The Greater than Class C (GTCC) Environmental Impact Statement (EIS) evaluated the potential impacts from the construction and operation of a new facility or facilities, or use of an existing facility, employing various disposal methods (geologic repository, intermediate depth borehole, enhanced near surface trench, and above grade vault) at six federal sites and generic commercial locations. For three of the locations being considered as possible locations, consulting tribes were brought in to comment on their perceptions on how GTCC low level radioactive waste would affect Native American resources (land, water, air, plants, animals, archaeology, etc.) short and long term. The consulting tribes produced essays that were incorporated into the EIS and these essays are in turn included in this collection. This essay was produced by the Confederated Tribes of the Umatilla Indian Reservation.

Solid oxide fuel cells (SOFCs) are promising power generation devices due to its high efficiency and low pollutant emissions. SOFCs operate with a wide range of fuels from hydrogen (H2) to hydrocarbons, and are mainly intended for stationary power generation. Compared to combustion systems, SOFCs have significantly lower environmental impacts. However, the full scale commercialization of SOFCs is impeded by high cost and problems associated with long-term performance and durability. The cell performance can be affected by various internal losses, involving cathode, anode and electrolyte. Anodic losses make a significant contribution to the overall losses, practically in anode-supported cells. Therefore, it is desirable to reduce the anodic losses in order to enhance the overall cell performance. Knowledge of the actual elementary reaction steps and kinetics of electrochemical reactions taking place on the anode is critical for further improvement of the anode performance. Since H2 and carbon monoxide (CO) are the primary reforming products when hydrocarbons are used as SOFC fuels, investigation of electrochemical reactions involving H2 and CO should provide a better understanding of SOFC electrochemical behavior with hydrocarbon feeds. However, still exist uncertainties concerning both H2 and CO electrochemical reactions. The overall objective of this research is to investigate the mechanistic details of H2 and CO electrochemical reactions on SOFC anodes. To achieve this objective, Ni/YSZ pattern anodes were used in the experimental study and as model anodes for the simulation work due to their simplified 2-D structure. The Ni/YSZ pattern anodes were fabricated using a bi-layer resist lift-off method. Imaging resist nLOF2035 and sacrificial resist PGMI SF11 were found to be effective in the bi-layer photolithographic process. Suitable undercut size was found critical for successful pattern fabrication. A simple method, involving taking microscopic photographs of photoresist pattern was developed, to check if the undercut size is large enough for the lift-off; semi-circle wrinkles observable in photographs indicate whether the undercut is big enough for successful pattern anode fabrication. The final product prepared by this method showed straight and clear Ni patterns. A systematic study was performed to determine the stable conditions for Ni/YSZ pattern anode performance. The microstructure and electrochemical behavior changes of the pattern anode were evaluated as a function of Ni thickness, temperature and H2O content in H2 environment. Ni/YSZ pattern anodes with 0.5 µm thick Ni were tested in dry H2 at 550°C without significantly changing the TPB line. Ni/YSZ pattern anodes with Ni thickness of 0.8 µm were tested at 550°C under dry and humidified H2 (3-70% H2O) conditions without TPB line change. For 0.8 µm thick patterns, the TPB length showed pronounced changes in the presence of H2 with 3-70% H2O at 700°C. Significant increase in TPB length due to hole formation was observed at 800°C with 3% and 10% H2O. Ni/YSZ pattern anodes with 1.0 µm thick Ni were stable in H2 with 3% H2O in the range 500-800°C, with only slight changes in the TPB line. Changes of TPB line and Ni microstructure were observed in the presence of 3-70% H2O above 700C. Stabilization of the pattern anode performance depends on temperature. To accelerate stabilization of the cell, pre-treatment of the cell in H2 with 3% H2O for ~22 hrs at 750°C or 800°C could be performed. In addition, comprehensive data sets for H2 and CO electrochemical oxidation reactions on Ni/YSZ pattern anodes were obtained under stable test conditions. For the H2/H2O system, the polarization resistance (Rp) increases as temperature, overpotential, H2 partial pressure, TPB length decreases. Rp is also dependent on H2O content. When the H2O content is between 3% and 30-40%, Rp decreased with increasing H2O content. However, Rp is less affected with further increases in H2O content. For the CO/CO2 system, polarization resistance depends on partial pressure of CO and CO2, temperature and overpotential. Moreover, the polarization resistance decreases when the partial pressure of CO2 and temperature increase. The partial pressure of CO has a positive effect on the polarization resistance. The polarization resistance decreases to a minimum when the overpotential is 0.1 V. For both H2 and CO electrochemical oxidations, charge transfer reactions contribute to the rate limiting steps. A 1-D dynamic SOFC half-cell model considering multiple elementary reaction kinetics was developed. The model describes elementary chemical reactions, electrochemical reactions and surface diffusion on Ni/YSZ pattern anodes. A new charge transfer reactions mechanism proposed by Shishkin and Ziegler (2010) based on Density Functional Theory (DFT) was investigated through kinetic modeling and pattern anode experimental validation. This new mechanism considers hydrogen oxidation at the interface of Ni and YSZ. It involves a hydrogen atom reacting with the oxygen ions bound to both Ni and YSZ to produce hydroxyl (charge transfer reaction 1), which then reacts with the other hydrogen atom to form water (charge transfer reaction 2). The predictive capability of this reaction mechanism to represent our experimental results was evaluated. The simulated Tafel plots were compared with our experimental data for a wide range of H2 and H2O partial pressures and at different temperatures. Good agreements between simulations and experimental results were obtained. Charge transfer reaction 1 was found to be rate-determining under cathodic polarization. Under anodic polarization, a change in rate-limiting process from charge transfer reaction 1 to charge transfer reaction 2 was found when increasing the H2O partial pressure. Surface diffusion was not found to affect the H2 electrochemical performance.

