| 直升机振动水平控制技术途径探讨 |
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| 引用本文： | 尹春望,童国荣.直升机振动水平控制技术途径探讨[J].直升机技术,2009(4). |
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| 作者姓名： | 尹春望 童国荣 |
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| 作者单位： | 中国直升机设计研究所,直升机旋翼动力学国防科技重点试验室,景德镇,333001 |
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| 摘 要： | 直升机的振动水平,是衡量当代直升机先进程度最主要的因素之一。直升机振动水平控制是非常复杂的系统工程,需要系统的控制方法、流程和技术。本文将面向工程实际,结合直升机的研制流程,从技术途径方面进行探讨。
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| 关 键 词： | 直升机 振动控制 |
Study of the Technological Approaches to Control Helicopters' Vibration |
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| Authors: | YIN Chunwang TONG Guorong |
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| Institution: | YIN Chunwang; TONG Guorong(National Defense Science&Technology Key Laboratory of Rotorcraft Aeromechanics; China Helicopter Research and Development Institute; Jingdezhen; 333001); |
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| Abstract: | The vibration degree is one of the main factors in judging a helicopter s advantages.It is very complicated to control the vibration degree in helicopter s design and manufacture,and it needs multiple controlling methods,flow and technologies.This paper will study the practicable technological approach that can control the vibration degree in helicopter s design and manufacture. |
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| Keywords: | helicopter vibration control |
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