Evaluación de la sustitucion parcial o total de aceite de palma (Elaeis guinensis) por aceite de fritura como fuente de energía en la ración alimenticia de pollos de engorde

La presente investigación estuvo dirigida a determinar la viabilidad, que sobre el desempeño productivo del pollo de engorde, podía ejercer la sustitución parcial o total del porcentaje de aceite de palma (Elaeís guínensis, Jacq) por aceite de fritura como fuente de energía en la ración alimenticia. La sustitución parcial o total se hizo con base en el 6% de aceite que se incluye en la fórmula alimenticia, ajustada a los requerimientos de los pollos de engorde. El ensayo experimental fue realizado en la granja avícola "La Trinidad", propiedad de la empresa TIP-TOP INDUSTRIAL S.A. Se utilizaron 700 pollos de engorde para producción comercial, del híbrido Peterson-Hubbard, de un día de edad y mantenidos en evaluación durante un periodo de 42 días. Estos fueron distribuidos aleatoriamente en cuatro tratamientos, conformados cada uno de cinco unidades experimentales, y éstas a su vez con 35 pollos cada una, quedando de la forma siguiente: Tratamiento T1 (testigo): 6% aceite de palma; tratamiento T2 : 2% aceite de palma y 4% aceite de fritura; tratamiento T3: 1% aceite de palma y 5% aceite de fritura; tratamiento T4 : 6% aceite de fritura. El resto de los ingredientes que conformó la dieta alimenticia fue igual para todos los tratamientos; así como también el manejo de los pollos se realizó al igual que lo hace la Empresa para toda su producción. Las variables estudiadas fueron consumo de alimento, peso vivo final y conversión de alimento. Los resultados obtenidos a partir de estas variables fueron analizados a través de un Diseño Completamente Aleatorio y sometidos a la Prueba de Tukey, el que proporcionó la superioridad existente entre tratamientos. Se encontraron diferencias significativas (p<0.05) entre tratamientos para la variable conversión alimenticia, con índices de conversión para el final de período experimental, de 1.8050, 1.7829, 1.7550 y 1.7310 para los tratamientos T1, T2, T3 y T4, respectivamente. Las variables consumo acumulado de alimento y peso vivo final no presentaron diferencias estadísticas a un nivel de significancia de p<0.05. El análisis financiero demostró que el tratamiento T4 tiene un menor costo de alimentación, siendo este de C$3.35/kg peso vivo. Encontrándose los tratamientos T1.T2 y T3 con costos de C$3.8210, C$3.5624; y C$3.4527/kg peso vivo, respectivamente. El mayor beneficio neto por kilogramo de peso vivo lo obtuvo el tratamiento T4, con C$0.47. Siendo el beneficio neto para los tratamientos T2 y T3 de C$0.26 y C$ 0.37, respectivamente. La mortalidad presentada por los tratamientos T1, T2, T3, y T4 para el final del período experimental fue de 5.13, 3.99, 2.85 y 3.99 (%), respectivamente.

Efecto de distintos intervalos de mediciones de leche sobre la estimación de producción de leche total, repetibilidad y la forma de la curva de lactancia en un hato reyna

El presente trabajo se realizó con el objetivo de estudiar el efecto de cuatro intervalos de medición de leche (diario, cada 7, 14 y 28 días) sobre la producción de leche total, la repetibilidad y la forma de la curva de lactancia. Para lo cual se utilizaron los registros productivos y reproductivos del hato criollo Reyna de la Finca San José ubicada en Masatepe, Nicaragua. Se estudiaron 105 lactancia provenientes de 28 vacas durante el periodo de 1982 - 1990. Las características estudiadas fueron PLTOT, repetibilidad y la forma de la curva de lactancia. Todos los análisis estadísticos fueron realizados con el procedimiento de mínimos cuadrados y máxima verosimilitud establecido en el paquete estadístico LSMLMW total, obteniéndose las siguientes medias de mínimos cuadrados: 1,655.23±77.79 para el tratamiento 1 total. Los valores encontrados para los indices de Repetibilidad para cada uno de los tratamientos fueron de: 0.46±0.11, 0.50±0.11, 0.48±0.11 y 0.50±0.11 para los tratamientos 1, 2, 3, 4 respectivamente Los valores para los parámetros y variables estudias en la curva de la lactancia fueron 3.2±2.5, 0.47±0.32, 0.01± 0.06, 51.81±29.10, 9.45±3.49 y 6.97±1.02 para a, b, c, Tp, Rp y S respectivamente Al estudiar el efecto de los tratamiento sobre las variables y parámetros de la curva de lactancia se determino que solamente la variable (S) que determina la persistencia fue afectada significativamente

