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Prediction of flammability limits of gas mixtures containing inert gases under variable temperature and pressure conditions

机译:在可变温度和压力条件下预测含有惰性气体的混合气体的可燃极限

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Gas turbines burn a large variety of gaseous fuels under elevated pressure and temperature conditions. During transient operations like maintenance, start-ups or fuel transfers, variable gas/air mixtures flow through the gas piping system and can cause damages in case of ignition. In order to properly control this risk of explosion and ensure safe operation, it is of the essence to have a good knowledge of the flammability limits of the gas mixtures involved, and to be in position to define safe inerting conditions every time it is required. While well-established methods are available in the engineering science to calculate flammability limits of fuel/air mixtures, no systematic methodology exists - to the authors' knowledge - for the prediction of the Lower and Upper Flammability Limits (UFL-LFL) of gaseous blends containing variable amounts of inert components and over a large temperature and pressure range. The purpose of this study was then the evaluation of the LFL and UFL of multi-component fuels in air, in function of pressure, temperature and the concentrations of the most frequently used inerting gases, namely: nitrogen, carbon dioxide and steam. Different prediction criteria proposed in the literature were tested and eventually an original methodology based on the adiabatic flame temperature (T_(ad)) was adopted as criterion and extended to gas mixtures and to high temperatures and pressures. Flame temperatures of different blends were calculated for different initial conditions assuming the access to the chemical equilibrium. Minimum temperature criteria corresponding to the Tad values reached at the LFL and UFL equivalence ratios were deduced from experimental data for each individual combustible molecule. It has been then possible to evaluate the minimum Tad values which ensure flame propagation of fuel blends on the lean and rich sides and to deduce the flammability limits. These calculations were repeated while adding various contents of the three selected inert gases. The methodology was validated by comparison against experimental data when available. The method proves to be simple, accurate, easy to use and applicable to large ranges of pressure, temperature and fuel compositions and to various diluents. The results confirm and quantify some well-known trends of flammability limits, e.g. their widening with increasing initial temperature and pressure, with a stronger effect on UFL than on LFL. The impact of the nature of the inerting gas was also successfully simulated for variable initial conditions and fuel compositions.
机译:燃气轮机在升高的压力和温度条件下燃烧多种气体燃料。在诸如维护,启动或燃料传输之类的过渡运行中,可变的气体/空气混合物流经气体管道系统,并且在起火时会造成损坏。为了适当地控制这种爆炸危险并确保安全运行,至关重要的是要充分了解所涉及气体混合物的可燃性极限,并能在每次需要时确定安全的惰化条件。尽管工程科学中已经建立了完善的方法来计算燃料/空气混合物的可燃极限,但据作者所知,尚没有系统的方法可用于预测气态混合物的上下可燃极限(UFL-LFL)在较大的温度和压力范围内含有可变数量的惰性组分。然后,本研究的目的是根据压力,温度和最常用的惰性气体(即氮气,二氧化碳和蒸汽)的浓度,对空气中多组分燃料的LFL和UFL进行评估。测试了文献中提出的不同预测标准,最终采用了基于绝热火焰温度(T_(ad))的原始方法作为标准,并将其扩展到混合气体以及高温和高压。在达到化学平衡的前提下,针对不同的初始条件计算了不同混合物的火焰温度。从每个单独的可燃分子的实验数据推导出与在LFL和UFL当量比下达到的Tad值相对应的最低温度标准。这样就有可能评估最小的Tad值,以确保燃料混合物在稀薄和浓密的一侧蔓延,并得出可燃性极限。在添加三种选择的惰性气体的各种含量的同时,重复了这些计算。通过与可用的实验数据进行比较来验证该方法。该方法被证明是简单,准确,易于使用的方法,适用于大范围的压力,温度和燃料成分以及各种稀释剂。结果证实并量化了一些易燃极限的众所周知的趋势,例如它们随着初始温度和压力的增加而扩大,对UFL的影响比对LFL的影响更大。还成功地模拟了惰性气体性质对可变初始条件和燃料成分的影响。

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