Reliability Study on Integral Ring Key Assembly of Small Solid Rocket Motor

Zhi-qiang Hu, Tao Yang, Bin-bin Zhang
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Abstract

In this paper, the reliability of integral ring key assembly of small solid rocket motor is analyzed by simulation and experiment. The integral ring key is a rectangular block composed of some special metal materials, which is directly contact with the motor housing during the assembly process. There are many problems of integral ring key the assembly process, such as large deformation, large friction and metal forming, so it is difficult to install. According to the technical requirements, the platform of assembly is designed. In order to provide different types of small solid rocket motors with integral ring key assembly, the pneumatic element, gas-liquid booster cylinder and ring key positioning structure are adopted to achieve integral ring key assembly. The ring key positioning device is equipped with a variety of positioning components, it can achieve different types of integral ring key assembly. Display dynamics method is used to simulate, within 36 seconds, the deformation and assembly process of certain type of integral ring key. The finite element stress and strain analysis of integral ring key connection structure is carried out in detail.
小型固体火箭发动机整体环键总成可靠性研究
本文通过仿真和实验对小型固体火箭发动机整体环键总成的可靠性进行了分析。整体环键是由一些特殊金属材料组成的矩形块,在装配过程中与电机外壳直接接触。整体环键在装配过程中存在许多问题,如变形大、摩擦大、金属成型等,因此安装困难。根据技术要求,设计了装配平台。为了给不同型号的小型固体火箭发动机提供整体式环键总成,采用气动元件、气液助力缸和环键定位结构实现整体式环键总成。该环键定位装置装有多种定位元件,可实现不同类型的整体环键装配。采用显示动力学方法,在36秒内模拟了某型整体环键的变形和装配过程。对整体环键连接结构进行了详细的有限元应力应变分析。
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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