1. 西北工业大学,西安,710072
2. 陕西大工旭航电磁科技有限公司,西安,710100
3. 凌云科技集团有限责任公司,当阳,444100
4. 中国民用航空飞行学院,广汉,618307
纸质出版:2023
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曹增强,张铭豪,谭学才,郭程翔,左都全. 航空复合材料结构铆接技术综述[J]. 航空制造技术, 2023, 66(1/2): 26-37. CAO Zengqiang, ZHANG Minghao, TAN Xuecai, GUO Chengxiang, ZUO Duquan. Overview of Riveting Technology for Aviation Composite Structure[J]. Aeronautical Manufacturing Technology, 2023, 66(1/2): 26-37.
CAO Zengqiang, ZHANG Minghao, TAN Xuecai, et al. Overview of Riveting Technology for Aviation Composite Structure[J]. Aeronautical Manufacturing Technology, 2023, 66(1/2).
曹增强,张铭豪,谭学才,郭程翔,左都全. 航空复合材料结构铆接技术综述[J]. 航空制造技术, 2023, 66(1/2): 26-37. CAO Zengqiang, ZHANG Minghao, TAN Xuecai, GUO Chengxiang, ZUO Duquan. Overview of Riveting Technology for Aviation Composite Structure[J]. Aeronautical Manufacturing Technology, 2023, 66(1/2): 26-37. DOI: 10.16080/j.issn1671-833x.2023.01/02.026.
CAO Zengqiang, ZHANG Minghao, TAN Xuecai, et al. Overview of Riveting Technology for Aviation Composite Structure[J]. Aeronautical Manufacturing Technology, 2023, 66(1/2). DOI: 10.16080/j.issn1671-833x.2023.01/02.026.
当前复合材料已成为飞机结构最主要的材料之一,然而我国复合材料应用与世界先进水平相比还存在一定差距,典型特征是复合材料用量占比较低。和金属结构相比,连接是复合材料结构制造与装配的薄弱环节,复合材料各向异性、脆性等特点决定了其连接面临的问题更复杂。复合材料结构采用铆接对于飞机减重、控制制造成本具有积极作用,但复合材料铆接易产生损伤,限制了其在关键连接部位应用。对航空复合材料结构铆接技术的应用进行了系统介绍,包括铆接工艺及方法、复材铆接结构形式和复材铆接所用紧固件;指出铆接过程中复合材料产生损伤的3 个主要方面:制孔过程的损伤,铆接过程复合材料结构表面承受的冲击损伤,以及镦头成形、钉杆膨胀时对复合材料的挤压损伤;重点针对安装过程对复合材料造成的冲击损伤、铆钉膨胀对复合材料造成的挤压损伤进行分析并提出相应的解决措施,主要从减小钉杆膨胀对复材的挤压程度、对复合材料采取保护措施两个方面入手;对比研究结论认为,制定合理的工艺规范、采用先进的铆接工艺方法和重视垫圈的保护作用可以有效抑制复材铆接损伤、提高复材铆接质量。最后,对复合材料铆接技术的发展提出了展望。
Composite materials had become one of the most important materials for aircraft structures. However
there is still a certain gap between the application of composite materials in China and the world’s advanced level. The typical feature is that the proportion of composite materials is relatively low. Compared with metal structures
the connection is the weak link in the assembly and manufacturing of composite structures. The riveting of composite structures has a positive effect on aircraft weight reduction and manufacturing cost control
but the riveting of composite materials is prone to damage
which limits its application in key connection parts. In this paper
the mechanical connection technology of aviation composite structure
especially the application of riveting technology
is systematically introduced
including riveting process and method
composite riveting structure and fasteners used in composite riveting. The damage of the composite material during riveting mainly includes three aspects: The damage in the hole making process
the impact damage on the surface of the composite material structure during riveting
and the extrusion damage to the composite material when the upsetting head is formed and the nail rod is expanded. This paper focuses on the impact damage to composite materials caused by the installation process and the extrusion damage to composite materials caused by the expansion of rivets
and puts forward corresponding solutions
mainly from reducing the extrusion degree of composite materials caused by the expansion of nail bars and taking protective measures for composite materials. Combining with the comparison of relevant research conclusions
it is concluded that formulating reasonable process specifications
adopting advanced riveting process methods and paying attention to the protection of gaskets can effectively suppress the riveting damage of composite materials and improve the riveting quality of composite materials. Finally
the development of composite riveting technology is prospected.
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