Corrosion Fatigue of Aluminum-Copper-Lithium Alloy 2050-T84 Submitted at Salt Spray and Aqueous Saline Solution

Interest in the improvement of the structural performance of aircraft has begun in the substitution of aluminum alloys due to the possibility of reduction of density, an increase of stiffness, high fracture toughness, greater resistance to the propagation of cracks by fatigue and greater resistance to corrosion. In these issues, the aluminum-copper-lithium alloy 2050-T84 is outstanding, which presents excellent mechanical properties even when subjected to aggressive atmospheres. The failure of structural components of aircraft occurs due to several factors that may arise from microstructural defects and/or applied static or cyclic stresses associated with atypical environments such as cryogenic or corrosive. In this sense, the results have evidenced the presence of precipitates that influence in the increase of the mechanical strength, behavior of fracture toughness, fatigue life, and corrosion fatigue, in different temperatures and aggressive means. Tensile and fracture toughness tests at 23 and −60°C the material showed ductility retention without a significant difference in the results. Fatigue crack growth in air and corrosion fatigue with 3.5 and 5% NaCl and aqueous solution with 3.5% NaCl showed a meaning difference in the threshold region; however, for the Paris region at the saline environment, fatigue crack growth (FCG) rates are similar

Factors Associated with Emotion Regulation in Men with Internet Access Living in Brazil during the COVID-19 Pandemic

Publisher Copyright: © 2022 by the authors. Licensee MDPI, Basel, Switzerland.Objective: to evaluate the factors associated with emotion regulation in men with internet access living in Brazil during the COVID-19 pandemic. Method: an epidemiological survey, conducted with 1015 men. An electronic form was applied containing sociodemographic and occu-pational characteristics, support and coping strategies, as well as emotional and behavioral aspects. Emotion regulation was assessed using the Emotion Regulation Questionnaire. Results: The prevalence values observed were 44.6% for Low Cognitive Reappraisal and of 47.1% for High Emotional Sup-pression. The following factors were identified as associated: (a) with Low Cognitive Reappraisal: being aged 30 years old or more, practicing physical activity, worrying about social distancing and having positive emotions and feelings; and (b) with High Emotional Suppression: being heterosexual, non-white race/skin color, having security support or public administration, not sanitizing food, worrying about lack of physical activity and not having negative emotions. Conclusion: the adoption of emotion regulation strategies was associated with individual, contextual and emotional/behavioral characteristics. Masculinity ideals seem to exert an influence on these relationships.publishersversionpublishe

SARS-CoV-2 introductions and early dynamics of the epidemic in Portugal

Genomic surveillance of SARS-CoV-2 in Portugal was rapidly implemented by the National Institute of Health in the early stages of the COVID-19 epidemic, in collaboration with more than 50 laboratories distributed nationwide. Methods By applying recent phylodynamic models that allow integration of individual-based travel history, we reconstructed and characterized the spatio-temporal dynamics of SARSCoV-2 introductions and early dissemination in Portugal. Results We detected at least 277 independent SARS-CoV-2 introductions, mostly from European countries (namely the United Kingdom, Spain, France, Italy, and Switzerland), which were consistent with the countries with the highest connectivity with Portugal. Although most introductions were estimated to have occurred during early March 2020, it is likely that SARS-CoV-2 was silently circulating in Portugal throughout February, before the first cases were confirmed. Conclusions Here we conclude that the earlier implementation of measures could have minimized the number of introductions and subsequent virus expansion in Portugal. This study lays the foundation for genomic epidemiology of SARS-CoV-2 in Portugal, and highlights the need for systematic and geographically-representative genomic surveillance.We gratefully acknowledge to Sara Hill and Nuno Faria (University of Oxford) and Joshua Quick and Nick Loman (University of Birmingham) for kindly providing us with the initial sets of Artic Network primers for NGS; Rafael Mamede (MRamirez team, IMM, Lisbon) for developing and sharing a bioinformatics script for sequence curation (https://github.com/rfm-targa/BioinfUtils); Philippe Lemey (KU Leuven) for providing guidance on the implementation of the phylodynamic models; Joshua L. Cherry (National Center for Biotechnology Information, National Library of Medicine, National Institutes of Health) for providing guidance with the subsampling strategies; and all authors, originating and submitting laboratories who have contributed genome data on GISAID (https://www.gisaid.org/) on which part of this research is based. The opinions expressed in this article are those of the authors and do not reflect the view of the National Institutes of Health, the Department of Health and Human Services, or the United States government. This study is co-funded by Fundação para a Ciência e Tecnologia and Agência de Investigação Clínica e Inovação Biomédica (234_596874175) on behalf of the Research 4 COVID-19 call. Some infrastructural resources used in this study come from the GenomePT project (POCI-01-0145-FEDER-022184), supported by COMPETE 2020 - Operational Programme for Competitiveness and Internationalisation (POCI), Lisboa Portugal Regional Operational Programme (Lisboa2020), Algarve Portugal Regional Operational Programme (CRESC Algarve2020), under the PORTUGAL 2020 Partnership Agreement, through the European Regional Development Fund (ERDF), and by Fundação para a Ciência e a Tecnologia (FCT).info:eu-repo/semantics/publishedVersio

