| 直升机耦合动力学设计对减摆器性能和布局的要求 |
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| 引用本文： | 凌爱民.直升机耦合动力学设计对减摆器性能和布局的要求[J].直升机技术,2010(3):1-6. |
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| 作者姓名： | 凌爱民 |
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| 作者单位： | 旋翼动力学国家级重点实验室,江西,景德镇,333001;中国直升机设计研究所,江西,景德镇,333001 |
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| 摘 要： | 从直升机耦合动力学设计的角度,结合型号设计使用情况,讨论分析了如何确定对减摆器性能的设计要求和安装布局,提出了在设计中,应着重考虑和利用减摆器性能的设计点和变化规律。
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| 关 键 词： | 动力学设计 减摆器 性能 布局 |
Requirements of Helicopter Coupled Dynamics Design on Performance and Layout of Dampers |
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| Authors: | LING Aimin |
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| Institution: | LING Aimin1,2(1.National Key Laboratory of Rotorcraft Aeromechanics,Jingdezhen 333001,China,2.China Helicopter Research and Development Institute,China) |
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| Abstract: | In this paper,how to determine the requirements of performance and layout on dampers was discussed and analyzed from the viewpoint of helicopter coupled dynamics design,combined with the engineering design and application.It was suggested that some important design points and characteristics of dampers should be carefully considered and used. |
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| Keywords: | dynamics design damper performance layout |
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