首页> 中文期刊> 《导弹与航天运载技术》 >运载火箭爆炸螺栓承载能力分析方法

运载火箭爆炸螺栓承载能力分析方法

         

摘要

The transverse unlocking plane of fairing in launch vehicle is usually connected by explosive bolts. The empirical formula used for calculating explosive bolt strength is rash without considering local deformation effect. In this paper, finite-element method was adopted to stimulate the local deformation of explosive bolt which disclosed the mechanism of local deformation of explosive bolt. A method for calculating explosive bolt load-bearing capacity was proposed. By comparing with finite-element calculation results, the revised method can enhance the calculating precision of explosive bolt load-bearing capacity significantly.%运载火箭的整流罩横向解锁面一般采用爆炸螺栓连接,目前针对爆炸螺栓强度计算采用的是经验算法,由于没有考虑局部变形效应往往偏于冒进.采用有限元方法对爆炸螺栓的局部变形进行详细的仿真,揭示了爆炸螺栓结构的局部变形机理,并提出一种计算爆炸螺栓承载能力的方法,通过与有限元计算结果的对比,修正后的方法能够大幅提高爆炸螺栓承载力的计算精度.

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