航天全复合材料异型贮箱密封仿真分析及验证

Simulation analysis and verification of aerospace full composite shaped storage tank seal

  • 摘要: 异型贮箱在提高结构空间利用效率、承担载荷方面,相较传统长柱型和球形贮箱更具优势。盛装燃料不渗漏是动力系统对贮箱的最基本要求。针对目前复合材料贮箱以强度和刚度设计为主,密封抗渗漏设计考虑不足的问题,本文以某型全复合材料异型贮箱为研究对象,开展抗渗漏设计与分析工作。首先,通过识别易渗漏部位,设计典型元件并进行充压试验,并结合无损检测与断口微观形貌分析,验证了密封涂层的可靠性。基于试验结果,进一步开展典型元件充压试验仿真分析,考虑尺寸效应对密封性能的影响,初步确定了HM-111密封涂层的许用张开位移0.076 mm。最后,对复合材料异型贮箱进行了结构设计,考虑刚度强度的同时,引入密封涂层的许用张开位移,通过与贮箱压力测试的实验结果对比,验证了张开位移作为密封涂层失效判定能够满足贮箱抗渗漏设计需求。

     

    Abstract: The shaped storage tank has more advantages than the traditional long-column and spherical storage tank in improving the utilization efficiency of structural space and bearing load. Holding fuel without leakage is the most basic requirement of the power system for the storage tank. In view of the problem that the strength and stiffness design of composite storage tank are the main design, and the sealing anti-leakage design is not considered enough, this paper takes a special type of composite storage tank as the research object to carry out anti-leakage design and analysis. Firstly, the reliability of the sealing coating is verified by identifying the leaky parts, designing typical components and performing pressure test, combined with non-destructive testing and fracture micro-structure analysis. Based on the test results, the simulation analysis of typical component charging test was further carried out, and the allowable opening displacement of HM-111 sealing coating was preliminarily deter-mined by considering the influence of size effect on sealing performance. Finally, the structure design of the composite special-shaped tank is carried out. Considering the rigidity and strength, the allowable opening dis-placement of the sealing coating is introduced. By comparing with the experimental results of the pressure test of the tank, the opening displacement as the failure determination of the sealing coating can meet the requirements of the anti-leakage design of the tank.

     

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