Academic literature on the topic 'T6I6'
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Journal articles on the topic "T6I6"
Sainis, Salil, Aakarshit Kalra, G. Dinesh Babu, and M. Nageswara Rao. "Weibull Analysis of the Effect of Interrupted Aging Treatments on the Fatigue Life of Components Made of Cast Aluminium Alloy 354." Advanced Materials Research 849 (November 2013): 223–27. http://dx.doi.org/10.4028/www.scientific.net/amr.849.223.
Full textRisanti, D. D., and Sybrand van der Zwaag. "Effect of Low Temperature Aging on Internal Friction of AA2024." Advanced Materials Research 463-464 (February 2012): 41–46. http://dx.doi.org/10.4028/www.scientific.net/amr.463-464.41.
Full textBabu, G. Dinesh, and M. Nageswara Rao. "Effect of Non-Conventional Aging Treatments on the Tensile Properties of Non-Hipped Castings of Aluminum Alloy 354." Advanced Materials Research 875-877 (February 2014): 1397–405. http://dx.doi.org/10.4028/www.scientific.net/amr.875-877.1397.
Full textBabu, G. Dinesh, and M. Nageswara Rao. "Effect of Non-Conventional Aging Treatments on the Tensile Properties and Quality Indices of Hipped Components Made of Cast Aluminum Alloy 354." Advanced Materials Research 875-877 (February 2014): 1429–36. http://dx.doi.org/10.4028/www.scientific.net/amr.875-877.1429.
Full textSibal, Prateek, G. Dinesh Babu, and M. Nageswara Rao. "Use of Strain Energy Density W and Qo as Quality Indices for Rating the Quality of Cast Aluminium Alloy354 as a Function of Processing Parameters." Advanced Materials Research 704 (June 2013): 189–94. http://dx.doi.org/10.4028/www.scientific.net/amr.704.189.
Full textKaczmarek, Ł., M. Steglinski, J. Sawicki, J. Swiniarski, D. Batory, K. Kyzioł, Ł. Kołodziejczyk, W. Szymanski, P. Zawadzki, and D. Kottfer. "Optimization of the Heat Treatment and Tribological Properties of 2024 and 7075 Aluminium Alloys." Archives of Metallurgy and Materials 58, no. 2 (June 1, 2013): 535–40. http://dx.doi.org/10.2478/amm-2013-0032.
Full textLipa, Sebastian, Łukasz Kaczmarek, Mariusz Stegliński, Hanna Radziszewska, Karol Kyzioł, and Daniel Kottfer. "Effect of core/shell precipitations on fatigue strength of 2024-T6I6 alloy." International Journal of Fatigue 127 (October 2019): 165–74. http://dx.doi.org/10.1016/j.ijfatigue.2019.06.006.
Full textRadziszewska, Hanna, Lukas Kaczmarek, and Zbigniew Gawroński. "Effect of Precipitation with Core-Shell Structure on Mechanical Properties of PN-EN 2024 T6I6 Alloy." Journal of Siberian Federal University. Chemistry 10, no. 1 (March 2017): 67–81. http://dx.doi.org/10.17516/1998-2836-0007.
Full textLI, Hai, Daozhao PAN, Zhixiu WANG, and Ziqiao ZHENG. "INFLUENCE OF T6I6 TEMPER ON TENSILE AND INTERGRANULAR CORROSION PROPERTIES OF 6061 ALUMINUM ALLOY." ACTA METALLURGICA SINICA 46, no. 4 (April 21, 2010): 494–99. http://dx.doi.org/10.3724/sp.j.1037.2010.00494.
Full textArfuso, Francesca, Elisabetta Giudice, Simona Di Pietro, Giuseppe Piccione, and Claudia Giannetto. "Modulation of Serum Protein Electrophoretic Pattern and Leukocyte Population in Horses Vaccinated against West Nile Virus." Animals 11, no. 2 (February 11, 2021): 477. http://dx.doi.org/10.3390/ani11020477.
Full textDissertations / Theses on the topic "T6I6"
Buha, Joka School of Materials Science & engineering UNSW. "Interrupted ageing of Al-Mg-Si-Cu alloys." Awarded by:University of New South Wales. School of Materials Science and engineering, 2005. http://handle.unsw.edu.au/1959.4/20794.
Full textAlateah, Souad Mohammed. "Transforming clinical mycobacteriology with modern molecular methodology." Thesis, University of St Andrews, 2018. http://hdl.handle.net/10023/15920.
Full textTownes, William Waverley VI. "a study of showing." Thesis, Virginia Tech, 2008. http://hdl.handle.net/10919/33347.
Full textMaster of Architecture
Jacumasso, Sheila Cristina. "CARACTERIZAÇÃO MICROESTRUTURAL DAS PARTÍCULAS DE SEGUNDA FASE DE UMA LIGA DE ALUMÍNIO AA7050 NAS CONDIÇÕES T7451, T6 E T6I4-65." UNIVERSIDADE ESTADUAL DE PONTA GROSSA, 2014. http://tede2.uepg.br/jspui/handle/prefix/1460.