Benzotriazole (BTAH) has been used as a corrosion inhibitor for copper and copper-, based alloys for more than 40 years. It has been successfully employed for the, prevention of both atmospheric corrosion and particularly for the protection of, copper under immersed conditions. Whilst BTAH is an excellent inhibitor in alkaline, solution its efficiency drops off markedly as the pH decreases. It was hypothesized, that a possible way to increase surface adsorption and subsequent better inhibition, over a wide pH range might be through the preparation of derivatives, particularly, carboxybenzotriazoles and alkyl esters of these compounds. In this work the following techniques: weight loss measurements, potentiodynamic, polarisation, SERS spectroscopy, electrochemical impedance spectroscopy and, coulometry were employed to investigate the inhibition efficiency of 4- and 5-, carboxybenzotriazole and their alkyl ester for copper corrosion. Molecular modelling, was also investigated as a tool for inhibitor design. Studies on 4- and 5- carboxybenzotriazole (CBT) showed that the inhibition, efficiency for copper corrosion in aerated acidic sulphate solution of each isomer was, pH, concentration and time dependant. At lower pH the 5-isomer is the better, inhibitor and this behaviour continues at higher pH. The anti-tarnishing test showed, that whilst both isomers exhibited these properties, 5-CBT was once again the, superior inhibitor. It was found that a commercial mixture of the octyl esters of 4- and 5-, carboxybenzotriazole inhibits copper corrosion in sulphate environments open to air., The inhibition efficiency of the ester mixture at the lx10-4 M level (pH - 0) is 98%, which compares very favourably with that for BTAH (- 50%). With respect to other, alkyl esters of 4- and 5-carboxybezotriazole, hexyl, butyl and methyl, it was found, that all of these inlibited copper corrosion in sulphate environments open to air. In, each case the inhibition efficiency is concentration, pH and time dependent. Both, coupon tests and EIS measurements indicate that inhibition efficiency depends on the, length of the alkyl chain. At pH - 0 the inhibition efficiency decreased in the order, octyl &gthexyl &gtbutyl &gtmethyl. At higher pH (- 8) the order is reversed. At the 1x104, M level (pH - 0) the inhibition efficiency of each of the alkyl esters is equal to or, better than that for BTAH. At higher pH (- 8) the inhibition efficiency in each case is, reduced in comparison to BTAH. but is still good enough for practical use ( 2 75%)., The inhibitive behaviour of the alkyl esters at low pH can be attributed to, chemisorption through an azole nitrogen of the protonated alkyl esters. The, hydrocarbon chain is also physically adsorbed and the increase in physical adsorption, as the chain is lengthened accounts for the improved inhibition efficiency. Dry films formed by immersing copper in solutions of alkyl esters of, carboxybenzotriazole also inhibit copper corrosion in both strongly acidic (pH - 0), and near neutral (pH - S) sulphate corrodents. The inhibition efficiency depends on, the solvents used to dissolve the esters, solution temperature and immersion time., Aqueous coating solutions furnish the most protective films. Films formed by, CBTAH-BU, CBTAH-HE and CBTAH-OE are more protective than that formed by, BTAH. The inhibition efficiency of the alkyl ester film increases as the alkyl chain is, made longer. Molecular modeling showed that the optimum crude binding energy (Eblnd), between each protonated ester molecule and the surface varied linearly with the alkyl, chain length. The resulting linear correlation between IE% and E bind for compounds, that are structurally similar suggested that the crude binding energy of a single, molecule with copper may be used to predict the inhibition performance of other, compounds constituting a series.

Thesis (doctoral)--Universität Bremen, 2007. / Includes bibliographical references (p. [153]-161).

Zugl.: München, Techn. Univ., Diss., 2008

Heidelberg, Univ., Diss., 2007.

