轰炸机巡航导弹旋转投弹仿真研究  

Simulation Analysis of Cruise Missile Rotary Launch inside Bomber

作　　者：李海军[1] 莫子烯 LI Hai-jun;MO Zi-xi(Department of Mechanical and Electrical Engineering,Naval Aeronautical University,Yantai Shandong 264001,China)

机构地区：[1]海军航空工程学院机械电子工程系,山东烟台264001

出　　处：《计算机仿真》2018年第7期37-40,174,共5页Computer Simulation

摘　　要：高机动性和隐身设计是现代战机研制的主流方向,也是战略轰炸机必不可少的技术要求。国产轰炸机一般采取外挂式发射巡航导弹,这种发射方式气动阻力大,不利于飞机的隐身,使飞机难以实现机动突防,进行远程战略打击。设计一种适用于国产轰炸机弹舱的旋转发射架,实现巡航导弹内埋式发射。在SolidWorks中建立其三维装配体模型,然后将模型导入多体动力学分析软件ADAMS中分析其动力学特性。分析结果表明,旋转发射架的动力学性能满足要求,能实现正常的转动和投弹。High mobility and stealthy design are the main directions for the development of modern fighters and it is also an essential technical requirement for strategic bomber. Our strategic bombers can only launch cruise missile outside the weapon bay, which is not good for the aerodynamics and stealth performance of a strategic bomber. In or- der to launch cruise missile inside bomber weapon bay, a new kind of rotary launcher was designed. Its 3 D model was built using SofidWorks and then the model was imported into ADAMS to analyze its vibration situation. We find out that the dynamic performance of rotary launcher can meet the requirements and realize the normal rotation and bomb- ing function.

关 键 词：战略轰炸机 旋转发射架 动力学仿真 

分 类 号：TJ762.2[兵器科学与技术—武器系统与运用工程]