Full textCoordenação de Aperfeiçoamento de Pessoal de Nível Superior
The AA7050 class from the 7XXX series alloys based on Al-Zn-Mg-Cu are widely used in aerospace structures and fuselage components, when the same are subjected to high stress loading due to its high ratio mechanical strength to density, in addition, to its corrosion resistance. The increased resistance of these alloys is obtained by heat treatment that involves solution treatment and ageing followed precipitation of a fine and homogeneous phase from the own chemical composition. In this, the present study aimed to perform the of AA7050 aluminum alloy microstructural characterization with different ageing heat treatment from the T7451, T6 and T6I4-65 conditions. Thus, different characterization techniques from the Optical Microscopy (OM), Scanning Electron Microscopy (SEM), Atomic Force Microscopy (AFM), Extraction of second phase particles, X-ray Diffraction (XRD) and Transmission Electron Microscopy (TEM) were used. It was evaluated which condition results is higher precipitation hardening phases that are responsible for the increased resistance of the alloy. The most significant results were obtained by TEM where it was possible to determine the morphology of the GPII zones in needles form with approximate size of 30nm and 10nm for both T6 and T6I4-65 conditions, respectively. Moreover, the metastable η' phase was identified in platelets form in the T7451, T6 and T6I4-65 conditions with approximate size of 50nm, 20nm and 10nm, respectively. The surface roughness analyses obtained by AFM have revealed that the T6I4-65 condition has higher surface roughness (Ra=14,87nm) when compared to the T7451 (Ra=7,65nm) and T6 (Ra=8,35nm) conditions. Indicating in this case, a higher density of small particles homogeneously distributed in the T6I4-65 aluminum alloy matrix.
As ligas da série 7XXX, da classe AA7050, à base de Al-Zn-Mg-Cu, são muito utilizadas na indústria aeroespacial, em estruturas de fuselagem e componentes sob alta tensão de carregamento, devido à sua alta relação entre resistência mecânica e densidade, além de sua resistência à corrosão. O aumento da resistência destas ligas é obtido por tratamento térmico de solubilização e envelhecimento, através da precipitação de uma fase fina e homogênea, proveniente da própria composição química. Neste contexto, o presente trabalho teve como objetivo principal realizar a caracterização microestrutural de uma liga de alumínio AA7050, submetida a diferentes tratamentos térmicos de envelhecimento nas condições T7451, T6 e T6I4-65. Desse modo, fez-se o uso de diferentes técnicas de caracterização entre elas Microscopia Ótica (MO), Microscopia Eletrônica de Varredura (MEV), Microscopia de Força Atômica (AFM), Extração de Partículas de segunda fase, Difração de Raios X (DRX) e Microscopia Eletrônica de Transmissão. Consequentemente, avaliou-se qual condição apresenta maior precipitação de fases endurecedoras que são responsáveis pelo aumento de resistência da liga. Os resultados mais significativos foram obtidos por MET onde foi possível determinar a morfologia das zonas GPII presentes na forma acicular (needles) com tamanho aproximado de 30nm na condição T6 e 10nm na condição T6I4-65. A fase metaestável η’ foi identificada na forma de plaquetas finas (platelets) nas condições T7451, T6 e T6I4-65 com tamanho aproximado de 50nm, 20nm e 10nm respectivamente. A rugosidade superficial obtida por AFM revelou que a condição T6I4-65 apresenta maior rugosidade superficial (Ra=14,87nm) quando comparado às condições T7451(Ra=7,65nm) e T6 (Ra=8,35nm), indicando maior densidade de partículas de pequena dimensão distribuída homogeneamente na matriz da liga de alumínio.
Trivette, Paul S. "A national survey of occupational stress, psychological strain and coping resources in elementary school counselors." Diss., Virginia Tech, 1993. http://hdl.handle.net/10919/38343.
Full textTopor, James E. "Analysis of grey level weighted Hough transforms." Thesis, This resource online, 1990. http://scholar.lib.vt.edu/theses/available/etd-07282008-135731/.
Full textTrump, Karen E. "Characteristics of mildly handicapped children in a small school district." Diss., Virginia Polytechnic Institute and State University, 1988. http://hdl.handle.net/10919/87678.
Full textEd. D.
Lima, Luis Otavio Ribas de. "Estudo sobre o tratamento térmico de envelhecimento interrompido T6I4-65 e influência na propagação de trinca por fadiga em uma liga de alumínio AA7050." UNIVERSIDADE ESTADUAL DE PONTA GROSSA, 2014. http://tede2.uepg.br/jspui/handle/prefix/1462.
