基于Open CASCADE的复合材料壳体应力响应规律及失效行为

Research on stress response law and failure behavior of composite case based on Open CASCADE

  • 摘要: 纤维缠绕复合材料壳体作为先进固体发动机的重要组成部分,其承载能力直接影响发动机的整体性能。本文基于Open CASCADE (OCC)平台,开发了复合材料壳体仿真分析系统,并以直径Φ480 mm壳体作为研究对象,构建了复合材料壳体参数化仿真模型。在此基础上深入探究了壳体椭球比、筒身长度变化对壳体应力分布的影响规律,并进行了水压爆破试验验证。结果表明:壳体封头处的应力随着椭球比的增加呈现先减小后增大的趋势,当椭球比为1.7时应力分布与等应力封头接近,封头处应力分布较均匀;当筒身长度过小时,由于前后赤道圆处经向弯矩的相互影响,筒身螺旋层纤维方向出现负应力现象。研究成果将为复合材料壳体结构设计参数选取提供理论参考。

     

    Abstract: As an important part of advanced solid engines, the load-bearing ability of filament-wound composite casings affects the overall performance of the engine directly. A simulation and analysis system for composite casings was developed based on the Open CASCADE (OCC) platform. Taking a diameter Φ 480 mm casing as the research object, a parametric simulation model for composite casings was constructed. Building upon this foundation, the influence of the ellipsoidal ratio and the cylindrical section length on the stress distribution of the casing was investigated in depth and a hydraulic burst tests were conducted for validation. The simulation results show that the stress fluctuation at the head of the casing decreases first and then increases with the increase of the ellipsoid ratio, and when the ellipsoid ratio is 1.7, the stress distribution is close to that of the equal stress head, which is more uniform. When the length of the barrel is too small, due to the mutual influence of the meridional bending moments at the front and rear equatorial circles, the negative stress phenomenon occurs in the direction of the spiral fiber of the barrel body. The research results will provide a theoretical reference for the selection of design parameters of composite casing structures.

     

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