluminum alloy consisting of only Al-Si fabricated by drilling non-porous Al-Si bar. From the compressive tests, it was confirmed that specific proof strength of the porous aluminum alloy fabricated by joining pipes and melt can be described by rule of mixture of Al-Si base metal, pure aluminium pipes and pores.

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Ilyin, Alexander P., Liudmila O. Root, and Andrei V. Mostovshchikov. "Application of Aluminum Nanopowder for Pure Hydrogen Production." Key Engineering Materials 712 (September 2016): 261–66. http://dx.doi.org/10.4028/www.scientific.net/kem.712.261.

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The problems of hydrogen energetic as well as a method of high pure hydrogen obtaining are presented in the paper. It was suggested to use the reaction of aluminium nanopowder with water, as the reaction proceeds with high rate even at ambient conditions (the rate of hydrogen emission reached 18 ml/(s∙g)) and high degree of conversion (up to 100 %). The unreasonableness of the replacement of aluminium nanopowder to coarse-grained powder in this reaction due to the low efficiency is shown in the article. As a solution for pure hydrogen obtaining, a phenomenon of self-heating of aluminum nanoparticles and the resulting hydrogen, as well as the effect of its high-temperature diffusion through the membrane of ultrahigh molecular weight polyethylene were used.

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Jorcin, Jean-Baptiste, Christine Blanc, Nadine Pébère, Bernard Tribollet, and Vincent Vivier. "Galvanic Coupling Between Pure Copper and Pure Aluminum." Journal of The Electrochemical Society 155, no. 1 (2008): C46. http://dx.doi.org/10.1149/1.2803506.

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Wang, Hai Chuan, Dan Liu, Zhi You Liao, Ming Li, Jie Lie, Gui Wang, and Matthew S. Dargusch. "Effect of Ultrasonic Power on the Microstructure and Hardness of Commercially Pure Aluminum." Advanced Materials Research 194-196 (February 2011): 1192–96. http://dx.doi.org/10.4028/www.scientific.net/amr.194-196.1192.

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Molten, commercially pure aluminum has been treated ultrasonically with differing input power. The results show that the ultrasonic power can significantly refine the microstructure of the aluminium and increase the hardness of the samples. A mathematical model developed in this paper can predict the effect of the ultrasonic power on the grain size of the pure aluminium well.

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6

OHNISHI, Tadakazu. "Hydrogen in pure aluminum and in aluminum alloys." Journal of Japan Institute of Light Metals 39, no. 3 (1989): 235–51. http://dx.doi.org/10.2464/jilm.39.235.

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TANAKA, Takakazu. "Impurities in commercial pure aluminum." Journal of Japan Institute of Light Metals 36, no. 5 (1986): 253–54. http://dx.doi.org/10.2464/jilm.36.253.

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8

Kucharčík, L., M. Brůna, and A. Sládek. "Influence of Chemical Composition on Porosity in Aluminium Alloys." Archives of Foundry Engineering 14, no. 2 (June 1, 2014): 5–8. http://dx.doi.org/10.2478/afe-2014-0026.

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Abstract Porosity is one of the major defects in aluminum castings, which results is a decrease of a mechanical properties. Porosity in aluminum alloys is caused by solidification shrinkage and gas segregation. The final amount of porosity in aluminium castings is mostly influenced by several factors, as amount of hydrogen in molten aluminium alloy, cooling rate, melt temperature, mold material, or solidification interval. This article deals with effect of chemical composition on porosity in Al-Si aluminum alloys. For experiment was used Pure aluminum and four alloys: AlSi6Cu4, AlSi7Mg0, 3, AlSi9Cu1, AlSi10MgCu1.

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Millogo, Myriam, Stéphane Bernard, and Philippe Gillard. "Combustion characteristics of pure aluminum and aluminum alloys powders." Journal of Loss Prevention in the Process Industries 68 (November 2020): 104270. http://dx.doi.org/10.1016/j.jlp.2020.104270.

