轴向过载下固体推进剂药柱变形研究  

Deformation of solid propellant grains under axial acceleration load

作　　者：刘中兵 利凤祥 李越森 胡春波[2] 

机构地区：[1]陕西动力机械研究所,陕西西安710025 [2]西北工业大学航天工程学院,陕西西安710072

出　　处：《推进技术》2004年第2期162-164,共3页Journal of Propulsion Technology

摘　　要：采用Φ315试验发动机,对某新型推进剂翼槽型药柱进行了10g,20g,30g和35g的轴向过载离心实验,测量了药柱前端面靠近内孔处测点的位移;并运用三维线性粘弹性有限元模型,对离心实验过程进行了数值模拟,以确定固体推进剂药柱在轴向过载作用下的变形问题。结果表明,计算值与实验结果符合较好,证实了粘弹性有限元模型适用于过载条件下药柱变形的研究。Using Φ315 test motor, the centrifugal test of 10 g, 20 g, 30 g and 35 g axial acceleration for a new propellant grain with fin-slots was completed. The displacements of the spots near inner hole in the fore end surface of the grain were measured. Using three dimensional linear viscoelasticity finite element model, numerical simulation was performed. The deformation of solid propellant grain under axial acceleration was investigated. The result shows that the difference between calculation and experiment is comparative small. It is approved that viscoelasticity finite element model can be used to the deformation study of grains under accelerations.

关 键 词：轴向载荷 有限元法 离心试验 固体推进剂 药柱变形 

分 类 号：V512[航空宇航科学与技术—航空宇航推进理论与工程]