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导弹起竖臂的静动态有限元分析
引用本文:黎刚果,张锡恩,王磊,刘于端. 导弹起竖臂的静动态有限元分析[J]. 兵工自动化, 2006, 25(2): 35-37
作者姓名:黎刚果  张锡恩  王磊  刘于端
作者单位:军械工程学院;军械工程学院
摘    要:某型导弹起竖臂静动态有限元模型在ANSYS中建立,并采用动静法对其分析.模型含起升载荷,臂架结构自重载荷、导弹重力等载荷.当起竖臂所载起升质量突然离地起升或下降制动时,将起升和导弹重力载荷乘以起升载荷动荷系数或乘以起升冲击系数,获得前10阶振型.对起竖臂动态分析中,起竖臂低阶振型表现为起竖臂整体的振动,高阶振型则为起竖臂某个局部的振动.

关 键 词:ANSYS  有限元模型  动静法  振型  导弹起竖臂
文章编号:1006-1576(2006)02-0035-03
收稿时间:2005-07-26
修稿时间:2005-09-01

Finite Element Analysis of Static-Dynamic for Certain Missile Erecting Arm
LI Gang-guo,ZHANG Xi-en,WANG Lei,LIU Yu-duan. Finite Element Analysis of Static-Dynamic for Certain Missile Erecting Arm[J]. Ordnance Industry Automation, 2006, 25(2): 35-37
Authors:LI Gang-guo  ZHANG Xi-en  WANG Lei  LIU Yu-duan
Affiliation:1. Dept. of Missile Engineering, Ordnance Engineering College, Shijiazhuang 050003, China; 2. Team of Equipment Repairing, Unit of Tibet Military Area, Lhasa 850000, China; 3. No.458 of Village Anhuai out of Zhongyang Gate, Nanjing 210028, China
Abstract:The finite element model of static-dynamic for certain missile erecting arm was built in ANSYS,and was analyzed in dynamic-static method.The model includes rising load,load of arm structure weight,load of missile weight and so on.When the erecting arm rose or stopped suddenly,the rising load and the load of missile weight were multiplied with the rising-load coefficient or rising-impulse coefficient;then,the first 10-vibration mode was got.In the dynamic analysis of rising arm,the lower vibration mode of the erecting arm was the vibration of the whole rising arm and the higher vibration mode of the erecting arm was the vibration of certain parts of the arm.
Keywords:ANSYS  Finite element model  Dynamic-static method  Vibration mode  Missile erecting arm
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