论文以122mm火箭炮为研究对象,通过查阅当前国内外关于火箭炮高低平衡结构的文献资料,阐述火箭炮平衡机构的分类及工作原理并对该新火箭炮的整体构型进行论证。在对火箭炮平衡机功能了解的基础上,根据火箭炮平衡机设计原理,给定相关条件,对火箭炮重力矩进行分析,进而得到所需的平衡力矩。根据双弹簧变刚度推式平衡机三点控制设计方法进行平衡机弹簧的总体设计,并阐述该平衡机阻尼装置的原理。最终得到所需的满足要求的火箭炮平衡5931
关键词 火箭炮、平衡机、重力矩、平衡力矩、双弹簧、阻尼
毕业设计说明书(论文)外文摘要
Title Contain redundant translation of the movement of the high and low machine system launcher balance machine design
Abstract
This paper is based on a 122mm rocket launcher as the research object, access to current home and abroad about rocket launcher discretion of the literature of equilibrium structure, expounds the classification of balancing mechanism rocket and the working principle of the new rocket and the whole of the configuration of the argument. In the balance of rocket machine function understand foundation, according to the rocket launcher balance machine design principle, given related conditions, analysis of rocket launcher heavy torque, and find the balance torque. According to the dual spring push type variable stiffness balance machine three control design methods and balance machine general design of the spring, and expounds the principle of balance machine damping device. Eventually find the meet the requirements of the rocket launcher balance machine.
Keywords Rocket launchers, balancing machines, heavy torque, balance torque, double spring, damping
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