After the identification of unexpected products formed from methyl dichloro-acetate and an amino-sulphonamide during the attempted synthesis of a derivative of 3,4-dihydro-2H-1,2,4-benzothiadiazine 1,1-dioxide, unprecedented selective acylation of the sulphonamido group in sulphanilamide was found to occur when esters of activated carboxylic acids were allowed to condense at 25 °C with the sodium salt of sulphanilamide in methanol. The scope of this reaction was examined both with respect to the amino-sulphonamide and with respect to the ester used as acylating agent. No limitations to the reaction were found among the amino-sulphonamides examined, each of which was acylated exclusively at the sulphonamido group. Methyl dichloro-acetate and methyl tricyloroacetate were effective acylating agents, ethyl dichloro-acetate was less so, and ethyl chloroacetate was ineffective. The mechanisms of the new reaction and of the classical acylation by acyl-pyridinium ions are discussed and compared, and explanations are offered for the contra-selectivity of the two reactions. The infrared spectra of the N-aminoarenesulphonyl-2, 2-dichloroacetamides and N-aminoarenesulphonyl-2, 2, 2-trichloroacetamides made by the new method reveal that in many cases these compounds have a zwitterionic structure in the solid state which is lost in their azo-β-naphthol derivatives. 相似文献
Universal Access in the Information Society - In Brazil, there are approximately 9.7 million inhabitants who are deaf or hard of hearing. Moreover, about 30% of the Brazilian deaf community is... 相似文献
The performance of cemented carbide cutting tools during machining is influenced not only by the mechanical properties of the coating and substrate but also by the topographies of their surfaces. A tool with good coating and substrate properties but unsuitable topographies may exhibit accelerated wear and, consequently, impaired performance. In this work, drills coated using physical vapor deposition (PVD) were produced with different substrate textures, which in turn generated different coating textures. The surface roughness values of the coated drills were measured together with the residual stress at the interface between substrate and coating. Drilling tests were performed and tool wear was measured during the machining process. Two different tool coatings were studied: TiAlN and TiAlCrSiN. The goal was to study how the characteristics of the substrate and coating (material, surface topography, and residual stress) influence tool life. Tool life experiments were carried out using drilling tests in AISI 1548 steel, which is often used in crankshafts. The primary tool wear mechanism was attrition in all the drills. The main conclusion of this work is that the tool with the lowest roughness and a TiAlCrSiN coating had the best performance in the conditions tested here. 相似文献
Software Quality Journal - Traditional runtime quantitative verification approaches for self-adaptive systems usually rely on the use of state-transition models to describe the system behaviour and... 相似文献
In the present study, Nb-stabilized ferritic stainless steel was prepared with annealing (430-A) and without annealing (430-NA) annealing, and the microstructure of the resulting samples was examined. The steel was then subjected to cold rolling and isothermal annealing in order to analyze its recrystallization kinetics and texture evolution. Microstructural characterization was performed by scanning and transmission electron microscopies. Recrystallization kinetics were evaluated by measuring the microhardness of the samples, and analyzing their kernel average misorientation and grain orientation spread via electron backscatter diffraction. The Avrami exponent data revealed that one-dimensional grain growth occurred owing to the migration of high-angle grain boundaries. The mean activation energies for recrystallization for 430-NA and 430-A was found to be 365 and 419 kJ mol−1, respectively. The recrystallization texture was influenced by oriented nucleation and selected growth mechanisms, as well as by the Nb carbonitride distribution and grain boundary energy. The recrystallized and growing grains with the {554}〈225〉 orientation showed a dimensional advantage over the other recrystallized components. The coincident site lattice boundaries were attributed to the progression of recrystallization since the CSL numeric fraction increased as the temperature increased. The {554}〈225〉 component was associated with the ∑19a boundary, which exerted a significant control on the selective growth during the recrystallization.
Iron‐promoted cyclization of 1‐benzyl‐2‐alkynylbenzenes with diorganyl diselenides led to the synthesis of 9‐(organoselanyl)‐5H‐benzo[7]annulenes whereby the mutual action between diorganyl diselenides and iron(III) chloride in a 0.5:1.0 mol ratio was essential in order to achieve the maximal yields of the products. The cyclization reaction tolerated a variety of functional groups, such as trifluoromethyl, chloro, fluoro and methoxy, in both the 1‐benzyl‐2‐alkynylbenzenes and the diorganyl diselenides, giving the seven‐membered heterocyclic products exclusively via a 7‐endo‐dig cyclization process.
A computational investigation of the interference between wings having different aspect ratios and a tractor propeller has been carried out to accurately determine the time-averaged aerodynamic characteristics of the aircraft in terms of the modified wing loads. At first, the aerodynamic interaction has been studied by modeling the wakes both of propeller and wing, in isolated and coupled configurations. The model is based on a hybrid numerical technique, the free wake analysis (FWA) and boundary element method (BEM), applied to the wakes of a propeller and a wing, respectively. The output data has been compared with those available from the experimental procedures. Subsequently, to describe the effects of the two interacting wakes, a three-dimensional BEM approach for an untapered wingspan was applied to evaluate the wing quasisteady loads. The research focused on the wing pressure coefficient distribution related to the altered upstream conditions of the coupled propeller, hence the wing loads and the pitching moment are computed. The results confirm the advantages of the present approach using the FWA and BEM to identify the aerodynamic features of the mutual interference of a wing and a propeller at angle of attack and at a fixed propeller operating condition. Applications of this numerical hybrid scheme to an isolated wing and propeller, in quasisteady flow conditions, as well as to coupled configurations, are shown in the present paper. They demonstrate that accurate results can be obtained with very low computational effort. 相似文献