摘要
叉耳连接结构是一种广泛应用于导弹尾翼连接的结构形式。主要针对某次尾翼静力试验中该类结构在刚度和强度方面出现的问题,建立了等效简化有限元模型,系统分析了螺栓布局、被连接件刚度匹配、螺栓/螺栓孔间隙以及螺栓预紧力对叉耳连接刚度、承载能力的影响。最后,根据分析结果,结合产品工艺性,对原叉耳结构进行了改进,并通过仿真验证了结果的正确性。
Lug joint is a kind of structure widely used in missile empennages connection. Aiming at the problem of the lug joints in a static experiment,we built the equal simplified FEA model,and systematically analyzed the influence of bolts distribution,stiffness matching of connected parts,bolt fit clearance and bolt preload on stiffness and strength of the joints.Finally,based on the analysis and manufacturability,the original structure got improved and validated by FEA simulation.
出处
《机械强度》
CAS
CSCD
北大核心
2018年第1期238-241,共4页
Journal of Mechanical Strength
关键词
叉耳
尾翼连接
连接刚度
承载能力
Lug joint
Empennages connection
Connection stiffness
Load bearing capability
