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固体火箭发动机结构可靠性计算方法分析
ANALYSIS OF CALCULATING METHODS FOR STRUCTURAL RELIABILITY IN SOLID ROCKET MOTORS
【摘要】 依据结构强度-工作应力理论模型,应用数理统计方法和对某团体发动机大量试验数据的实例计算,证明了总体变异系数法和样本变异系数法在结构可靠性计算中的一致性。在置信度为0.90时,其结构可靠度大于0.9954。同时表明总体变异系数法是较佳方法,影响结构可靠性的主要因素是样本标准差。
【Abstract】 he consistance of the population dissociation coefficient method andthe sample dissociation coefficient method for the calculation of structural reliabilityin solid rocket motors was reviewed.At the same time it is shown the population dissociation coefficient method is abetter calculating method for structural reliability in solid rocket motors and themajor factor affecting structural strength reliability is the standard deviation.
【关键词】 固体推进剂火箭发动机;
结构可靠性;
可靠性计算;
可靠性评价;
【Key words】 Solid propellant rocket engine; Structural reliability; Reliability calculation; Reliability assessment;
【Key words】 Solid propellant rocket engine; Structural reliability; Reliability calculation; Reliability assessment;
- 【文献出处】 推进技术 ,JOURNAL OF PROPULSION TECHNOLOGY , 编辑部邮箱 ,1995年01期
- 【分类号】V430
- 【被引频次】7
- 【下载频次】179