| 航空发动机整机稳态动力响应计算 |
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| 引用本文： | 任兴民,顾家柳.航空发动机整机稳态动力响应计算[J].航空学报,1997,18(5):625-626. |
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| 作者姓名： | 任兴民 顾家柳 |
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| 作者单位： | 西北工业大学振动工程研究所, 西安, 710072 |
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| 摘 要： | 建立了静子与转子部分的数学模型，提出了借实测的安装节动刚度，计算各主轴承到安装节的传递函数和转子系统的动力响应，进而预计发动机整机稳态动力响应的方法。附有一双转子航空发动机计算实例。
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| 关 键 词： | 航空发动机 稳态响应 动刚度测量 |
| 收稿时间： | 1997-01-15 |
| 修稿时间： | 1997-04-15 |
CALCULATION OF STEADY STATE DYNAMIC RESPONSE OF AEROENGINE |
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| Ren Xingmin,Gu Jialiu.CALCULATION OF STEADY STATE DYNAMIC RESPONSE OF AEROENGINE[J].Acta Aeronautica et Astronautica Sinica,1997,18(5):625-626. |
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| Authors: | Ren Xingmin Gu Jialiu |
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| Institution: | Institute of Vibration Engineering, Northwestern Polytechnical University, Xian, 710072 |
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| Abstract: | A mathematical model of rotor and stator is given. A calculation method is established to calculate the dynamic response of engines mounting points by using the measured dynamic stiffness of the mounting points. Both the dynamic response of rotor stator system and the transfer function between main supports and mounting points can be calculated simultaneously. Finally, a certain type of double spool aeroengine is taken as an example. |
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| Keywords: | aeroengine steady state response measurement of dynamic stiffness |
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