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Bainbridge, Ian Frank, and John Andrew Taylor. "The Surface Tension of Pure Aluminum and Aluminum Alloys." Metallurgical and Materials Transactions A 44, no. 8 (March 16, 2013): 3901–9. http://dx.doi.org/10.1007/s11661-013-1696-9.

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Dissertations / Theses on the topic "Pure Aluminum"

1

Zou, Yu. "Microstructural studies of cold sprayed pure nickel, copper and aluminum coatings." Thesis, McGill University, 2010. http://digitool.Library.McGill.CA:8881/R/?func=dbin-jump-full&object_id=92381.

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Leblanc, Robert Samuel. "Influence of Nozzle Material and Spray Parameters on Pure Aluminum and Aluminum 7075 coatings using Cold Gas Dynamic Spray." Thesis, Université d'Ottawa / University of Ottawa, 2016. http://hdl.handle.net/10393/34202.

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Commercial airplanes are still using aluminum alloys as their primary structural material. Even if the used carbon fiber reinforced polymers is becoming more popular due to their extremely high strength to weight ratio, the majority of the existing flying fleet is still made out of aluminum alloys. This material was primarily used due to its high strength to weight ratio, ease to machine, excellent corrosion resistance properties and its high crash energy absorption. Aircraft components made of aluminum alloys are subjected to high stresses and harsh environments during flight, potentially leading them to crack and/or corrode. Presently, there is no industrial approved method to repair these components. Recycling damaged aircraft parts by repairing them would result in large cost savings for the industry. The present study was motivated by the potential use of the cold gas dynamic spray (CGDS) process to repair damaged aluminum 7075-T6 aircraft components. Two feedstock materials were used to repair this alloy in this research: pure aluminum and aluminum 7075. Pure aluminum is used in the aircraft industry on non-bearing components due to its extremely high corrosion resistance properties. Aluminum 7075 is the material of choice for structural applications due to its high strength. The results of this study show that CGDS could be potentially used to repair aluminum components on aircrafts. However, this research demonstrated that new commercially available equipments need to be further developed to successfully produce repaired components that meet the industry standards.

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Mjali, Kadephi Vuyolwethu. "Laser bending of commercially pure grade 2 titanium alloy plates: mechanisms analysis and characterisation of mechanical properties." Thesis, Nelson Mandela Metropolitan University, 2014. http://hdl.handle.net/10948/d1021147.

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The processing of materials has become a specialist field and the industry will continue to grow due to rising costs in labour and raw materials which has forced many automotive industry suppliers to invest heavily in this field. In order to be relevant and competitive in today’s industrial world, companies in South Africa are now forced to dedicate billions of rands in profits to research and development. Metals like titanium are finding favour with automotive and aviation companies in pursuit of savings in fuel consumption. This saving is achieved by reducing weight on aircraft and automobiles yet still meeting acceptable and improved structural integrity. In-depth research into the behaviour of various materials under varying loading conditions is therefore essential. The study on the processing of commercially pure grade 2 titanium alloy plates focuses on the development of process parameters for bending the material using a 4kW Nd: YAG laser to an approximate radius of curvature of 120mm. The resulting mechanical properties of laser formed plates are then compared to those obtained from mechanically formed samples. The titanium parent material was used to benchmark the performance of formed samples. The effect of process parameters on the mechanical properties and structural integrity also formed part of this study. To obtain the bending parameters for laser forming, various combinations of processing speeds and laser powers were used. The line energy is dependent on the power and scanning velocity parameters and these are shown in table 1. The laser power, line energy and scanning velocity were the main parameters controlled in this study and the beam diameter remained unchanged. Residual stress analysis, micro-hardness and fatigue life testing were carried out to analyse mechanical properties and the structural integrity of the plate samples. Microstructural analysis was also done to observe changes in the material as a result of the forming processes. From the results it is evident that laser forming is beneficial to the hardness of titanium but detrimental to the fatigue life at higher line energies. Residual stress analysis showed the amount of stress within the study samples increased with each forming operation. This information was vital in the analysis of the fatigue life of titanium. A fatigue life prediction model was developed from this study and it shed some light on the behaviour of titanium in fatigue testing. The model could be used to predict fatigue life when no fatigue data is available for commercially pure grade 2 titanium alloy plates. In conclusion, this study helped establish parameters that could be used to bend titanium while the analysis of mechanical properties showed the limits of working with this alloy.

