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一种涡轴发动机系统应急状态快速响应控制方法

陈国强 张海波 严长凯 王健康

陈国强, 张海波, 严长凯, 王健康. 一种涡轴发动机系统应急状态快速响应控制方法[J]. 航空动力学报, 2012, 27(11): 2609-2615.
引用本文: 陈国强, 张海波, 严长凯, 王健康. 一种涡轴发动机系统应急状态快速响应控制方法[J]. 航空动力学报, 2012, 27(11): 2609-2615.
CHEN Guo-qian, ZHANG Hai-bo, YAN Chang-kai, WANG Jian-kang. A new rapid response emergency control method for turbo-shaft engines[J]. Journal of Aerospace Power, 2012, 27(11): 2609-2615.
Citation: CHEN Guo-qian, ZHANG Hai-bo, YAN Chang-kai, WANG Jian-kang. A new rapid response emergency control method for turbo-shaft engines[J]. Journal of Aerospace Power, 2012, 27(11): 2609-2615.

一种涡轴发动机系统应急状态快速响应控制方法

基金项目: 航空科学基金(2010ZB52011); 高校基本科研业务费专项基金(NS2010055)

A new rapid response emergency control method for turbo-shaft engines

  • 摘要: 针对直升机应急状态下特殊快速响应需求,基于涡轮放气原理,提出了一种新的应急状态快速响应控制方法.在应急状态下,除了燃油控制外,同时将涡轮放气量作为发动机控制变量,采用多变量鲁棒方法设计了应急状态直升机/涡轴发动机三变量快速响应控制器,该综合控制方法不仅实现了直升机垂飞通道的控制,而且在保持输出功率通道稳定,即自由涡轮转速恒定的前提下,借助于涡轮放气实现了燃气涡轮转速的闭环控制,有效实现了发动机功率快速跟随能力.最后,以直升机UH-60/涡轴发动机T700综合模型为对象,仿真验证了在直升机应急状态急升-急降过程中,直升机垂飞速度、发动机自由涡轮转速以及燃气涡轮转速跟踪指令的情况,结果表明:相比传统的PID(proportional integration differential)控制,基于快速响应控制方法建立的闭环系统响应迅速,动静态品质良好,能够达到直升机应急状态的特殊设计要求.

     

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出版历程
  • 收稿日期:  2011-11-11
  • 刊出日期:  2012-11-28

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