| 飞机地面模拟试验反推力电液加载系统的实现 |
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| 引用本文： | 施光林,泮健.飞机地面模拟试验反推力电液加载系统的实现[J].中国机械工程,2010(1). |
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| 作者姓名： | 施光林 泮健 |
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| 作者单位： | 上海交通大学; |
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| 摘 要： | 介绍了一种专用于飞机地面模拟气动加载试验的电液伺服系统;详细分析了该电液伺服加载系统的结构与特点;重点叙述了系统的具体控制策略;分别给出了在终止反推状态、正常着落状态和收回状态下的试验结果。试验结果表明,所研究的反推力电液伺服加载系统的动态力跟踪误差不大于15%,达到了工程实际应用的目的。
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| 关 键 词： | 飞机 地面模拟 反推力 电液伺服加载系统 动态力跟踪误差 |
Electro-hydraulic Force Servo System for Simulating Thrust in Reverse of Experimental Systems on the Ground for Airplane |
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| Shi Guanglin Pan JianShanghai Jiao Tong University,Shanghai.Electro-hydraulic Force Servo System for Simulating Thrust in Reverse of Experimental Systems on the Ground for Airplane[J].China Mechanical Engineering,2010(1). |
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| Authors: | Shi Guanglin Pan JianShanghai Jiao Tong University Shanghai |
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| Affiliation: | Shi Guanglin Pan JianShanghai Jiao Tong University,Shanghai,200240 |
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| Abstract: | The electro-hydraulic force servo system was introduced, which was used to give force to a certain kind of airplane during its experiments on the ground.The characteristics and structure of this electro-hydraulic force servo system was analyzed in detail. The control strategy of the system was emphasized on, and the experimental results of stop mode, normal mode and back mode were also given respectively. The experimental results show that the dynamic trace error of this electro-hydraulic force servo system... |
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| Keywords: | airplane simulation on the ground thrust in reverse electro-hydraulic force servo system dynamic force track error |
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