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On the optimal design of one-rotor two-stages rotary-vane compressors

机译:一转子两级旋转叶片式压缩机的优化设计

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The efficiency increase reachable with more than one compression stage is a well known result of the thermodynamic principles, since this allows the gas cooling between consecutive stages and makes the transformation approach the isothermal limit.In the sliding vane rotary compressors is possible to integrate two stages of compression within a single stator, so to keep down the system dimension and its weight. However, for the specific compressor type at issue, some considerations on the optimization procedure to be followed in the design phase are required. The need of maintaining a fixed pressure level at the discharge port opening, the unavoidable reduction of the swept angle useful for the compression phase in each stage, the necessity of matching vane volumes in the stages with the cooling effect on the gas specific volume and some additional constraints imposed by system design (on the possible stator geometries) offer many theoretical aspect to be deepened, in order to obtain an optimized machine design in terms of thermodynamic efficiency.In the present paper the Authors developed a procedure which permits to define, starting from the choice of free parameters and the ideal performance expected, the optimum design in terms of ideal energy consumption. The procedure is based on a geometric and thermo-fiuid dynamic modeling of the phenomena which occur inside the compressor.
机译:一个以上压缩阶段可达到的效率提高是热力学原理的众所周知的结果,因为这允许在连续的阶段之间进行气体冷却,并使转换接近等温极限。 在滑片中,旋转式压缩机可以将两个压缩阶段集成在单个定子中,从而降低系统尺寸和重量。但是,对于有争议的特定压缩机类型,需要考虑设计阶段要遵循的优化程序。需要在排出口处保持固定的压力水平,不可避免地要减小每个阶段中压缩阶段所用的后掠角,必须使各个阶段中的叶片体积相匹配,并具有对气体比容的冷却效果,以及一些由系统设计(可能的定子几何形状)施加的其他约束条件提供了许多要深化的理论方面,以便在热力学效率方面获得优化的机器设计。 在本文中,作者开发了一种程序,该程序允许从自由参数的选择和预期的理想性能开始,根据理想的能耗来定义最佳设计。该程序基于对压缩机内部发生的现象进行几何和热流体动力学建模。

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