Study of fatigue and toughness of friction stir welded (FSW) aluminum and lithium-aluminum alloys subjected to corrosive and cryogenic atmospheres

A pesquisa por novos materiais e processos que possam garantir aeronaves mais leves e operacionalmente mais viáveis, tem-se dado praticamente em todos os componentes de uma aeronave, com consequência direta no menor consumo de combustível e benefícios para o fabricante, operadores e a população em geral com aplicação do conceito de \'aeronave verde\'. Nestes quesitos, materiais/processos, destacam-se as ligas de alumínio (2xxx e 7xxx) e a solda por fricção mistura (FSW- Friction Stir Welding) por sua relação custo/benefício. A soldagem por fricção de elementos estruturais aeronáuticos formados de materiais dissimilares que possuem propriedades mecânicas distintas é de grande interesse para a indústria aeronáutica, devido aos ganhos de peso e de custo de operação que esse tipo de junção pode gerar. Sendo assim foram avaliadas as principais propriedades mecânicas de interesse e correlacionar com a microestrutura de ligas dissimilares e similares soldadas pelo processo de FSW e a inteiração destas com os meios ambiente, criogênico e corrosivo aos quais, aeronaves podem ser sujeitas durante os voos. Para tal desenvolvimento a solda dissimilar foi realizada com as ligas de alumínio-lítio 2050-T84 e alumínio 7050-T7451, enquanto que a solda similar foi realizada com a liga de alumínio-lítio 2198-T851. Foram feitas análises de ciclo térmico durante a soldagem e ambas juntas foram classificadas como solda quente, que prevê intensa variação microestrutural e afetam as propriedades mecânicas de dureza, a tenacidade fadiga e corrosão fadiga. A caracterização microestrutural realizada pela técnica de EBSD evidenciou alta quantidade de CAA que resultou na redução da dureza e aumento da tenacidade à fratura na região de contato entre a peça de trabalho e o ombro da ferramenta. De contra partida, a taxa de propagação de trinca por fadiga aumentou ligeiramente no meio salino.The research for new materials and processes that produce light materials and operationally viable, has occurred in almost all the components of an aircraft, with a direct consequence in the lower fuel consumption and benefits for the manufacturing, operators and the population in application of the concept of \'green aircraft\'. In these questions, materials/processes, the most important are aluminum alloys (2xxx and 7xxx) and friction stir welding for their cost/benefit ratio. Friction stir welding of aeronautical structural elements made of dissimilar materials with distinct mechanical properties is of great interest to the aeronautical industry due to the weight and operating costs that this type of joint can result. Thus, the main mechanical properties of interest and correlate with the microstructure of dissimilar and similar alloys welded by the FSW and their interaction with the ambient, cryogenic and corrosive environments to which aircraft may be subject during flight. To development, the dissimilar weld performed with the lithium-aluminum alloys 2050-T84 and aluminum 7050-T7451, while the similar solder performed with the lithium-aluminum alloy 2198-T851. Thermal cycle analyzes were done during welding and both joints were classified as hot welding, which provides intense microstructural variation and affect the mechanical properties of hardness, fatigue toughness and fatigue corrosion. The microstructural characterization performed by the EBSD technique evidenced a high amount of CAA that resulted in low hardness and high fracture toughness in the region of contact between the workpiece and the tool shoulder. On the other hand, the rate of crack propagation by fatigue increased slightly in the saline atmosphere

Study toughness and fatigue in atmosphere assisted of the aircraft alloy grade AA2050-T84

