| 航空发动机加力过渡过程数控研究 |
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| 引用本文： | 张辉,陶涛,张加桢.航空发动机加力过渡过程数控研究[J].航空动力学报,1997,12(1):98-100,112. |
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| 作者姓名： | 张辉 陶涛 张加桢 |
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| 作者单位： | 航空系统工程研究所，西北工业大学 |
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| 摘 要： | 研究航空发动机接通加力过程中的控制问题，即研究在接通加力过程中，如何协调好加力供油量与尾喷口面积之间的变化关系，使得这一过程尽量不影响主发动机的工作状态，以保证发动机安全稳定的工作
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| 关 键 词： | 航空发动机 燃烧室 过渡过程 控制问题 |
| 收稿时间： | 1/1/1996 12:00:00 AM |
| 修稿时间： | 4/1/1996 12:00:00 AM |
STUDY ON DIGITAL CONTROL OF ENGINE REHEAT TRANSIENT PROCESS |
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| Zhang Hui,Tao Tao and Zhang Jiazhen.STUDY ON DIGITAL CONTROL OF ENGINE REHEAT TRANSIENT PROCESS[J].Journal of Aerospace Power,1997,12(1):98-100,112. |
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| Authors: | Zhang Hui Tao Tao and Zhang Jiazhen |
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| Institution: | China Institute of Aeronautics System Engineering, Beijing 100012;7th Dept.Northwestern Polytechnical University, Xi'an 710072;7th Dept.Northwestern Polytechnical University, Xi'an 710072 |
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| Abstract: | The emphasis of this study is laid on designing a reheat-starting transient control subsystem of an aeroengine,after the main fuel control system of the engine has been designed.That is to say,the study pursued to the reheat-starting transient control method,which can coordinate the changes of the reheat fuel supply and the nozzle area,so the reheat-starting transient process does not affect the regimes of the core engine as possible,so that the engine can work safely and steadily.The optimal control method is employed with success. |
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| Keywords: | Afterburners Transient process Control problems |
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