Analysis on contact reliability of missile suspension and rail based on high moment

Q4 Engineering
Yong-shou Liu, Zongzhan Gao, W. Gou, Xin-Dang He
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引用次数: 0

Abstract

The strength reliability and parameter sensitivity of a missile suspension under the condition of assembling with rail were studied.Firstly,finite element redevelopment technology was performed to build parametric models of missile suspension and rails for checking whether the structure strength met the design requirements.Secondly,considering the machining deviation and design tolerances may cause the stochastically of actual dimensions,the structure dimensions of key parts were expressed by random variables.Combining finite element parametric method and the fourth moment reliability method,the strength reliability and parameter sensitivity analysis of the missile suspension structure were performed.According to the reliability analysis results,the missile suspension failure probability 0.000 607 was obtained.The results of sensitivity analysis show that the ear length and ear pieces medial thickness are the main influencing factors of the hanging structural strength;the dimension error is the main reason leading to dispersion of strength.Finally,compared with other reliability methods,the analysis method proposed in this paper possesses higher accuracy and efficiency,which is especially fit for the reliability analysis of complex structures.
基于大力矩的导弹悬架与轨道接触可靠性分析
研究了导弹悬架在轨道装配条件下的强度、可靠性和参数灵敏度。首先,采用有限元再开发技术建立导弹悬架和轨道的参数化模型,校核结构强度是否满足设计要求;其次,考虑到加工偏差和设计公差可能引起实际尺寸的随机性,将关键零件的结构尺寸用随机变量表示。结合有限元参数法和四阶矩可靠度法,对导弹悬架结构进行了强度可靠度和参数灵敏度分析。根据可靠性分析结果,得到导弹悬架失效概率为0.000 607。灵敏度分析结果表明,耳长和耳片内侧厚度是影响悬架结构强度的主要因素,尺寸误差是导致悬架结构强度分散的主要原因。最后,与其他可靠性分析方法相比,本文提出的分析方法具有更高的精度和效率,特别适合于复杂结构的可靠性分析。
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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来源期刊
Guti Huojian Jishu/Journal of Solid Rocket Technology
Guti Huojian Jishu/Journal of Solid Rocket Technology Engineering-Aerospace Engineering
CiteScore
0.80
自引率
0.00%
发文量
4234
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