A indústria aeronáutica tem buscado melhorias no conceito de integridade estrutural, a partir do desenvolvimento de projetos mais otimizados com a produção de aeronaves mais leves e seguras. Tais projetos garantem aeronaves operacionalmente mais viáveis e redução no consumo de combustível, beneficiando o fabricante, os operadores e a população em geral, pois aplica o conceito de aeronave verde. Estruturas aeronáuticas em operação recebem solicitações de cargas típicas de vôo, como pressurização, sustentação, que por sua vez, geram esforços dos mais variados tipos e suas combinações, como tração, compressão, fadiga, torção, flexão, flambagem, cargas aeroelásticas, vibrações e flutter, associados a ambientes críticos. O conhecimento sobre o comportamento do material estrutural perante ambientes corrosivo ou de baixa temperatura, é importante para avaliação da vida útil das aeronaves. Neste contexto, o objetivo deste trabalho foi avaliar o comportamento da liga AA2050-T84 sob ponto de vista de corrosão-fadiga e tenacidade a fratura em criogenia e, correlacionar com a microestrutura e fractografia através de ensaios mecânicos e de tenacidade a fratura em temperatura ambiente e criogênica. As condições de ensaios foram determinadas próximas a de serviço a que o material será inserido sendo, para criogenia -54 ºC e para os ensaios de propagação de trinca por fadiga em atmosfera ambiente e névoa salina com concentração de solução de 3,5% e 5% NaCl, frequência de 15Hz e razões de carga R = 0,1 e 0,5. Os resultados em criogenia mostraram que há melhora nas propriedades trativas e estabilidade na tenacidade, pois o material retém dutilidade com o decréscimo da temperatura. Os ensaios de propagação de trinca por fadiga foram executados com ΔK decrescente e os parâmetros para geração de névoa salina foram determinados experimentalmente. As curvas de crescimento de trinca e determinação do fator limite foram comparadas quanto a razão de carga e atmosfera de ensaio. Observou-se que para os ensaios de propagação de trinca por fadiga a presença da névoa salina acelera a taxa de propagação e resultam em um fator limite menor.The aviation industry has sought improvements with the concept of structural integrity, from the development of more optimized designs with production aircraft with low weight and secure. These projects ensure an aircraft more operationally doable and reduced fuel consumption, benefiting the manufacturer, operators and the people, applying the concept of green aircraft. Aerospace structures in operation receive requests loads typical of flight, how pressurization support and lift that produce several types and combinations of requests, such as tensile, compression, fatigue, torsion, bending, buckling , aeroelastic loads, vibration and flutter associated with critical environments. Knowledge about the behavior of the structural material into corrosive environments or cryogenic temperature, it is important for evaluation to the lifetime of the aircraft. Accordingly , the aim of this study was to estimate the behavior of AA2050 - T84 alloy, about corrosion-fatigue and fracture toughness at cryogenic situations and correlate with microstructure and fractography, by mechanical tests and fracture toughness at room temperature and cryogenic. The test conditions has been determined near of the service that the material will be inserted, for cryogenic temperature -54 ºC and testing of fatigue crack propagation in air and salt spray with concentration of 3.5% and 5% NaCl, frequency 15Hz and load ratios R = 0.1 and 0.5. The cryogenic results showed that there improvement in tensile properties and stability in toughness due the restraint of ductility with decreasing temperature. Tests of fatigue crack propagation were carried out with ΔK decreasing and the parameters to obtain salt spray were determined experimentally. The crack growth curves and determination of the threshold were compared the according to load ratio and test atmosphere. In the fatigue crack propagation it was observed that presence of salt spray accelerates the rate of propagation and result in a lower threshold

Study toughness and fatigue in atmosphere assisted of the aircraft alloy grade AA2050-T84

