热能动力工程2024,Vol.39Issue(9) :162-169.DOI:10.16146/j.cnki.rndlgc.2024.09.019

基于遗传算法的超临界CO2压缩机防喘振自抗扰控制

Anti-surge ADRC of Supercritical CO2 Compressor based on Genetic Algorithm

孙韬志 曹越 司风琪
热能动力工程2024,Vol.39Issue(9) :162-169.DOI:10.16146/j.cnki.rndlgc.2024.09.019

基于遗传算法的超临界CO2压缩机防喘振自抗扰控制

Anti-surge ADRC of Supercritical CO2 Compressor based on Genetic Algorithm

孙韬志 1曹越 1司风琪1
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作者信息

  • 1. 东南大学能源热转换及其过程测控教育部重点实验室,江苏南京 210096
  • 折叠

摘要

在超临界CO2压缩机运行过程中,可转导叶工作状态随压缩机转速等状态变量频繁变化,会引起压缩机喘振,严重时会导致压缩机设备损坏.针对此问题,本文采取了一种基于遗传算法的防喘振自抗扰控制方法.该方法在压气机出口处设置防喘振阀控制喘振,通过遗传算法整定自抗扰控制器,使防喘振阀的开度随转速等状态变量的变化而相应变化,进而改变出口压力,使压缩机工作在平衡点.仿真结果表明:遗传算法优化后的自抗扰控制器防喘振控制效果更优,调节时间缩短了 20%~33%,超调量减小了 30%~45%,使控制过程更加平滑,能够在稳定转速的同时抑制扰动.

Abstract

During the operation of supercritical CO2 compressor,the working state of adjustable guide vane changed frequently with the compressor speed and other state variables,which will cause the com-pressor to surge,and in serious cases the compressor equipment will be damaged.To solve this problem,this paper adopted an anti-surge auto disturbance rejection control(ADRC)method based on genetic al-gorithm.This method set up an anti-surge valve at the outlet of the compressor to control surge,and used a genetic algorithm to tune the auto-disturbance rejection controller,so that the opening of the anti-surge valve changed accordingly with changes in state variables such as speed.The opening of the anti-surge valve changed the outlet pressure,allowing the compressor to operate at the equilibrium point.The simu-lation results show that the auto disturbance rejection controller optimized by genetic algorithm has better anti surge control effect,with a shortened adjustment time of 20%to 33%and a reduced overshoot of 30%to 45%,making the control process smoother and able to stabilize the speed while suppressing dis-turbances.

关键词

超临界CO2压缩机/喘振/遗传算法/自抗扰控制

Key words

supercritical CO2 compressor/surge/genetic algorithm/auto disturbance rejection control(ADRC)

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基金项目

国家自然科学基金(52206006)

江苏省基础研究计划(自然科学基金)青年基金项目(BK20210240)

出版年

2024
热能动力工程
中国 哈尔滨 第七0三研究所

热能动力工程

CSTPCDCSCD北大核心
影响因子:0.345
ISSN:1001-2060
参考文献量15
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