首页> 外文期刊>Journal of Engineering for Gas Turbines and Power >An Investigation on the Loss Generation Mechanisms Inside Different Centrifugal Compressor Volutes for Turbochargers
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An Investigation on the Loss Generation Mechanisms Inside Different Centrifugal Compressor Volutes for Turbochargers

机译:涡轮增压器不同离心压缩机蜗壳内部的损耗机理研究

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In centrifugal compressor design, the volute plays a key role in defining the overall efficiency and operating range of the stage. The flow at the impeller outlet is indeed characterized by a high kinetic energy content, which is first converted to potential energy in the diffuser downstream. The compressed gas is then collected by the volute at the cylindrical outlet section of the diffuser and directed to the intake piping, possibly with a further pressure recovery to enhance the stage performance. Due to the high flow speed at the volute inlet, the capability of ensuring the lowest amount of total pressure loss is pivotal to prevent a detriment of the machine efficiency. Moreover, the flow conditions change when the volute operates far from its design point: at mass flow rates lower than the design one, the flow becomes diffusive, while at higher mass flow rates the fluid is accelerated, thus leading to different loss-generation mechanisms. These phenomena are particularly relevant in turbocharger applications, where the compressor needs to cover a wide functioning range; moreover, in these applications, the definition of the volute shape is often driven also by space limitations imposed by the vehicle layout, leading to a variety of volute types. The present paper reports an analysis on the sources of thermodynamic irreversibilities occurring inside different volutes applied to a centrifugal compressor for turbocharging applications. Three demonstrative geometrical configurations are analyzed by means of three- dimensional (3D) numerical simulations using common boundary conditions to assess the overall volute performance and different loss mechanisms, which are evaluated in terms of the local entropy generation rate. The modification of the loss mechanisms in off-design conditions is also accounted for by investigating different mass flow rates. It is finally shown that the use of the entropy generation rate for the assessment of the irreversibilities is helpful to understand and localize the sources of loss in relation to the various flow structures.
机译:在离心压缩机的设计中,蜗壳在确定级的整体效率和工作范围方面起着关键作用。叶轮出口处的流动确实具有高动能含量的特征,该动能含量首先在下游的扩散器中转化为势能。然后,压缩气体通过蜗壳收集在扩散器的圆柱形出口部分,并被引导至进气管道,可能还会进行进一步的压力回收,以提高级性能。由于蜗壳入口处的高流速,确保最低总压力损失的能力至关重要,以防止损害机器效率。此外,当蜗壳远离其设计点运行时,流动条件也会发生变化:当质量流量低于设计流量时,流量会扩散,而当质量流量高于设计流量时,流体会加速流动,从而导致产生不同的损失的机理。这些现象在涡轮增压器应用中尤为重要,在这种应用中,压缩机需要涵盖广泛的功能范围;此外,在这些应用中,蜗壳形状的定义通常也受到车辆布局所施加的空间限制的驱动,从而导致多种蜗壳类型。本文报告了对应用于涡轮增压应用的离心压缩机的不同蜗壳内部发生的热力学不可逆性来源的分析。通过使用共同边界条件的三维(3D)数值模拟,分析了三个演示性几何构型,以评估整体蜗壳性能和不同的损失机制,并根据局部熵产生率对其进行了评估。通过研究不同的质量流率,也可以解决非设计条件下损失机理的修改。最终表明,使用熵产生率评估不可逆性有助于理解和定位与各种流动结构有关的损失源。

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