固体火箭发动机密封结构随机有限元可靠性分析

通过研究固体发动机密封结构主要部件橡胶O形密封圈的力学性能,应用积分类随机有限元法实现了密封结构随机因素下的结构响应,完成了固体发动机密封结构在长时间贮存老化和工作状态下的力学性能模拟及随机有限元可靠性分析。

利用积分随机有限元计算结构可靠度

积分随机有限元是一种新型随机有限元,它利用确定性有限元实现随机分析。本文首先利用积分随机有限元得到结构功能函数的各阶矩,通过Gram-Charlier级数拟合得到结构功能函数的概率密度函数,最后利用数值积分计算出结构的可靠度。作为对比,利用直接Monte-Carlo法模拟对结果进行验证,结果表明,本方法利用较少的积分点即可得到较高的计算精度,且随机变量可服从任何分布,与其它的可靠度计算方法相比具有一定的优势。

Research on reliability of turbine disk with random structure

Structure of a rotor and other design parameters are all viewed as constant using finite element software to analyze reliability of the rotor. In this case,reliability analysis of the rotor can't be realized for design parameters as random. Based on theory of elastic mechanics,starting with the micro element of the rotor,stress formulas on arbitrary point of turbine disc with equal and variable thickness are deducted under the influence of centrifugal force and temperature field on rotor system simultaneously. Considering the random of structural size of the turbine rotor,temperature stress,rotating speed,external loads and material strength,the reliability of a rotor is studied with stress-strength interference model,integral stochastic finite element method(ISFEM) and Gram-Charlier series method,and random structural reliability of the rotor is computed with higher accuracy.

涡轮转子随机结构的可靠性研究

以传统的应力-强度干涉模型为基础,考虑了涡轮转子随机结构尺寸、温度应力、转速、外载荷和材料强度等参数的随机性,利用积分随机有限元和Gram-Charlier级数方法对转子局部应力最大处进行可靠性分析.该方法计算结果与Monte-Carlo仿真值比较,二者相对误差非常小,计算结果比较精确,既避免了有限元计算量大和速度慢的情况,又实现了转子随机结构的可靠性计算.