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Mjali, Kadephi Vuyolwethu. "Mechanisms, analysis and characterisation of mechanical properties of laser formed commercially pure grade 2 titanium alloy plates." Thesis, Nelson Mandela Metropolitan University, 2014. http://hdl.handle.net/10948/d1021083.

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The processing of materials has become a specialist field and the industry will continue to grow due to rising costs in labour and raw materials which has forced many automotive industry suppliers to invest heavily in this field. In order to be relevant and competitive in today’s industrial world, companies in South Africa are now forced to dedicate billions of rands in profits to research and development. Metals like titanium are finding favour with automotive and aviation companies in pursuit of savings in fuel consumption. This saving is achieved by reducing weight on aircraft and automobiles yet still meeting acceptable and improved structural integrity. In-depth research into the behaviour of various materials under varying loading conditions is therefore essential. The study on the processing of commercially pure grade 2 titanium alloy plates focuses on the development of process parameters for bending the material using a 4kW Nd: YAG laser to an approximate radius of curvature of 120mm. The resulting mechanical properties of laser formed plates are then compared to those obtained from mechanically formed samples. The titanium parent material was used to benchmark the performance of formed samples. The effect of process parameters on the mechanical properties and structural integrity also formed part of this study. To obtain the bending parameters for laser forming, various combinations of processing speeds and laser powers were used. The line energy is dependent on the power and scanning velocity parameters and these are shown in table 1. The laser power, line energy and scanning velocity were the main parameters controlled in this study and the beam diameter remained unchanged. Residual stress analysis, micro-hardness and fatigue life testing were carried out to analyse mechanical properties and the structural integrity of the plate samples. Microstructural analysis was also done to observe changes in the material as a result of the forming processes. From the results it is evident that laser forming is beneficial to the hardness of titanium but detrimental to the fatigue life at higher line energies. Residual stress analysis showed the amount of stress within the study samples increased with each forming operation. This information was vital in the analysis of the fatigue life of titanium. A fatigue life prediction model was developed from this study and it shed some light on the behaviour of titanium in fatigue testing. The model could be used to predict fatigue life when no fatigue data is available for commercially pure grade 2 titanium alloy plates. In conclusion, this study helped establish parameters that could be used to bend titanium while the analysis of mechanical properties showed the limits of working with this alloy.

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5

Krishnakumar, Rengan. "Passivation behavior of pure aluminum and sputtered non- equilibrium Al-Cr and Al-Ta alloy films /." The Ohio State University, 1993. http://rave.ohiolink.edu/etdc/view?acc_num=osu1487843688958645.

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6

Terhune, Shannon Derek. "An electron backscatter diffraction analysis of the microstructure of pure aluminum processed by equal-channel angular pressing." Thesis, Monterey, California. Naval Postgraduate School, 1998. http://hdl.handle.net/10945/8304.

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Equal-channel angular (ECA) pressing is a promising method to achieve refinement of grain size to 1.0 micrometer or less for aluminum and its alloys. Computer-aided electron backscatter diffraction (EBSD) analysis of high purity aluminum (99.99%) which had been subjected to one pass, four passes, and twelve passes through an ECA die was performed. Grain and subgrain size and boundary misorientation distributions during such large-strain deformation processing were of particular interest. A texture was present after one pressing and the boundary misorientation distribution had a peak at 5 deg - 10 deg although boundaries were present in all misorientation ranges. Fine equaixed grains were achieved after twelve passes through the ECA die, accompanied by random orientation and misorientation distributions

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7

Dunn, Darrell Scott. "Characterization and evaluation of anodized commercially pure titanium and titanium-aluminum-vanadium alloy surfaces for systemic antibiotic release." Thesis, The University of Arizona, 1990. http://hdl.handle.net/10150/144641.