A indústria aeronáutica tem buscado melhorias no conceito de integridade estrutural, a partir do desenvolvimento de projetos mais otimizados com a produção de aeronaves mais leves e seguras. Tais projetos garantem aeronaves operacionalmente mais viáveis e redução no consumo de combustível, beneficiando o fabricante, os operadores e a população em geral, pois aplica o conceito de aeronave verde. Estruturas aeronáuticas em operação recebem solicitações de cargas típicas de vôo, como pressurização, sustentação, que por sua vez, geram esforços dos mais variados tipos e suas combinações, como tração, compressão, fadiga, torção, flexão, flambagem, cargas aeroelásticas, vibrações e flutter, associados a ambientes críticos. O conhecimento sobre o comportamento do material estrutural perante ambientes corrosivo ou de baixa temperatura, é importante para avaliação da vida útil das aeronaves. Neste contexto, o objetivo deste trabalho foi avaliar o comportamento da liga AA2050-T84 sob ponto de vista de corrosão-fadiga e tenacidade a fratura em criogenia e, correlacionar com a microestrutura e fractografia através de ensaios mecânicos e de tenacidade a fratura em temperatura ambiente e criogênica. As condições de ensaios foram determinadas próximas a de serviço a que o material será inserido sendo, para criogenia -54 ºC e para os ensaios de propagação de trinca por fadiga em atmosfera ambiente e névoa salina com concentração de solução de 3,5% e 5% NaCl, frequência de 15Hz e razões de carga R = 0,1 e 0,5. Os resultados em criogenia mostraram que há melhora nas propriedades trativas e estabilidade na tenacidade, pois o material retém dutilidade com o decréscimo da temperatura. Os ensaios de propagação de trinca por fadiga foram executados com ΔK decrescente e os parâmetros para geração de névoa salina foram determinados experimentalmente. As curvas de crescimento de trinca e determinação do fator limite foram comparadas quanto a razão de carga e atmosfera de ensaio. Observou-se que para os ensaios de propagação de trinca por fadiga a presença da névoa salina acelera a taxa de propagação e resultam em um fator limite menor.The aviation industry has sought improvements with the concept of structural integrity, from the development of more optimized designs with production aircraft with low weight and secure. These projects ensure an aircraft more operationally doable and reduced fuel consumption, benefiting the manufacturer, operators and the people, applying the concept of green aircraft. Aerospace structures in operation receive requests loads typical of flight, how pressurization support and lift that produce several types and combinations of requests, such as tensile, compression, fatigue, torsion, bending, buckling , aeroelastic loads, vibration and flutter associated with critical environments. Knowledge about the behavior of the structural material into corrosive environments or cryogenic temperature, it is important for evaluation to the lifetime of the aircraft. Accordingly , the aim of this study was to estimate the behavior of AA2050 - T84 alloy, about corrosion-fatigue and fracture toughness at cryogenic situations and correlate with microstructure and fractography, by mechanical tests and fracture toughness at room temperature and cryogenic. The test conditions has been determined near of the service that the material will be inserted, for cryogenic temperature -54 ºC and testing of fatigue crack propagation in air and salt spray with concentration of 3.5% and 5% NaCl, frequency 15Hz and load ratios R = 0.1 and 0.5. The cryogenic results showed that there improvement in tensile properties and stability in toughness due the restraint of ductility with decreasing temperature. Tests of fatigue crack propagation were carried out with ΔK decreasing and the parameters to obtain salt spray were determined experimentally. The crack growth curves and determination of the threshold were compared the according to load ratio and test atmosphere. In the fatigue crack propagation it was observed that presence of salt spray accelerates the rate of propagation and result in a lower threshold

Núcleos de Ensino da Unesp: artigos 2008

Conselho Nacional de Desenvolvimento Científico e Tecnológico (CNPq

Evaluation of a quality improvement intervention to reduce anastomotic leak following right colectomy (EAGLE): pragmatic, batched stepped-wedge, cluster-randomized trial in 64 countries

Background Anastomotic leak affects 8 per cent of patients after right colectomy with a 10-fold increased risk of postoperative death. The EAGLE study aimed to develop and test whether an international, standardized quality improvement intervention could reduce anastomotic leaks. Methods The internationally intended protocol, iteratively co-developed by a multistage Delphi process, comprised an online educational module introducing risk stratification, an intraoperative checklist, and harmonized surgical techniques. Clusters (hospital teams) were randomized to one of three arms with varied sequences of intervention/data collection by a derived stepped-wedge batch design (at least 18 hospital teams per batch). Patients were blinded to the study allocation. Low- and middle-income country enrolment was encouraged. The primary outcome (assessed by intention to treat) was anastomotic leak rate, and subgroup analyses by module completion (at least 80 per cent of surgeons, high engagement; less than 50 per cent, low engagement) were preplanned. Results A total 355 hospital teams registered, with 332 from 64 countries (39.2 per cent low and middle income) included in the final analysis. The online modules were completed by half of the surgeons (2143 of 4411). The primary analysis included 3039 of the 3268 patients recruited (206 patients had no anastomosis and 23 were lost to follow-up), with anastomotic leaks arising before and after the intervention in 10.1 and 9.6 per cent respectively (adjusted OR 0.87, 95 per cent c.i. 0.59 to 1.30; P = 0.498). The proportion of surgeons completing the educational modules was an influence: the leak rate decreased from 12.2 per cent (61 of 500) before intervention to 5.1 per cent (24 of 473) after intervention in high-engagement centres (adjusted OR 0.36, 0.20 to 0.64; P < 0.001), but this was not observed in low-engagement hospitals (8.3 per cent (59 of 714) and 13.8 per cent (61 of 443) respectively; adjusted OR 2.09, 1.31 to 3.31). Conclusion Completion of globally available digital training by engaged teams can alter anastomotic leak rates. Registration number: NCT04270721 (http://www.clinicaltrials.gov)