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Experimental observation and thermodynamic modeling of non-ideal expanding flows of siloxane MDM vapor for ORC applications

机译:用于ORC应用的硅氧烷MDM蒸气非理想膨胀流的实验观察和热力学模型

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This paper reports extensive experimental results characterizing the supersonic expansion of an organic vapor in non-ideal thermodynamic conditions typical of organic Rankine cycle (ORC) turbines. Data are also employed to assess the accuracy of different thermodynamic models used to describe non-ideal expansions.Experiments were carried out on a converging-diverging nozzle test section, where siloxane vapor MDM expanded in the proximity of the saturation curve, the typical operating region of ORC expanders, thus proving the importance of the present investigation for ORC technology. Indeed, detailed experimental data representative of ORC expansions, useful for design tool assessment, were lacking in the open literature up to date.Two nozzles, featuring exit Mach number of 2.0 and 1.5, were tested from highly non-ideal states to dilute gas conditions. The nozzle flow was characterized by measuring total pressure, total temperature and static pressure along the axis. The Mach number was measured at the centerline through schlieren imaging. Vapor expansion was found to be dependent on inlet conditions, thus proving the flow non ideality.State-of-the-art thermodynamic models proved their capability of fully describing the flow non ideality, while simpler and easier to implement equations of state, such as van der Waals, can be acceptable for preliminary expander calculations. (C) 2018 Elsevier Ltd. All rights reserved.
机译:本文报道了广泛的实验结果,这些实验结果表征了有机朗肯循环(ORC)涡轮机在非理想热力学条件下有机蒸气的超音速膨胀。还使用数据评估了用于描述非理想膨胀的不同热力学模型的准确性。实验在收敛-发散喷嘴测试部分进行,其中硅氧烷蒸气MDM在饱和曲线附近(典型工作区域)膨胀ORC扩展器的使用,从而证明了本研究对ORC技术的重要性。的确,迄今为止,公开文献中都缺乏可用于设计工具评估的代表ORC扩展的详细实验数据。已经从高度非理想状态测试了两个喷嘴(出口马赫数分别为2.0和1.5)以稀释气体条件。通过测量沿轴的总压力,总温度和静压力来表征喷嘴流量。通过schlieren成像在中心线测量马赫数。发现蒸汽膨胀取决于入口条件,从而证明了流动非理想状态。最新的热力学模型证明了它们能够充分描述流动非理想状态的能力,同时更容易实现状态方程,例如van der Waals对于初步的膨胀机计算是可以接受的。 (C)2018 Elsevier Ltd.保留所有权利。

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