An Experimental Study of Kerosene Combustion in a Supersonic Model Combustor Using Effervescent Atomization

Investigation of kerosene combustion in a Mach 2.5 flow was carried out using a model supersonic combustor with cross-section area of 51 mm × 70 mm and different integrated fuel injector/flameholder cavity modules. Experiments with pure liquid atomization and with effervescent atomization were characterized and compared. Direct photography, Schlieren imaging, and planar laser induced fluorescence (PLIF) imaging of OH radical were utilized to examine the cavity characteristics and spray structure. Schlieren images illustrate the effectiveness of gas barbotage in facilitating atomization and the importance of secondary atomization when kerosene sprays interacting with a supersonic crossflow. OH PLIF images further substantiate our previous finding that there exists a local high-temperature radical pool within the cavity flameholder, and this radical pool plays a crucial role in promoting kerosene combustion in a supersonic combustor. Under the same operation conditions, comparison of the measured static pressure distributions along the combustor also shows that effervescent atomization generally leads to better combustion performance than the use of pure liquid atomization. Furthermore, the present results demonstrate that the cavity characteristics can be different in non-reacting and reacting supersonic flows. As such, the conventional definition of cavity characteristics based on non-reacting flows needs to be revised.

Pulverized-coal combustion in Wall-Protecting-Jets combustor (WPJC)

A new type of pulverized-coal combustor, called "Wall-Protecting-Jets Combustor" (hereafter, WPJC has been proposed, designed and studied with both CFD (Computational Fluid Dynamics) and experimental methods. The WPJC is based on a novel concept in which all inlet jets are along the combustor wall. Pilot combustion experiments were conducted to investigate the combustion performance of WPJC. Two-phase flows and pulverized-coal combustion were simulated to study the mechanism of),WPJC using the commercial software FLUENT. The results show that the WPJC has many remarkable advantages: wall-protection by the cold jets without the use of refractory materials; low-temperature and three-stage combustion with low NOx emission; negligible ash/slag-deposition; multiple functions with convenient switching between them; effective adjustment of the combustion intensity and the ignition position.

Investigation of Vaporized Kerosene Injection and Combustion in a Supersonic Model Combustor

Injection and combustion of vaporized kerosene was experimentally investigated in a Mach 2.5 model combustor at various fuel temperatures and injection pressures. A unique kerosene heating and delivery system, which can prepare heated kerosene up to 820 K at a pressure of 5.5 MPa with negligible fuel coking, was developed. A three-species surrogate was employed to simulate the thermophysical properties of kerosene. The calculated thermophysical properties of surrogate provided insight into the fuel flow control in experiments. Kerosene jet structures at various preheat temperatures injecting into both quiescent environment and a Mach 2.5 crossflow were characterized. It was shown that the use ofvaporized kerosene injection holds the potential of enhancing fuel-air mixing and promoting overall burning. Supersonic combustion tests further confirmed the preceding conjecture by comparing the combustor performances of supercritical kerosene with those of liquid kerosene and effervescent atomization with hydrogen barbotage. Under the similar flow conditions and overall kerosene equivalence ratios, experimental results illustrated that the combustion efficiency of supercritical kerosene increased approximately 10-15% over that of liquid kerosene, which was comparable to that of effervescent atomization.

超临界煤油超声速燃烧特性实验 Experiments on Supersonic Combustion of Supercritical Kerosene

针对各种温度、压力下，马赫数2．5流场中超临界煤油的超声速燃烧性能进行了实验研究。研制并测试了一个新型二级煤油加热系统，该系统能够把0．8kg的煤油在5．5MPa压力下加热至至950K而不产生严重的结碳。超声速燃烧试验表明，在相同的来流和燃料当量比条件下，超临界煤油的燃烧效率比室温煤油提高10％～15％，与氢气泡雾化的燃烧效率相当。

Constant volume combustion of aluminum and cornstarch dust in microgravity

The subject of the present work is to report an experimental comparative study of the effect of dispersion-induced turbulence on dust combustion in constant volume vessel, carried out both in normal gravity and in microgravity environment. Dispersion system with small scale of turbulence, creating uniform homogeneous mixture, was used in experiments. To improve reproducibility of the explosion data an ignitor of small energy, with local soft ignition was developed. Both factors contributed to acquisition of more reproducible experimental data. In experiments under microgravity conditions a dust suspension during combustion remains constant. This makes possible to study dust explosion under stationary dust suspension without influence of turbulence.