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Postoperative infections are one of the most feared complications following orthopedic implant procedures. Bacterial infections occur in approximately 1-2% of the patients who undergo orthopedic implant surgery. Treatment of these infections is typically done by administering antibiotics either locally or systemically. Systemic release of antibiotics from bone cement has been reasonably successful. However, it would also be desirable to develop a method of antibiotic release from porous coated implants designed for osseointegration. The principal objective of this research was to explore the feasibility of using anodizing (electrochemical oxidation) as a surface modification technique to facilitate the attachment of antibiotics to commercially pure titanium (CP Ti) and Ti-6Al-4V orthopedic implant materials. In particular the effect of anodizing conditions on the characteristics of the oxide coating such as thickness, composition and porosity has been investigated. Using microbiological methods, the efficacy of in-vitro attachment of antibiotics to anodized surfaces was determined.

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Xenikos, Dimitrios George. "Statics and dynamics of the mixed state in pure and aluminum-doped yttrium barium copper oxide high-temperature superconductors /." The Ohio State University, 1994. http://rave.ohiolink.edu/etdc/view?acc_num=osu1487856076412837.

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Nastic, Aleksandra. "Repair of Aluminum Alloy Aerospace Components and Cold Gas Dynamic Spray Flow Distribution Study." Thesis, Université d'Ottawa / University of Ottawa, 2015. http://hdl.handle.net/10393/32998.

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Aluminum alloys have been used for decades in aircraft as they offer a wide range of properties explicitly developed to provide a set of characteristics adapted to structural and non-structural components. However, aircraft components inevitably undergo degradation during service due to their extensive use and exposure to harsh environments. Typical repair methods are either not efficient for large scale repairs due to their low material growth rate, not suitable for field repair or involve the use of high process temperatures. The present research aims at evaluating the cold gas dynamic spray (CGDS) as a potential repair technology to restore Al7075-T6 nose landing gear steering actuator threads found on the Boeing 757 aircraft. Moreover, it studies the suitability of using cold spray to deposit Al2024 material. The influence of process parameters and substrate surface preparation on the material deposition efficiency and resulting microstructural and mechanical repair properties is also evaluated.

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Swaroop, N. R. Sathya. "Processing And High Temperature Deformation Of Pure And Magnesia Doped Alumina." Thesis, Indian Institute of Science, 2000. http://hdl.handle.net/2005/180.

