Scheme Design and Verification of Heavy-duty Universal Launch Base under Strong Constraints

Hu Binglun, Peng Xueming, Qu Maohua, Li Chong
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Abstract

In order to solve the problem of “The base must be replaced for cartridge replacement” caused by the difference of cartridge length in the current general launch system, this paper proposes an adjustable base which can realize two state height switching and self-locking in a narrow space under the constraint of limited launch compartment space and strong launch recoil force. The key structural parameters are obtained through mechanical analysis, the multi-body dynamics model is established based on Pro/E, the kinematics performance is analyzed based on the virtual displacement principle, and the kinematics and dynamics simulation is verified through ADAMS. Finally, the load performance of the adjustable base is verified through HyperMesh. The results show that the adjustable base proposed in this paper can meet the installation and launch requirements of two types of multi type cartridge, greatly improving the versatility of the launch system and the convenience of adding multi type weapons to ships.
强约束下重型通用发射基地方案设计与验证
为了解决目前一般发射系统中由于弹筒长度不同而导致的“更换弹筒必须更换基座”问题,本文提出了一种可调基座,在有限的发射舱空间和强大的发射后坐力约束下,在狭小的空间内实现两种状态高度切换和自锁。通过力学分析获得关键结构参数,基于Pro/E建立多体动力学模型,基于虚拟位移原理对其运动学性能进行分析,并通过ADAMS进行运动学和动力学仿真验证。最后,通过HyperMesh验证了可调底座的负载性能。结果表明,本文提出的可调基座能够满足两种多型弹的安装和发射要求,大大提高了发射系统的通用性和舰载多型武器的便利性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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