Techn. Universiẗat, Diss., 2004--Darmstadt.

Les alliages de magnésium représentent une alternative à l’utilisation d’alliages d’aluminium ou de matériaux composites, en particulier dans le secteur aéronautique dans l’objectif de réduire la masse des structures. Ces travaux de thèse ont pour but de participer au développement de nouvelles méthodes de protection des alliages de magnésium, plus efficaces et respectueuses de l’environnement. Pour mener à bien ces travaux, des techniques électrochimiques, en particulier la spectroscopie d’impédance électrochimique, ont été couplées à des mesures par microscopie à force atomique (AFM), à des analyses par spectroscopie d’émission atomique à plasma induit (ICP-AES) et par spectroscopie de masse d’ions secondaires à temps de vol (Tof-SIMS) ainsi que des essais normalisés industriels. Tout d’abord, la résistance à la corrosion en milieu Na2SO4 de trois alliages de magnésium contenant des terres rares (WE43, EV31 et ZE41) a été étudiée et comparée à celle de deux alliages riches en aluminium (AZ31 et AZ91) et à celle du magnésium pur. Pour tous les alliages, il a été montré que les particules intermétalliques agissent comme des cathodes locales. Cet effet de couplage galvanique est plus marqué pour les particules riches en terres rares, en particulier dans le cas de l’alliage EV31. Conjointement, la corrosion est contrôlée par la dissolution de la matrice riche en magnésium et par le recouvrement progressif de la surface métallique par un film d’oxydes/hydroxydes. Ce film est plus protecteur pour les alliages que pour le magnésium pur mais cet effet bénéfique n’est toutefois pas suffisant pour compenser le rôle néfaste joué par les particules intermétalliques. Au final, l’ajout de terres rares augmente la vitesse de corrosion des alliages de magnésium en milieu Na2SO4 par rapport à celle des alliages AZ ou celle du magnésium pur. Dans le cas de l’alliage WE43, qui a été retenu pour la suite de l’étude, il a été montré que le film protecteur d’oxydes est plus mince et plus stable que celui formé sur le Mg pur, en particulier en présence d’ions chlorure. Ces résultats ont été expliqués par l’incorporation des éléments d’alliages, comme l’yttrium, qui serait responsable de la formation d’un film d’oxydes plus compact. Puis, plusieurs méthodes de protection ont été envisagées dans le but d’obtenir une résistance à la corrosion compatible avec les exigences de l’industrie aéronautique. Un traitement d’anodisation, développé par la société Prodem et appelé CEP, en combinaison avec plusieurs primaires de peinture sans chromate, proposés par la société Mapaéro (hydrodiluable ou haut-extrait sec) ont été évalués et comparés aux solutions de référence chromatées. Il a été montré que les traitements de conversion actuels, même en présence de primaire chromaté, ne permettent pas une protection efficace des alliages de magnésium. Le traitement CEP, de par sa structure poreuse, permet une bonne adhésion avec les primaires. Les meilleures performances ont été obtenues pour le traitement CEP revêtu par le primaire haut-extrait sec. Des analyses supplémentaires ont montré que l’ajout d’un vernis permettait d’obtenir un système de protection prometteur pour le remplacement des systèmes de référence sur la base des exigences clés aéronautiques. / Magnesium alloys represent an alternative to aluminum alloys and composite materials – especially in the aeronautic sector with the aim of reducing the structural mass. The main goal of this thesis is to participate in the development of new protection methods that would be more efficient and environmentally-friendly. To this end, electrochemical techniques – such as electrochemical impedance spectroscopy (EIS) – were used together with atomic force microscopy, inductively coupled plasma atomic emission spectrometry, time-of-flight secondary ion mass spectrometry and standardized industrial tests. First, the corrosion resistance in Na2SO4 solution of three magnesium alloys containing rare earths (WE43, EV31 and ZE41) was studied and compared to those of two aluminum-rich magnesium alloys (AZ31 and AZ91) and pure magnesium. For all the alloys, it was shown that intermetallic particles act as local cathodes. This galvanic coupling was stronger in the case of rare earths magnesium alloys, especially for the EV31 alloy. Their corrosion was controlled at the same time by the dissolution of magnesium-rich matrix and by the progressive covering of the alloy surface by an oxides/hydroxides layer. This film was more protective in the case of the alloys; but it is not sufficient to counterbalance the detrimental effect of intermetallic particles. Ultimately, the addition of rare earths increases the corrosion rate of magnesium alloys in Na2SO4 solution compared to aluminum magnesium alloys or pure magnesium. Concerning the WE43 alloy, it was shown that the protective oxide film was thinner and more stable than the one formed on pure magnesium, especially in the presence of chloride ions. These results were explained by the incorporation of alloying elements, like yttrium, that should be responsible of the formation of a more compact film. Then, several protection methods were considered to obtain a corrosion-resistant system that would be compatible with key requirements of the aeronautic industry. The combination of the anodization treatment developed by Prodem Company, called CEP, and the water-based or high-solid coatings offered by Mapaero Company was assessed and compared to classical chromated coatings. It was concluded that current chemical conversion treatments did not provide enough protection for magnesium alloys. The CEP treatment porous morphology acts as an efficient primer base. The best performances were obtained for the CEP treatment in combination with high solid chromate-free coatings. Complementary analysis showed that, with an additional varnish layer, the developed protection system is compatible with aeronautic key requirements.

