蜂窝结构热膨胀系数测量技术研究

Xiaojun Tang, Lixia Liu, Guobao Dai, Zijie Sun, Yaodong Yang, Ao Li
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引用次数: 0

摘要

蜂窝结构因其重量轻、强度高而被广泛用作航空、航天等领域承重结构的主要夹层。在某些使用条件下,蜂窝结构受高低温影响而产生的变形会影响结构的整体力学性能。因此,准确评估蜂窝结构的热膨胀性能成为结构设计的关键。然而,现有的热膨胀系数测量方法主要存在中空结构无法有效接触、网格光学目标面积有限且难以检测等问题。针对上述情况,本文提出了一种测量蜂窝结构热膨胀系数的方法,并建立了测量系统,通过对蜂窝结构的测试,有效地获得了蜂窝结构的热膨胀性能。同时,利用标准试件验证了系统的测量精度。实验结果表明,该方法具有很高的测量精度。
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Research on Measurement Technology of Coefficient of Thermal Expansion of Honeycomb Structure
Honeycomb structure is widely used as the main sandwich layer of load-bearing structure in aviation, aerospace and other fields because of its light weight and high strength. Under some service conditions, the deformation of the honeycomb structure affected by high and low temperature will affect the overall mechanical performance of the structure. Therefore, accurate evaluation of the thermal expansion performance of the honeycomb structure becomes the key to structural design. However, the existing measurement methods of thermal expansion coefficient mainly have problems such as the hollow structure cannot be effectively contacted, the area of the grid optical target is limited and difficult to detect. In view of the above conditions, in this paper, a method for measuring the thermal expansion coefficient of honeycomb structure is proposed, and the measurement system is built, and the thermal expansion performance of honeycomb structure is effectively obtained by testing the honeycomb structure. At the same time, the measurement accuracy of the system is verified by using standard test pieces. The experimental results show that the method has high measurement accuracy.
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