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Creep resistance is an important design criterion at high temperatures especially when continuous attempts are made to increase the efficiencies by increasing the operating temperatures. Alumina is an important high temperature material and in addition to that it is used in wide variety of applications such as substrates for electronic packaging, spark plugs, envelopes for sodium vapour lamps, cutting tools (when reinforced with silicon carbide) and in artificial joint prostheses. Studies on creep in alumina. have started as early as 1961. There are differing mechanisms proposed to explain the creep behaviour of alumina in the literature, but until now there is no any unanimous decision as to what the rate controlling mechanism is. Magnesia doped at ppm levels can produce significant changes in the microstructure of alumina, the most important consequence of that being the grain growth inhibition, which renders alumina superplastic. However, in a stoichiometric oxide like alumina, small impurities can create extrinsic defects which would change the diffusivities and creep rates. Therefore the background impurities in alumina should be kept to a minimum, if small dopant effects have to be studied. The present study was undertaken making use of high purity alumina powder and comparing the grain growth and creep properties of pure and magnesia doped alumina, especially since no such investigation was carried out in the recent past with high purity alumina. Pure alumina was processed by cold compaction followed by cold isostatic pressing (CIP) and pressureless sintering in air at 1773 K for 1 hour. Magnesia doped alumina was prepared by calcining a mixture of alumina and magnesium nitrate at 973 K for 2 hours followed by cold compaction, CIPing and pressureless sintering in air at 1773 K. Both pure and magnesia doped alumina were further annealed at 1873 K for various times to get grain sizes in the ranges of 1-5 μm. Grain growth kinetics of pure and magnesia doped alumina were studied at 1823 and 1873 K. The parameter Kg which quantifies the mobility of the grain boundary was got. It was found that Kg had decreased in the magnesia doped alumina (in comparison with pure alumina) by a factor of about 3 to 4 which was marginal and insignificant. The grain sizes followed a log normal distribution in both the cases, indicative of normal grain growth. Creep studies were conducted on pure and magnesia doped alumina in three modes, namely, constant stress, temperature jump and stress jump test. The temperature range used was 1673 to 1773 K and the stress range used was 10 to 100 MPa. The creep parameters were found to be n~1.6, p~3.7 and Q-545 kJ mol"1 for pure alumina and n~l .3, p~3.0 and Q~460 kJ mol-1 for magnesia doped alumina. The creep rates in the case of magnesia doped alumina were found to have increased by a factor of 2 to 3, in comparison with pure alumina. The increase in creep rates were found to be insignificant. The creep data were analyzed and the possibility of the dislocation and interface reaction controlled creep mechanisms were ruled out since they were inconsistent with the data. It was found, from creep parameters and the comparison of theoretical Coble and Nabarro-Herring creep rates with the experimental rates, that Coble creep might be rate controlling. The activation energy values suggested that aluminium ion diffusing along grain boundary might be the rate controlling species. However, when the theoretical creep rates considering various species were compared, the rate controlling species turned out to be oxygen ion diffusing along the grain boundary.

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Books on the topic "Pure Aluminum"

1

Slaby, Scott M. Degradation of perfluorinated ether lubricants on pure aluminum surfaces: Semiempirical quantum chemical modeling. Cleveland, OH: National Aeronautics and Space Administration, Lewis Research Center, 1997.

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Terhune, Shannon Derek. An electron backscatter diffraction analysis of the microstructure of pure aluminum processed by equal-channel angular pressing. Monterey, Calif: Naval Postgraduate School, 1998.

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Nielsen, Anni V. Electrochemical studies of pure aluminium in sodiumhydroxidesolutions. Manchester: UMIST, 1993.

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Grjotheim, K. Aluminium smelter technology: A pure and applied approach. 2nd ed. Dusseldorf: Aluminium Verlag, 1988.

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El-Mashri, Saleh M. Structure of anodic-oxide and hydrated oxide films on pure aluminium. [s.l.]: typescript, 1985.

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Slaby, Scott M. Degradation of perfluorinated ether lubricants on pure aluminium surfaces: Semiempirical quantum chemical modeling. Washington, D.C: National Aeronautics and Space Administration, 1997.

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W, Ewing David, Zehe Michael J, and United States. National Aeronautics and Space Administration., eds. Degradation of perfluorinated ether lubricants on pure aluminum surfaces: Semiempirical quantum chemical modeling. [Washington, D.C.]: National Aeronautics and Space Administration, 1997.

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Book chapters on the topic "Pure Aluminum"

1

Han, L., C. Vian, J. Song, Z. Liu, Q. Han, C. Xu, and L. Shao. "Grain Refining of Pure Aluminum." In Light Metals 2012, 967–71. Cham: Springer International Publishing, 2012. http://dx.doi.org/10.1007/978-3-319-48179-1_168.

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Han, L., C. Vian, J. Song, Z. Liu, Q. Han, C. Xu, and L. Shao. "Grain Refining of Pure Aluminum." In Light Metals 2012, 967–71. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2012. http://dx.doi.org/10.1002/9781118359259.ch168.

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Duque, F., and A. Mañanes. "Stability and electronic properties of pure aluminum clusters." In The European Physical Journal D, 223–27. Berlin, Heidelberg: Springer Berlin Heidelberg, 1999. http://dx.doi.org/10.1007/978-3-642-88188-6_43.