Full textCoordenação de Aperfeiçoamento de Pessoal de Nível Superior
Aluminum alloys have been the primary material of choice for the aircraft due to their properties such as low density, high mechanical and corrosion resistance. Commercial aircraft apply aluminum alloys for the fuselage, wings and supporting structure due to the extensive knowledge in design and production of aluminum components, and most importantly, aluminum alloys continue to be developed, keeping it highly competitive. A great development happen with the heat-treatable alloys, which allow improvement of the mechanical properties. Among this alloys stand out the Al-Zn-Mg-Cu series, known for high strength, toughness and corrosion resistance. The improvement of those alloys occurs by the precipitation of nanometric particles MgZn2, called η phase. This study’s aim was to promote an interrupted heat treatment T6I4-65 in an AA7050 aluminum alloy, with fatigue crack growth resistance as priority. Interrupted heat treatments’ goal is optimizing the consumption of solute atoms during process of nucleation and growth of precipitates as a finely dispersion. The T6I4-65 condition obtained was analyzed by differential scanning calorimetry, DSC, optical and electronic microscopy, mechanical tests as hardness, tensile and fatigue crack growth. The T6I4-65 treatment results in a microstructure with a fine dispersion of precipitated phase η’, about 75% smaller than those resulting from in current use, T7451. This microstructure resulted in a reduction of up to 24% in fatigue crack growth rate compared to that resulting from T7451 treatment, keeping the ductility of 17% of area reduction and yield strength higher than 400MPa.
Ligas de alumínio são o principal material de uso na indústria aeronáutica devido a suas propriedades como baixa densidade, alta resistência mecânica e a corrosão. Aeronaves comerciais utilizam ligas de alumínio em sua fuselagem, asas e na estrutura de suporte devido ao extenso conhecimento no projeto e produção de componentes em alumínio, e mais importante, as ligas de alumínio continuam a serem desenvolvidas, mantendo-se altamente competitivas. Ocorreu um grande avanço com o desenvolvimento das ligas tratáveis termicamente, que permitiram a otimização das propriedades mecânicas. Entre estas ligas tratáveis, destaca se a família Al-Zn-Mg-Cu, conhecidas pela alta resistência mecânica, tenacidade e resistência a corrosão. O aperfeiçoamento destas ligas ocorre pela precipitação de partículas nanométricas de MgZn2, conhecida como fase η. O objetivo deste trabalho foi obter um tratamento térmico interrompido T6I4-65 em uma liga de alumínio AA7050 com prioridade ao aumento de resistência à propagação de trinca por fadiga. Tratamentos interrompidos tem por objetivo otimizar o consumo de átomos de soluto durante os processos de nucleação e crescimento dos precipitados endurecedores na liga na forma de dispersão finamente dispersa. A condição T6I4-65 obtida foi analisada por meio de calorimetria diferencial de varredura, DSC, microscopia ótica e eletrônica de varredura e transmissão, ensaios mecânicos dureza, tração e propagação de trinca por fadiga. Este tratamento resultou em uma microestrutura com uma dispersão de finos precipitados de fase η’, cerca de 75% menores que os resultantes de tratamentos de uso corrente, T7451. Esta microestrutura promoveu a redução de até 24% na taxa de propagação de trinca por fadiga em comparação à resultante do tratamento T7451, mantendo grande ductilidade, até 17% de redução de área e limite de escoamento superior a 400MPa.
Šplíchal, Jan. "Návrh snížení počtu svarů u rámových dveří kolejových vozidel z Al slitin." Master's thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2019. http://www.nusl.cz/ntk/nusl-399353.
Full textTornaris, George Andreas. "Traffic flow management under emergency conditions in and around the Virginia Tidewater area tunnels." Thesis, Virginia Polytechnic Institute and State University, 1986. http://hdl.handle.net/10919/101325.
Full textM.S.
Books on the topic "T6I6"
Correll, Robert, and Julie Adair King. Canon EOS Rebel T6i / 750D for Dummies. Wiley & Sons, Incorporated, John, 2015.
Find full textCorrell, Robert, and Julie Adair King. Canon EOS Rebel T6i / 750D for Dummies. Wiley & Sons, Incorporated, John, 2015.
Find full textCanon EOS Rebel T6s / T6i: From Snapshots to Great Shots. Peachpit Press, 2015.
Find full textBusch, David D. Canon EOS Rebel T6s/T6i/760D/750D Guide to Digital SLR Photography. Rocky Nook, 2016.
Find full textBook chapters on the topic "T6I6"
Uhríčik, Milan, Peter Kopas, Peter Palček, Tatiana Oršulová, and Patrícia Hanusová. "MULTIAXIAL FATIGUE EXPERIMENTAL ANALYSIS OF 6063-T66 ALUMINUM ALLOY OF THE BASE MATERIAL AND THE WELDED MATERIAL." In Quality Production Improvement - QPI, edited by Robert Ulewicz, 334–41. Warsaw, Poland: Sciendo, 2019. http://dx.doi.org/10.2478/9783110680591-045.
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