Multiplex CARS measurements in supersonic H-2/air combustion

H-2 and O-2 multiplex coherent anti-stokes Raman spectroscopy (CARS) employing a single dye laser has been explored to simultaneously determine the temperature and concentrations of H-2 and O-2 in a hydrogen-fueled supersonic combustor. Systematic calibrations were performed through a well-characterized H-2/air premixed flat-flame burner. In particular, temperature measurement was accomplished using the intensity ratio of the H-2 S(5) and S(6) rotational lines, whereas extraction of the H-2 and O-2 concentrations was obtained from the H-2 S(6) and O-2 Q-branch, respectively. Details of the calibration procedure and data reduction are discussed. Quantification of the supersonic mixing and combustion characteristics applying the present technique has been demonstrated to be feasible. The associated detection limits as well as possible improvements are also identified.

Revelation of a Functional Dependence of the Sum of Two Uniaxial Strengths/Hardness on Elastic Work/Total Work of Indentation

Dimensional and finite element analyses were used to analyze the relationship between the mechanical properties and instrumented indentation response of materials. Results revealed the existence of a functional dependence of (engineering yield strength sigma(E,y) + engineering tensile strength sigma(E,b))/Oliver & Pharr hardness on the ratio of reversible elastic work to total work obtained from an indentation test. The relationship links up the Oliver & Pharr hardness with the material strengths, although the Oliver & Pharr hardness may deviate from the true hardness when sinking in or piling up occurs. The functional relationship can further be used to estimate the SUM sigma(E,y) + sigma(E,b) according to the data of an instrumented indentation test. The sigma(E,y) + sigma(E,b) value better reflects the strength of a material compared to the hardness value alone. The method was shown to be effective when applied to aluminum alloys. The relationship can further be used to estimate the fatigue limits, which are usually obtained from macroscopic fatigue tests in different modes.

Damage of a high-energy solid propellant and its effects on combustion

In order to improve the safety of high-energy solid propellants, a study is carried out for the effects of damage on the combustion of the NEPE (Nitrate Ester Plasticized Polyether) propellant. The study includes: (1) to introduce damage into the propellants by means of a large-scale drop-weight apparatus; (2) to observe microstructural variations of the propellant with a scanning electron microscope (SEM) and then to characterize the damage with density measurements; (3) to investigate thermal decomposition; (4) to carry out closed-bomb tests. The NEPE propellant can be considered as a viscoelastic material. The matrices of damaged samples axe severely degraded, but the particles are not. The results of the thermal decomposition and closed-bomb tests show that the microstructural damage in the propellant affects its decomposition and burn rate.

Measurements of thermal radiation in ultralight metal foams with open cells

Highly porous ultralightweight cellular metal foams with open cells have attractive mechanical, thermal, acoustic and other properties and are currently being exploited for high-temperature applications (e.g. acoustic liners for combustion chambers). In such circumstances, thermal radiation in the metal foam becomes a significant mechanism of heat transfer. This paper presents results from experimental measurements on radiative transfer in Fe-Cr-Al-Y (a steel-based high-temperature alloy) foams having high porosity (95 per cent) and different cell sizes, manufactured at low cost from the sintering route. The spectral transmittance and reflectance are measured at different infrared wavelengths ranging from 2.5 to 50 μm, which are subsequently used to determine the extinction coefficient and foam emissivity. The results show that the spectral quantities are strongly dependent on the wavelength, particularly in the short-wavelength regime (less than 25 μm). While the extinction coefficient decreases with increasing cell size, the effect of cell size on foam reflectance is not significant. When the temperature is increased, the total extinction coefficient increases but the total reflectance decreases. The effective radiative conductivity of the metal foam is obtained by using the guarded hot-plate apparatus. With the porosity fixed, the effective radiative conductivity increases with increasing cell size and increasing temperature. © IMechE 2004.

Simulation of Coal Combustion by AUSM Turbulence-Chemistry Char Combustion Model and a Full Two-Fluid Model

An algebraic unified second-order moment (AUSM) turbulence-chemistry model of char combustion is introduced in this paper, to calculate the effect of particle temperature fluctuation on char combustion. The AUSM model is used to simulate gas-particle flows, in coal combustion in a pulverized coal combustor, together with a full two-fluid model for reacting gas-particle flows and coal combustion, including the sub-models as the k-epsilon-k(p) two-phase turbulence niodel, the EBU-Arrhenius volatile and CO combustion model, and the six-flux radiation model. A new method for calculating particle mass flow rate is also used in this model to correct particle outflow rate and mass flow rate for inside sections, which can obey the principle of mass conservation for the particle phase and can also speed up the iterating convergence of the computation procedure effectively. The simulation results indicate that, the AUSM char combustion model is more preferable to the old char combustion model, since the later totally eliminate the influence of particle temperature fluctuation on char combustion rate.