32 research outputs found

    ICES 2005-1031 RAILPLUG DESIGN OPTIMIZATION TO IMPROVE LARGE-BORE NATURAL GAS ENGINE PERFORMANCE

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    ABSTRACT It is a very challenging problem to reliably ignite extremely lean mixtures, especially for the low speed, high load conditions of stationary large-bore natural gas engines. If these engines are to be used for the distributed power generation market, it will require operation with higher boost pressures and even leaner mixtures. Both place greater demands on the ignition system. The railplug is a very promising ignition system for lean burn natural gas engines with its high-energy deposition and high velocity plasma jet. High-speed photography was used to study the dis charge process. A heat transfer model is proposed to aid the railplug design. A parameter study was performed both in a constant volume bomb and in an operating natural gas engine to improve and optimize the railplug designs. The engine test results show that the newly designed railplugs can ensure the ignition of very lean natural gas mixtures and extend the lean stability limit significantly. The new railplug designs also improve durability. INTRODUCTION Over the past few years, industry and government have jointed together to develop high efficiency, low emissions, large-bore natural gas fueled stationary engines for either natural gas transportation or power generation. They have targeted fuel efficiency at over 50%, NO x emissions as low as 0.01 gm/BHP-hr, and decreasing maintenance costs by 10% [1]. This will require operation with higher boost pressures and even leaner mixtures. Both place greater demands on the ignition system

    Hakan Ertürk The Application of an Inverse Formulation in the Design of Boundary Conditions for Transient Radiating Enclosures

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    This study considers the design of thermal systems that are built to radiatively heat objects from a specified initial condition to a specified steady state following a prescribed temperature history

    Treatment of Design Fire Uncertainty using Quadrature Method of Moments

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    The use of a single design fire in a performance based fire design code typically fails to account for the inherent uncertainty in knowledge of the future use of the space. Uncertainties in knowledge of intended use and the implications in terms of fuel loading and potential heat release rate can be bounded using probabilistic methods. Use of a cumulative distribution function (CDF) and the related probability density function (PDF) specify the best available estimate of the probability (likelihood) of a fire of given size to take place in a compartment. Monte Carlo simulation is a widely used computational method for treating uncertainty that might be described by a PDF . In this technique, one samples the uncertain variables from their underlying PDFs and runs a fire model for each sample. For complex fire models, this approach may be computationally intractable. In this work we present a computationally efficient technique called the Quadrature Method of Moments (QMOM) for propagating uncertainty bound in distributions. In QMOM one solves for only the moments of a relevant uncertain parameter. The cumulative distribution function (CDF) of the uncertain parameter provides all the statistical information required for risk assessments. We consider a simplified propagation of uncertainty problem. Results using both the ASET and CFAST fire models indicate that computation of the moments of the PDF using QMOM and the reconstruction of the CDF by matching the moments with those of a 4-parameter Generalized Lambda Distribution (GLD) give accurate results at a significantly smaller computational cost

    Extension of the PECOS Quasi-steady Ablation Toolkit for Uncertainty Propagation

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    Low-order models are quite useful for sensitivity analysis and design. This work details work done on adding complementary pieces to the PECOS low-order, quasi-steady-state ablation model to facilitate uncertainty propagation. The PECOS quasi-steady state ablation model is a one-dimensional, quasi-steady-state, algebraic ablation model that uses finite-rate surface chemistry and equilibrium pyrolysis-gas-production submodels to predict surface recession rate. The material response model is coupled to a film-transfer boundary layer model to enable the computation of heat and mass transfer from an ablating surface. For comparison to arc jet data, a simple shock heated gas model is coupled. A coupled model consisting of submodels for the shock heated gases, film heat and mass transfer, and material response is exercised against recession rate data for surface and in-depth ablators. Comparisons are made between the quasi-state-state ablation model and the unsteady ablation code, Chaleur, as well as to other computations for a graphite ablator in arcjet facilities. The simple models are found to compare reasonably well to both the experimental results and the other calculations. Uncertainty propagation using a moment based methods is presented. The method is applied to a number of simplified sample problems, for both univariate and multivariate scenarios. The results of this study are discussed, and conclusions about the utility of the method as well as the properties of the ablation code are drawn

    Thermoplastic Polyurethane Elastomer Nanocomposites: Morphology, Thermophysical, and Flammability Properties

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    Novel materials based on nanotechnology creating nontraditional ablators are rapidly changing the technology base for thermal protection systems. Formulations with the addition of nanoclays and carbon nanofibers in a neat thermoplastic polyurethane elastomer (TPU) were melt-compounded using twin-screw extrusion. The TPU nanocomposites (TPUNs) are proposed to replace Kevlar-filled ethylene-propylene-diene-monomer rubber, the current state-of-the-art solid rocket motor internal insulation. Scanning electron microscopy analysis was conducted to study the char characteristics of the TPUNs at elevated temperatures. Specimens were examined to analyze the morphological microstructure during the pyrolysis reaction and in fully charred states. Thermophysical properties of density, specific heat capacity, thermal diffusivity, and thermal conductivity of the different TPUN compositions were determined. To identify dual usage of these novel materials, cone calorimetry was employed to study the flammability properties of these TPUNs
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