王文煜1,2, 李锋3, 任飞翔3, 韦兴宇1,2, 熊健1,2()
收稿日期:
2023-12-20
修回日期:
2024-02-02
接受日期:
2024-03-20
出版日期:
2024-04-03
发布日期:
2024-03-29
通讯作者:
熊健
E-mail:jx@hit.edu.cn
基金资助:
Wenyu WANG1,2, Feng LI3, Feixiang REN3, Xingyu WEI1,2, Jian XIONG1,2()
Received:
2023-12-20
Revised:
2024-02-02
Accepted:
2024-03-20
Online:
2024-04-03
Published:
2024-03-29
Contact:
Jian XIONG
E-mail:jx@hit.edu.cn
Supported by:
摘要:
轻质高强复合材料网格加筋壳体结构因其卓越的比强度、比刚度及设计灵活性,被广泛应用于航空航天领域。其制备工艺涉及纤维缠绕、模压和嵌锁等多种技术,确保结构的精确性与稳定性。概述了其制备工艺(纤维缠绕、模具热压及嵌锁成型)及力学性能表征方法,包括静力学失效模式、极限载荷及动力学模态振型分析。此外,综述了航空航天领域复合材料多功能化的最新研究进展,并展望了其未来发展趋势,旨在为相关领域的研究与应用提供有价值的参考。
中图分类号:
王文煜, 李锋, 任飞翔, 韦兴宇, 熊健. 轻质高强复合材料网格加筋壳体结构设计方法及力学性能研究进展[J]. 航空学报, 2024, 45(17): 530001-530001.
Wenyu WANG, Feng LI, Feixiang REN, Xingyu WEI, Jian XIONG. Research progress on structural design methods and mechanical properties of lightweight high⁃strength composite lattice stiffened shell structure[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(17): 530001-530001.
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