Comparative exergy analysis of direct alcohol fuel cells using fuel mixtures

Within the last years there has been increasing interest in direct liquid fuel cells as power sources for portable devices and, in the future, power plants for electric vehicles and other transport media as ships will join those applications. Methanol is considerably more convenient and easy to use than gaseous hydrogen and a considerable work is devoted to the development of direct methanol fuel cells. But ethanol has much lower toxicity and from an ecological viewpoint ethanol is exceptional among all other types of fuel as is the only chemical fuel in renewable supply. The aim of this study is to investigate the possibility of using direct alcohol fuel cells fed with alcohol mixtures. For this purpose, a comparative exergy analysis of a direct alcohol fuel cell fed with alcohol mixtures against the same fuel cell fed with single alcohols is performed. The exergetic efficiency and the exergy loss and destruction are calculated and compared in each case. When alcohol mixtures are fed to the fuel cell, the contribution of each fuel to the fuel cell performance is weighted attending to their relative proportion in the aqueous solution. The optimum alcohol composition for methanol/ethanol mixtures has been determined.

Perspectives on the design and use of direct alcohol fuel cells fed by alcohol blends

The fast-growing power demand by portable electronic devices has promoted the increase of global production of portable PEM fuel cell, a quarter of them consist of direct methanol fuel cell (DMFC) units. These present the advantage of being fuelled directly with a liquid fuel, as well as direct ethanol fuel cells (DEFC) do.

Sheath vaporization of a monodisperse fuel-spray jet

The group vaporization of a monodisperse fuel-spray jet discharging into a hot coflowing gaseous stream is investigated for steady flow by numerical and asymptotic methods with a two-continua formulation used for the description of the gas and liquid phases. The jet is assumed to be slender and laminar, as occurs when the Reynolds number is moderately large, so that the boundary-layer form of the conservation equations can be employed in the analysis. Two dimensionless parameters are found to control the flow structure, namely the spray dilution parameter 1, defined as the mass of liquid fuel per unit mass of gas in the spray stream, and the group vaporization parameter e, defined as the ratio of the characteristic time of spray evolution due to droplet vaporization to the characteristic diffusion time across the jet. It is observed that, for the small values of e often encountered in applications, vaporization occurs only in a thin layer separating the spray from the outer droplet-free stream. This regime of sheath vaporization, which is controlled by heat conduction, is amenable to a simplified asymptotic description, independent of ε,in which the location of the vaporization layer is determined numerically as a free boundary in a parabolic problem involving matching of the separate solutions in the external streams, with appropriate jump conditions obtained from analysis of the quasi-steady vaporization front. Separate consideration of dilute and dense sprays, corresponding, respectively, to the asymptotic limits λ<<1 and λ>>1, enables simplified descriptions to be obtained for the different flow variables, including explicit analytic expressions for the spray penetration distance.

Flamelet structures in spray ignition

In typical liquid-fueled burners the fuel is injected as a high-velocity liquid jet that breaks up to form the spray. The initial heating and vaporization of the liquid fuel rely on the relatively large temperatures of the sourrounding gas, which may include hot combustion products and preheated air. The heat exchange between the liquid and the gas phases is enhanced by droplet dispersion arising from the turbulent motion. Chemical reaction takes place once molecular mixing between the fuel vapor and the oxidizer has occurred in mixing layers separating the spray flow from the hot air stream. Since in most applications the injection velocities are much larger than the premixed-flame propagation velocity, combustion stabilization relies on autoignition of the fuel-oxygen mixture, with the combustion stand-off distance being controlled by the interaction of turbulent transport, droplet heating and vaporization, and gas-phase chemical reactions. In this study, conditions are identified under which analyses of laminar flamelets canshed light on aspects of turbulent spray ignition. This study extends earlier fundamental work by Liñan & Crespo (1976) on ignition in gaseous mixing layers to ignition of sprays. Studies of laminar mixing layers have been found to be instrumental in developing un-derstanding of turbulent combustion (Peters 2000), including the ignition of turbulent gaseous diffusion flames (Mastorakos 2009). For the spray problem at hand, the configuration selected, shown in Figure 1, involves a coflow mixing layer formed between a stream of hot air moving at velocity UA and a monodisperse spray moving at velocity USUA. The boundary-layer approximation will be used below to describe the resulting sl ender flow, which exhibits different igniting behaviors depending on the characteristics of t he fuel. In this approximation, consideration of the case U A = U S enables laminar ignition distances to be related to ignition times of unstrained spray flamelets, thereby pro viding quantitative information of direct applicability in regions of low scala r dissipation-rate in turbulent reactive flows (see the discussion in pp. 181–186 of Peters (2000)) . This report is organized as follows. Effects of droplet dispersion dynamics on ignition of sprays in turbulent mixing layers are discussed in Section 2. The formulation f or ignition in laminar mixing layers is outlined in Sections 3 and 4. The results are presented in Section 5. In Section 6, the mixture-fraction field and associated scalar dissipat ion rates for spray ignition are discussed. Finally, some brief conclusions are drawn in Section 7.

