基于Solidworks与ADAMS机载导弹弹射机构的设计与联合仿真  

Design and Combined Simulation Based on Solidworks and ADAMS Ejection Mechanism

作　　者：李海军[1] 王殿宇[1] 陈育良[1] 

机构地区：[1]海军航空工程学院兵器科学与技术系,山东烟台264001

出　　处：《测试技术学报》2016年第1期10-16,共7页Journal of Test and Measurement Technology

摘　　要：针对我国目前传统机载导弹弹射装置的弊端,提出一种采用EHA作为动力源,压缩弹簧蓄能弹射的新型弹射装置.利用Solidworks建模软件建立弹射装置的三维装配模型,将其导入动力学分析软件ADAMS中,并设计边界条件及约束条件,对弹射过程进行仿真分析.仿真结果表明,本文所设计的弹射装置合理可行,满足弹射技术要求.According to the disadvantages of traditional airborne missile ejection mechanism in our country,a new type of ejection compression spring energy storage ejection mechanism which uses the EHA as a sources of power is presented in this paper.Using Solidworks modeling software to establish 3 dassembly model of ejection device,import it into large dynamics analysis software ADAMS.Design boundary conditions and constraints of the ejection process simulation analysis.The simulation results show that the designed ejection mechanism and is feasible,meet the ejection technical requirements.

关 键 词：机载导弹 弹射装置 弹簧蓄能 联合仿真 

分 类 号：TJ760.2[兵器科学与技术—武器系统与运用工程]