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    基于正交设计的压缩空气储能系统效率分析

    Analysis on Exergy Efficiency of a Compressed-air Energy Storage System Based on Orthogonal Design

    • 摘要: 根据压缩空气储能系统的结构特性,采用正交设计和数值模拟方法对压缩空气储能系统的压缩机绝热(火用)效率、级间冷却温度、储气室最低工作压力、回热度、膨胀透平绝热(火用)效率和燃烧室(火用)效率等6个参数进行实验设计和数值模拟,并对模拟结果进行(火用)效率分析.通过对实验结果的方差进行分析,得到设计参数对系统(火用)效率的影响程度.结果表明:在压缩空气储能系统中,压缩机绝热(火用)效率、级间冷却温度、回热度、压缩机绝热(火用)效率与级间冷却温度的交互作用、级间冷却温度与回热度的交互作用以及压缩机绝热(火用)效率与膨胀透平绝热(火用)效率之间的交互作用为影响压缩空气储能系统总过程(火用)效率的显著因素;在现有技术水平下,降低压缩机级间冷却温度和提高回热度是提高压缩空气储能系统(火用)效率的最佳选择.

       

      Abstract: According to structural features of a compressed-air energy storage (CAES) system, six parameters of the system were experimentally designed and numerically simulated based on orthogonal method, such as the compressor adiabatic efficiency, inter-stage cooling temperature, minimum operating pressure of storage volume, regenerator effectiveness, expansion turbine adiabatic efficiency and combustion chamber efficiency etc., and subsequently an exergy analysis was conducted to the simulation results, while an analysis of variance was carried out to the experimental results to study the effects of above design parameters on the exergy efficiency of the system. Results show that the exergy efficiency of CAES system is mainly affected by the significant parameters, such as the compressor adiabatic efficiency, the inter-stage cooling temperature, the regenerator effectiveness, as well as the interactions between the compressor adiabatic efficiency and inter-stage cooling temperature, the inter-stage cooling temperature and regenerator effectiveness, and between the compressor adiabatic efficiency and expansion turbine adiabatic efficiency, etc. Under present condition of technology, the exergy efficiency of CAES system can be improved by reducing the inter-stage cooling temperature and increasing the regenerator effectiveness.

       

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