| 大流量航空发动机高空模拟进气压力智能与复合控制技术 |
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| 引用本文： | 但志宏,侯敏杰,石小江,张松.大流量航空发动机高空模拟进气压力智能与复合控制技术[J].燃气涡轮试验与研究,2011,24(2):13-16,30. |
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| 作者姓名： | 但志宏 侯敏杰 石小江 张松 |
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| 作者单位： | 1. 南京航空航天大学能源与动力学院,江苏,南京,210016;中国燃气涡轮研究院,四川,江油,621703
2. 中国燃气涡轮研究院,四川,江油,621703 |
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| 基金项目： | 航空基金(20091024007) |
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| 摘 要： | 在航空发动机高空模拟过渡态考核试验中,要同时实现进气压力的稳定和快速控制非常困难.针对系统实际工况及被控对象的特点,本项目成功开展了进气压力智能与复合控制技术专项研究,并进行了关键技术总结.实际结果表明,采用该技术后,进气压力控制系统能实现高精度和快速度的高效统一.
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| 关 键 词： | 航空发动机高空模拟试验 进气压力控制系统 仿人工智能 复合控制 前馈 |
Research of Inlet Pressure Intelligence and Compound Control Technology on Aero-engine Altitude Simulating Tests |
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| DAN Zhi-hong,HOU Min-jie,SHI Xiao-jiang,ZHANG Song.Research of Inlet Pressure Intelligence and Compound Control Technology on Aero-engine Altitude Simulating Tests[J].Gas Turbine Experiment and Research,2011,24(2):13-16,30. |
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| Authors: | DAN Zhi-hong HOU Min-jie SHI Xiao-jiang ZHANG Song |
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| Institution: | DAN Zhi-hong1,2,HOU Min-jie2,SHI Xiao-jiang2,ZHANG Song2(1.College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China,2.China Gas Turbine Establishment,Jiangyou 621703,China) |
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| Abstract: | In aero-engine altitude simulating tests,it is very difficult to control inlet pressure quickly and stably.According to the actual operating conditions and characteristics of inlet pressure control systems,an inlet pressure compound control system is introduced in this paper.It summarized the key technology of the system including the artificial-intelligence control strategy and the compound control strategy,which are based on the combination of the classical PID control strategy and the forward feed contro... |
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| Keywords: | aero-engine altitude simulating test inlet pressure control system artificial intelligence compound control feedforward |
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