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As the power transmission system of an aircraft,a hydraulic pipeline system is equivalent to the " blood vessel" of the aircraft. With the development of aircraft hydraulic system to high pressure,high speed and high power ratio,the fluid-structure interaction vibration mechanism of hydraulic pipeline is more complex and the influence of friction coupling on vibration cannot be ignored. The fluid-structure interaction of hydraulic pipeline will lead to system vibration,lower reliability of system operation and even pipeline rupture. Taking a hydraulic pipeline of C919 aircraft wingtip as the research object,a 14-equation model of fluid-structure interaction vibration considering friction coupling effect is established in this paper. The effects of friction and fluid parameters on the pipeline fluid-structure interaction vibration characteristics are studied and verified by experiments. The research results will provide theoretical guidance for the analysis of the pipeline fluid-structure interaction vibration and have important theoretical significance and great engineering value for promoting the localization process of large aircraft. 相似文献
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针对一种参数可变液压蓄能器样机(其充气压力、充气体积、工作介质阻尼系数及进油口结构参数能够根据液压系统工况变化实时调整),采用磁流变液作为其主要工作介质之一,通过磁流变液工作腔实时调整样机的阻尼系数,以满足不同液压系统动态特性的要求.重点研究磁流变液工作腔的结构及其外加电磁线圈磁路,在此基础上建立该部分数学模型,并将其与参数可变蓄能器样机整体数学模型结合进行理论分析,最后通过实验研究验证结构设计及理论分析的正确性. 相似文献
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