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Study of Bonding Technology and Property of Foam-Sandwich Co-Bulkhead of Cryogenic Tank on Launch Vehicle

机译:运载火箭低温夹层泡沫-三明治式共隔板的粘结技术及性能研究

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摘要

As an ideal layout scheme for launch vehicle, bearing co-bulkhead tank can improve the slenderness ratio of launch vehicle, reduce structure weight and increase structure efficiency. In this paper, a novel cryogenic tank co-bulkhead was fabricated by vacuum assisted resin transfer molding (VARTM) process. Consisting of LD10 alloy and polymethacrylimide (PMI) foam-sandwich, the new cryogenic tank co-bulkhead was designed with variable-thickness, hemi-ellipsoid structure, thermal insulation and bearing function. Fundamental temperature distribution, thermal stress and low-temperature load sensitivity of the foam-sandwich co-bulkhead were also assessed by finite element analysis and environment tests in simulated service environment. The results showed that the analog values highly agreed with the test results, and thermal insulation and bearing function of the foam-sandwich co-bulkhead could satisfy the design requirement, which proved the reliability of bonding quality and feasibility of the bonding technique.
机译:作为运载火箭的理想布局方案,带有轴承的双头坦克可以提高运载火箭的细长比,减轻结构重量并提高结构效率。在本文中,通过真空辅助树脂传递模塑(VARTM)工艺制造了一种新型的低温储罐共挤头。由LD10合金和聚甲基丙烯酰亚胺(PMI)泡沫三明治组成的新型低温储罐共压头设计具有可变厚度,半椭圆结构,隔热和承载功能。还通过有限元分析和模拟服务环境中的环境测试,评估了泡沫-三明治式共挤头的基本温度分布,热应力和低温负荷敏感性。结果表明,该模拟值与试验结果高度吻合,泡沫-三明治式共挤头的隔热和承载性能可以满足设计要求,证明了粘结质量的可靠性和粘结技术的可行性。

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