These are the ejection mechanisms for the compartments 这是用来弹射船舱的装置
Okay , these are the ejection mechanisms 这些是弹射装置
We are according to customers special request order and we are provide include : ejection mechanism , move mould setting , mould hot up setting , mould seat , save setting and hydraulic oil etc 同时还可根据客户要求特殊订制供应:顶缸退料装置、移模装置、模具加热装置、模座、安全装置及液压油等。
Our core inserting pulling mechanisms and threading rotation ejection mechanisms international patent give a solution to the problems arising from the operation of oil cylinders , oil motors and electric motors 在国内外尚属空白。采用此抽插芯机构和螺纹转动脱模机构,解决了油缸油马达电机在生产使用中的缺陷。
Firstly , the diagram of the mechanism and the kinematics model is established . afterward , on the basis of this , the kinematics simulation of the missile ejection mechanism is accomplished 首先建立了该系统的物理模型和结构简图,在分析机构的运动过程的基础上,建立了运动学模型,并对导弹弹射机构的运动学模型进行了仿真。
This work is useful to the design and analysis of the new ejection mechanism , especially the new cylinder . finally , we gave some clue for further research basing on the summary of this paper 最后分别分析了不同惯性负载mw 、不同行程s 、不同有效面积ae对作动筒动特性的影响,为设计新的导弹弹射装置特别是气压作动筒提供了理论依据。
With the successfully biding of core inserting pulling mechanisms and threading rotation ejection mechanisms supported by nation innovation financial and the approval of establishing large injection forming molds project technology r d center , jinsu company is gradually switch the center of industry structure to produce high precision and automatism high - end molds , and the base point that supports the new development is gradually emerged . i believe in 2007 jinsu will make great progress 随着公司“模具开合模抽插芯与螺纹转动脱模同步机构”的通过论证与国家创新基金项目的获得与支持,金塑公司在2006年正在逐步地把产业结构重心转移到生产高精度全自动的新型模具方向上来,支撑新一轮快速发展的基点正在逐步形成,我相信在2007年金塑公司必定会乘风破浪更上一层楼。
This paper describes the development and trend of the weapon bay which the fighter plane equipped with at home and abroad , especially the missile ejection mechanism ; the kinematics and dynamics analysis about a sort of missile ejection mechanism is discussed and the model of the system is simulated by the tools in matlab , such as solver and so on 本文在讲述国内外飞机武器舱,特别是导弹弹射系统的发展现状和发展趋势的基础上,对现有引进的某型系统机构进行了运动学和主要部件的动力学分析,并通过matlab提供的解算器等工具对建立的系统模型进行了仿真。