| 直升机振动与减振特性分析 |
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| 引用本文： | 柳文林,穆志韬,段成美.直升机振动与减振特性分析[J].海军航空工程学院学报,2004,19(5):533-536. |
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| 作者姓名： | 柳文林 穆志韬 段成美 |
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| 作者单位： | 海军航空工程学院研究生管理大队,烟台,264001;海军航空工程学院青岛分院,青岛,266041 |
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| 摘 要： | 针对直升机的振动情况,分析了振动的危害和引起振动的各种激振力,主要介绍了用于减振的结构优化设计,被动式减振技术和主动式减振技术的原理及应用,最后展望了减振技术的发展趋势。
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| 关 键 词： | 直升机 振动 旋翼 |
| 修稿时间： | 2003年12月25 |
Research on Vibration and Vibration Reduction Characteristics of Helicopter |
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| LIU Wen-lin,MU Zhi-tao,DUAN Cheng-mei.Research on Vibration and Vibration Reduction Characteristics of Helicopter[J].Journal of Naval Aeronautical Engineering Institute,2004,19(5):533-536. |
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| Authors: | LIU Wen-lin MU Zhi-tao DUAN Cheng-mei |
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| Institution: | LIU Wen-lin Graduate Students'Bridge of NAEI,Yantai,264001,MU Zhi-tao DUAN Cheng-mei Qingdao Branch of NAEI,Qingdao,266041 |
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| Abstract: | Based on the vibration of helicopter,the effect of vibration on helicopter and the forces,which can induce vibration are analyzed.The principle and application of structure optimal design,passive and active vibration reduction systems are mainly dealt with.Finally the new technology and development on vibration reduction are presented. |
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| Keywords: | helicopter vibration rotor wings |
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