某型导弹发射装置筒盖系统降载技术研究  

Study on the reducing intensity technology of missile launcher's hatch system

作　　者：张代国 国庆见 吴友生 刘志彬 

机构地区：[1]海军驻郑州地区军事代表室,河南郑州450015 [2]郑州机电工程研究所,河南郑州450015

出　　处：《舰船科学技术》2010年第7期89-93,共5页Ship Science and Technology

摘　　要：通过分析筒盖系统模态和筒口压力场规律,得出筒盖系统最大载荷是由耦合共振引起的结论。根据该结论,提出了在筒盖锁定器与其连接支撑之间增加阻尼器的降载方案。经理论分析,该方案可大大降低筒盖系统在筒口压力场作用下的最大载荷。Through analyzing the mode of the hatch-system and the rules of pressure-field near canister outlet,this report has educed the maximal load acted on the hatch-system is produced by resonance.Based on this conclusion,this report put forward a scheme to reduce the load,which is adding a damper between the locker of the hatch-system and the hatch-system joint.Through analyses,this scheme could reduce the load mostly acted on hatch-system by the pressure-field near canister outlet.

关 键 词：发射装置 筒盖系统 筒口压力场 阻尼器 

分 类 号：E925[军事—军事装备学] TJ76[兵器科学与技术—武器系统与运用工程]