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Hartwig, K. T., G. S. Yuan, and P. Lehmann. "Strain Resistivity at 4.2 K in Pure Aluminum." In Advances in Cryogenic Engineering Materials, 405–12. Boston, MA: Springer US, 1986. http://dx.doi.org/10.1007/978-1-4613-9871-4_49.

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Hartwig, K. T., A. Lumbis, and J. Roelli. "Cyclic-Strain Resistivity in Pure Aluminum at 20 K." In Advances in Cryogenic Engineering Materials, 725–32. Boston, MA: Springer US, 1990. http://dx.doi.org/10.1007/978-1-4613-9880-6_94.

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Ota, Mie, Takahiro Seo, and Kei Ameyama. "Microstructure and Mechanical Properties of Harmonic Structure Designed Pure Aluminum." In Proceedings of the 8th Pacific Rim International Congress on Advanced Materials and Processing, 3253–58. Cham: Springer International Publishing, 2013. http://dx.doi.org/10.1007/978-3-319-48764-9_401.

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Ota, Mie, Takahiro Seo, and Kei Ameyama. "Microstructure and Mechanical Properties of Harmonic Structure Designed Pure Aluminum." In PRICM, 3253–58. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2013. http://dx.doi.org/10.1002/9781118792148.ch401.

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Mánic, Tomáš, Bjørn Holmedal, and Odd Sture Hopperstad. "Modeling of Transients as a Response to Changes in Strain-Path of Commercially Pure Aluminium." In ICAA13: 13th International Conference on Aluminum Alloys, 849–54. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2012. http://dx.doi.org/10.1002/9781118495292.ch126.

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Hirata, Tomotake, Taiki Morishige, Masato Tsujikawa, and Kenji Higashi. "Influences of Alloying Elements on Grain Sizes in Friction Stir Processed Pure Aluminum and Aluminum Alloys." In Supplemental Proceedings, 677–84. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2011. http://dx.doi.org/10.1002/9781118062173.ch86.

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Slimani, A., P. Fleischmann, and R. Fougères. "Cyclic Plasticity of Pure Aluminum Studies by Continuous Acoustic Emission Measurement." In Nondestructive Characterization of Materials II, 299–307. Boston, MA: Springer US, 1987. http://dx.doi.org/10.1007/978-1-4684-5338-6_29.

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Conference papers on the topic "Pure Aluminum"

1

Pethe, Rajiv G., Milind Bedekar, Richard E. Demaray, Chandra V. Deshpandey, and Henry Shao. "Pure aluminum process solution for advanced LCDs." In Electronic Imaging '97, edited by Tolis Voutsas and Tsu-Jae King. SPIE, 1997. http://dx.doi.org/10.1117/12.270287.

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Han, Do-Suck, and Jong-Ku Yoon. "The Wettability of Silicon Carbide by Liquid Pure Aluminum and Aluminum Alloys." In International Congress & Exposition. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 1994. http://dx.doi.org/10.4271/940808.

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Nishimoto, Koji, Yoshihiro Okumoto, Tomoki Harano, Ken Atagi, Hiroo Fujii, and Seiji Katayama. "Laser pressure welding of galvanized steel and pure aluminum." In ICALEO® 2008: 27th International Congress on Laser Materials Processing, Laser Microprocessing and Nanomanufacturing. Laser Institute of America, 2008. http://dx.doi.org/10.2351/1.5061424.

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"Influence of Alumina (Al2O3) Nanosized Reinforcements on Dimensional Stability of Pure Aluminum Matrix Nanocomposite." In International Conference on Chemical, Metallurgy and Material Science Engineering. Emirates Research Publishing, 2015. http://dx.doi.org/10.17758/erpub.er815036.

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Nishimoto, Koji, Yoshihiro Okumoto, Tomoki Harano, Ken Atagi, Hiroo Fujii, and Seiji Katayama. "Laser pressure welding of Zn-coated steel and pure aluminum." In ICALEO® 2007: 26th International Congress on Laser Materials Processing, Laser Microprocessing and Nanomanufacturing. Laser Institute of America, 2007. http://dx.doi.org/10.2351/1.5061196.

