摘要方舱具有利用率高、机动性好、通用性强、运输方式多样,便于维修以及可以在恶劣环境中提供良好的内部工作环境等独特的优点,特别是在现代化战争中具有不可低估的重要作用。为了满足现代战争对后勤装备补给及时、操作方便快捷、机械化信息化程度高等要求。提高装备的战场生存能力开展“机液平台”的研制具有极其重要的军事和现实意义。49623
本文介绍了一种扩展方舱的展开系统,选择了一个适合复杂地形的结构,并利用液压技术控制扩展方舱的展开与收回,根据该扩展方舱的展开系统液压系统的技术指标对该系统进行整体方案设计。并且讨论和选择了适当的同步方案,控制方案,设计了液压原理图和电气控制图。最后按照所给机构性能参数和液压性能参数进行元件的选择计算,以满足该方舱所要达到的要求指标。
毕业论文关键字: 方舱 同步 电液控制
Abstract
The advantages of shelter are high utilization, mobility, versatility and variety of modes of transport.It also can be convenient for maintenance and can provide unique advantages of the internal working conditions in harsh environments, especially in the important role of modern war can not be underestimated. In order to meet modern warfare, logistical equipment and supplies in a timely manner, easy to operate, high degree of mechanization and informationization requirements. Improve equipment, battlefield survivability to carry out the machine solution platform "developed an extremely important military and practical significance.
This article describes an extension of the commencement of the shelter system, select a structure suitable for complex terrain, and the use of hydraulic technology to control the commencement of the extended shelter and recover the system, according to the technical specifications of the extension tank to expand the system hydraulic system overall program design. And discuss and select the appropriate synchronization scheme, the control program designed hydraulic schematic and electrical control diagram. Finally, in accordance with the given institutional performance parameters and hydraulic performance parameters to component selection and calculation, to meet the requirements of indicators to be achieved in the cabin.
Keywords: shelter Synchronous electro-hydraulic control
目 录
第一章 绪论 1
1.1课题背景 1
1.2方舱扩展电液控制系统设计的意义 1
1.3 国内外发展状况 2
1.4方舱的发展趋势 3
第二章 总体方案的设计 4
2.1方舱的简介 4
2.2方舱的组成部分 4
2.3设计原则 4
2.4方舱结构的选择 5
2.5 驱动装置设计 6
2.5.1确定动力源 6
2.5.2确定动力执行元件 7
2.6控制系统设计 8
2.6.1继电器控制 8
2.6.2PLC控制 8
2.6.3 单片机控制 8
2.6.4计算机控制 8
2.7同步方案的确定 9
2.8系统的维护 12
2.9液压系统空载试验