| 航空发动机高空模拟试验进气压力复合控制研究 |
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| 引用本文： | 赵涌,侯敏杰,黄振南,张松,彭炬.航空发动机高空模拟试验进气压力复合控制研究[J].燃气涡轮试验与研究,2010,23(1):37-41. |
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| 作者姓名： | 赵涌 侯敏杰 黄振南 张松 彭炬 |
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| 作者单位： | 1. 中国燃气涡轮研究院,四川,江油,621703
2. 电子科技大学,四川,成都,610054 |
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| 摘 要： | 针对航空发动机高空模拟试验进气压力控制系统动态特性较差的问题，提出在进气压力常规PID反馈控制的基础上．增加按空气流量补偿的前馈控制，构成压力复合控制系统。试验结果证明，所设计的复合控制系统能实现快速度和高精度的统一。
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| 关 键 词： | 核心机 高空模拟试验 复合控制 半物理仿真 |
Research on Aircraft Engine Inlet Pressure Compound Control in Altitude Simulation Test |
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| ZHAO Yong,HOU Min-jie,HUANG Zhen-nan,ZHANG Song,PENG Ju.Research on Aircraft Engine Inlet Pressure Compound Control in Altitude Simulation Test[J].Gas Turbine Experiment and Research,2010,23(1):37-41. |
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| Authors: | ZHAO Yong HOU Min-jie HUANG Zhen-nan ZHANG Song PENG Ju |
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| Institution: | ZHAO Yong1,HOU Min-jie1,HUANG Zhen-nan2,ZHANG Song1,PENG Ju1(1.China Gas Turbine Establishment,Jiangyou 621703,China,2.University of Electronic Science , Technology of China,Chengdu 610054,China) |
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| Abstract: | Aiming at the problem that the inlet pressure control system had an inferior dynamic perfor-mance in aero engine altitude simulation tests,a compound control system based on the combination of the classical PID control strategy and the feed forward control strategy of flow compensation was present-ed in this paper.The results from the hardware-in-the-loop simulation tests indicated a reasonable com-patibility between the speed and the precision by compound control system. |
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| Keywords: | core engine altitude simulating test compound control hardware-in-the-loop simulation(HILS) |
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