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Gerngross-Baytekin, Melike, Mark Daniel Gerngross, Jürgen Carstensen, and Rainer Adelung. "Interlocked by nanoscale sculpturing: pure aluminum copper contacts (Conference Presentation)." In Nanotechnology VIII, edited by Ion M. Tiginyanu. SPIE, 2017. http://dx.doi.org/10.1117/12.2265800.

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Glam, Benny, Daniel Moreno, Shalom Eliezer, and Dan Eliezer. "Study of dislocation walls evolution during spall in pure aluminum." In SHOCK COMPRESSION OF CONDENSED MATTER - 2011: Proceedings of the Conference of the American Physical Society Topical Group on Shock Compression of Condensed Matter. AIP, 2012. http://dx.doi.org/10.1063/1.3686443.

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Smirnov, S. V., D. I. Vichuzhanin, A. V. Nesterenko, and A. S. Igumnov. "A fracture locus for commercially pure aluminum at 300 °C." In MECHANICS, RESOURCE AND DIAGNOSTICS OF MATERIALS AND STRUCTURES (MRDMS-2016): Proceedings of the 10th International Conference on Mechanics, Resource and Diagnostics of Materials and Structures. Author(s), 2016. http://dx.doi.org/10.1063/1.4967124.

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Haga, Toshio, Sinjiro Imamura, Hisaki Watari, and Shinichi Nishida. "Effect of Casting Conditions on Fluidity of Aluminum Alloy in Die Casting." In JSME 2020 Conference on Leading Edge Manufacturing/Materials and Processing. American Society of Mechanical Engineers, 2020. http://dx.doi.org/10.1115/lemp2020-8625.

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Abstract The fluidity of pure aluminum and Al-Si alloys was investigated for casting thin products using a spiral die in die casting. An aluminum alloy with good fluidity can be die-cast into thin products. For a Si content of less than 6 mass%, the fluidity increased with decreasing Si content. For a Si content of greater than 6 mass%, the fluidity increased with increasing Si content. The fluidity was affected by latent heat, flowability in the semisolid state, and heat transfer between the die and metal. For pure aluminum, the latent heat is small and there is no semisolid state. However, pure aluminum has excellent fluidity because the heat transfer between the die and metal is small. For Al-25%Si, the latent heat is very large and flowability increases in the semisolid state. Therefore, the fluidity of Al-25%Si is high. Fluidity typically increases with increasing die temperature. The increase in fluidity due to an increase in die temperature for the pure aluminum is small compared with that for hypoeutectic Al-Si alloys. This means that the heat transfer between the pure aluminum and the die is smaller than that for hypoeutectic Al-Si alloys. Therefore, the influence of die temperature on the fluidity of the pure aluminum is small. It is estimated that the chill layer of the pure aluminum rapidly peels from the die, decreasing the heat transfer between the pure aluminum and the die.

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Zhou, Tingting, Yang Yang, and Maobing Shuai. "Constitutive Model Research on Pure Aluminum Considering Dynamic Recovery and Recrystallization." In 2016 3rd International Conference on Mechatronics and Information Technology. Paris, France: Atlantis Press, 2016. http://dx.doi.org/10.2991/icmit-16.2016.135.

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Reports on the topic "Pure Aluminum"

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Henshall, G. A., and N. Q. Nguyen. Ambient temperature fracture strength of pure alumina. Office of Scientific and Technical Information (OSTI), December 1990. http://dx.doi.org/10.2172/6299642.

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Hoffmann, C., C. Hubbard, and J. Keiser. Study of mixed �/�-alumina and pure �-alumina fused cast refractories after exposure in the black liquor gasifier in New Bern, North Carolina. CRADA final report. Office of Scientific and Technical Information (OSTI), March 1999. http://dx.doi.org/10.2172/770424.

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