Optimización de la gasificación de lodos de estaciones depuradoras de aguas residuales urbanas para minimizar la formación de alquitranes

La gasificación de lodos de depuración es una alternativa atractiva para generar gases combustibles como H2 y CO. A su vez, estos gases pueden emplearse como materias primas para la obtención de productos químicos orgánicos y combustibles líquidos. Sin embargo, la gasificación no está exenta de problemas como el ligado a la generación de residuos sólidos y alquitrán. El alquitrán en el gas puede ser un inconveniente para emplear el gas como combustible por las obstrucciones y corrosión en los equipos. Dado que las condiciones de gasificación influyen en la producción de alquitrán, este trabajo de investigación se ha centrado en analizar la influencia de parámetros como la temperatura, la carga de alimentación, el tamaño de partícula, el agente gasificante y la utilización de catalizadores en la gasificación en lecho fluidizado de lodos de depuración. Adicionalmente a la medición del efecto de los anteriores parámetros en la producción y composición del alquitrán, también se ha cuantificado su influencia en la producción y composición del gas y en producción del residuo carbonoso. Los resultados muestran que el incremento de la carga de alimentación (kg/h.m2) provoca el descenso de la producción de gas combustible y el incremento del residuo carbonoso y del alquitrán debido a la reducción del tiempo de residencia del gas lo que supone un menor tiempo disponible para las reacciones gas-gas y gas-sólido ligadas a la conversión del alquitrán y del residuo carbonoso en gases combustibles. También se ha comprobado que, el aumento del tamaño de partícula, al incrementar el tiempo de calentamiento de ésta, tiene un efecto similar en los productos de la gasificación que el derivado del incremento en la carga de alimentación. La utilización de una temperatura de gasificación alta (850 ºC), el empleo de aire-vapor como agente gasificante y/o catalizadores primarios como la dolomía consiguen reducir la producción de alquitrán. ABSTRACT Gasification of sewage sludge is an attractive alternative for generating of fuel gases such as H2 and CO. These gases, in turn, can be used as raw materials for the production of organic chemicals and liquid fuel. However, gasification is not without problems as the linked ones to production of char and tar. The tar in the gas can be an inconvenience for to use it as fuel by the problems of blockage and corrosion in the equipments. Since the gasification conditions affect the production of tar, this research has focused on analysing the influence of parameters such as temperature, throughput, the particle size, the gasifying agent and the use of catalysts in the fluidized bed gasification of sewage sludge. In addition to measuring the effect of the above parameters on the production and composition of the tar, it has also been quantified their influence on the yield and composition of the gas and char production. The results show that higher throughput (kg/h.m2) leads to a reduction of fuel gas production and an increase in the production of char and tar, this owes to a lower of gas residence time or what is the same thing less time available for gas-solid and gas-gas reactions attached to the conversion of tar and char to fuel gases. There has also been proven that the rising in particle size, by the increasing heating time of it, has a similar effect in the products of gasification that the results by the rise in the throughput. The applications a high gasification temperature (850 ° C), the use of air-steam as gasifying agent and/or dolomite as primary catalysts are able to reduce the production of tar.

Source terms for calculations of vaporizing and burning fuel sprays with non-unity Lewis numbers in gases with temperature-dependent thermal conductivities

Liquid-fueled burners are used in a number of propulsion devices ranging from internal combustion engines to gas turbines. The structure of spray flames is quite complex and involves a wide range of time and spatial scales in both premixed and non-premixed modes (Williams 1965; Luo et al. 2011). A number of spray-combustion regimes can be observed experimentally in canonical scenarios of practical relevance such as counterflow diffusion flames (Li 1997), as sketched in figure 1, and for which different microscalemodelling strategies are needed. In this study, source terms for the conservation equations are calculated for heating, vaporizing and burning sprays in the single-droplet combustion regime. The present analysis provides extended formulation for source terms, which include non-unity Lewis numbers and variable thermal conductivities.