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Modeling wing tank flammability.

机译:模拟翼舱可燃性。

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An investigation into the fire safety of a wing fuel tank has been performed to aid in the effort to eliminate or reduce the possibility of a wing fuel tank explosion in a commercial aircraft. A computational model is built to predict the generation of flammable mixtures in the ullage of wing fuel tanks. The model predicts the flammability evolution within the tank based on in-flight conditions of a wing fuel tank. The model is validated through supporting experiments performed in an altitude chamber, the wind tunnel facility as well as data obtained from flight tests. The results from the experiments are compared to the computational results. Computational results from the altitude chamber follow the general trend of the experimental results, but produce them at a different flash point. This is due to the replenishment of species with lower flash point at the surface of the fuel which emulates the flash point of the entire fuel to be lower. Experimental results for the aluminum wing tests from the wind tunnel experiments are in good agreement with the computational results as well.;A simpler model is developed from a program that calculates fuel air ratio within the ullage of fuel tanks in order to reduce the required number of inputs to the model. This model is applied to the data sets for the experiments performed in the altitude chamber and wind tunnel. For the tests conducted in the altitude chamber, the correlation estimates the hydrocarbon concentrations extremely well during ascent and descent. During the on-ground condition the estimation is good, but not as accurate as the ascent or descent conditions. For the tests conducted in the wind tunnel, the computational values follow the general trend of the experimental values, but the computational values estimates the total hydrocarbon concentration approximately 10% lower than the experimental value consistently.;Flammability studies are also performed in order to track the effects of temperature, pressure, and oxygen concentration on the upper and lower flammability limits. For the temperature and pressure profiles considered in this work, it is found that the temperature and pressure effects on the flammability limits are minimal. In contrast, the oxygen concentration has a significant effect on the flammability limits of the vapor; the flammable region narrows with a decrease in oxygen concentration.
机译:已经进行了对机翼燃料箱的防火安全性的研究,以帮助消除或减少商用飞机中机翼燃料箱爆炸的可能性。建立一个计算模型来预测机翼燃油箱缺损时易燃混合物的产生。该模型根据机翼燃油箱的飞行条件预测燃油箱内的可燃性演变。该模型通过在高空舱,风洞设施中进行的辅助实验以及从飞行测试中获得的数据进行了验证。将实验结果与计算结果进行比较。来自高空反应室的计算结果遵循实验结果的总体趋势,但是在不同的闪点产生它们。这是由于补充了在燃料表面具有较低闪点的物质,从​​而使整个燃料的闪点更低。风洞实验得到的铝翼试验的实验结果也与计算结果非常吻合。;从一个程序中开发了一个更简单的模型,该程序可以计算燃料箱余量内的燃料空气比,从而减少所需数量模型的输入。该模型被应用于在高空舱和风洞中进行的实验的数据集。对于在高空舱中进行的测试,相关性非常好地估计了上升和下降期间的碳氢化合物浓度。在地面条件下,估算是好的,但不如上升或下降条件准确。对于在风洞中进行的测试,计算值遵循实验值的总体趋势,但是计算值估计总烃浓度始终比实验值低约10%.;还进行了易燃性研究以追踪温度,压力和氧气浓度对可燃性上限和下限的影响。对于这项工作中考虑的温度和压力曲线,发现温度和压力对可燃性极限的影响最小。相反,氧浓度对蒸气的可燃性极限有显着影响。易燃区域随着氧气浓度的降低而变窄。

著录项

  • 作者

    Dadia, Dhaval D.;

  • 作者单位

    Rutgers The State University of New Jersey - New Brunswick.;

  • 授予单位 Rutgers The State University of New Jersey - New Brunswick.;
  • 学科 Engineering Mechanical.
  • 学位 M.S.
  • 年度 2009
  • 页码 116 p.
  • 总页数 116
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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