Les nappes métalliques assurent la structure des pneumatiques. Leur fabrication se décline en plusieurs étapes : le dépôt électrolytique du laiton sur le substrat en acier perlitique, le tréfilage humide du renfort laitonné et l’assemblage mélange-renfort. La pondération de chaque étape sur les mécanismes de corrosion a été évaluée.La composition du revêtement laiton est le premier paramètre étudié. Des caractérisations de surface telles que MEB-EBSD et XPS ont été réalisées et contribuent à l’interprétation des résultats électrochimiques. Les essais électrochimiques ont été menés dans 0,01 M NaCl et couplés à des analyses de solution ICP-AES. Le comportement global du renfort immergé ainsi que le suivi de l’évolution de l’ORR et de la dissolution de l’acier laitonné ont été caractérisés par voltampérométrie linéaire ainsi que par spectroscopie d’impédance électrochimique sous polarisation. L’influence de la composition du revêtement sur le comportement en corrosion a été déterminée.Lors de l’étape de tréfilage, les déformations microstructurales générées ainsi que le lubrifiant ont été identifiés comme des paramètres influents à partir des caractérisations de surface MEB et desoutils électrochimiques (voltampérométrie linéaire et cyclique, SIE sous polarisation, étude des lubrifiants en solution).Dans l’assemblage, le mélange peut agir en tant que cathode. La nature des couplages galvaniques (renfort-mélange ou renfort-renfort) a été identifiée par des mesures ZRA en fonction des conditions de vieillissement. Il a également été montré que les espèces relarguées par le mélange influencent le comportement en corrosion du renfort. La cinétique de dégradation du composite a été évaluée par mesure de la force à la rupture du renfort. La synergie possible entre lubrifiant et mélange a été vérifiées. / The tire structure is provided by metal-rubber composites. Their manufacturing process is divided into several steps : electroplating of brass on steel wires, brass-coated steel wet wire drawing and rubber/wire mixing. The weight of each step on corrosion mechanisms was evaluated.The brass coating composition is the first parameter studied. Surface characterizations such as SEM-EBSD and XPS have been performed and contribute to the electrochemical resultats understanding. Electrochemical experiments were done in 0.01 M NaCl and coupled with ICP-AES measurements. Linear voltammetry as well as electrochemical impedance spectroscopy under polarization are used to characterize the overall behavior of the brass reinforcement and to follow the ORR and dissolution evolution. The coating composition influence on the corrosion behavior has been determined.During the wet wire drawing, microstructure mechanical deformations and lubricant were identified as influencing parameters by means of surface characterization and electrochemical tools (linear and cyclic voltammetry, EIS under polarization, study of lubricants in solution).In the composite, the rubber can act as cathode. The galvanic couplings (rubber-wire or wire-wire) have been identified by ZRA measurements under different aging conditions. The species released by the rubber have revealed an influence on the corrosion behavior. The composite degradation kinetic was evaluated by breaking force measurements. The possible synergy between lubricant and rubber has been verified.

Abstract Thesis in Business Administration, School of Business and Economics, Linnaeus University, 2FE26E, 2017 Author: Hanna Daneshmir Supervisor: Frederic Bill Examiner: Anna Stafsudd
 Title: Emotional Intelligence in an Entrepreneurial context Background: Emotional Intelligence (EI) has been said to matter twice as much as Intelligent Quotient (IQ) for predicting business success (Goleman, 1998b). This study addresses Emotional Intelligence in previously unexplored context in Sweden: entrepreneurship. Purpose: The purpose of this research is to explain Emotional Intelligence and its possible relationship with the entrepreneur. Hypothesis: Being an entrepreneur is positively related to EQ Method: The study has a deductive research approach where the hypothesis is formed by the theoretical framework of Emotional Intelligence, providing an empirical framework that measures the concept in the entrepreneurial context and outlines linkages among the constructs. The study is conducted among members of the business organization Företagarna in Region Halland, Sweden, by the measurement instrument Emotional Intelligence Scale (EIS). Conclusion: The assumptions derived from a theoretical perspective could be confirmed empirically. Being an entrepreneur is positively related to EQ. Keywords: CEO, EI, EIS, EQ, Emotional Intelligence, Entrepreneurs, Entrepreneurship