铆接工艺参数对复合材料双面埋头结构力学性能影响研究

丁梦; 陈昆岚; 张铭豪; 谭学才; 蔡鹏; 曹增强

doi:10.16080/j.issn1671-833x.25010123

您当前的位置：

首页 >

文章列表页 >

铆接工艺参数对复合材料双面埋头结构力学性能影响研究

研究论文 | 更新时间：2026-06-16

- 铆接工艺参数对复合材料双面埋头结构力学性能影响研究
- 航空制造技术 2026年69卷第10期页码：147-158
- 作者机构：
  
  凌云科技集团有限责任公司，武汉 430040
  凌云（宜昌）航空装备工程有限公司，宜昌 444100
  西北工业大学，西安 710072
  陕西大工旭航电磁科技有限公司，西安 710100
- 作者简介：
  
  曹增强，教授，博士生导师，研究方向为飞机先进装配与长寿命连接技术、电磁加载技术。
- 基金信息：
  
  陕西省2025年自然科学基础研究计划(2025SYS-SYSZD-064)
- DOI：10.16080/j.issn1671-833x.25010123
  中图分类号： V257
- 收稿：2025-07-16，
  
  修回：2025-08-17，
  
  录用：2025-10-09，
  
  纸质出版：2026-05-15
- 稿件说明：
移动端阅览
引文格式：丁梦，陈昆岚，张铭豪，等.铆接工艺参数对复合材料双面埋头结构力学性能影响研究[J].航空制造技术，2026, 69（10）：25010123.

DING Meng, CHEN Kunlan, ZHANG Minghao, et al. Research on effects of riveting process parameters on mechanical properties of CFRP double-sided countersunk structures[J]. Aeronautical Manufacturing Technology, 2026, 69(10): 25010123.
引文格式：丁梦，陈昆岚，张铭豪，等.铆接工艺参数对复合材料双面埋头结构力学性能影响研究[J].航空制造技术，2026, 69（10）：25010123. DOI： 10.16080/j.issn1671-833x.25010123.

DING Meng, CHEN Kunlan, ZHANG Minghao, et al. Research on effects of riveting process parameters on mechanical properties of CFRP double-sided countersunk structures[J]. Aeronautical Manufacturing Technology, 2026, 69(10): 25010123. DOI： 10.16080/j.issn1671-833x.25010123.

摘要

碳纤维增强复合材料（Carbon fibre-reinforced polymer

CFRP）/金属双面埋头铆接结构可以满足飞机气动外形和轻量化连接的需求。为研究铆接工艺参数对复合材料双面埋头结构力学性能的影响，针对实际机型结构中CFRP/30CrMnSiA高强钢和CFRP/2A12硬铝合金两种叠层形式，以及TA1纯钛实心埋头铆钉和Ti45Nb半空心尾管埋头铆钉两种铆钉类型，开展了不同钉孔间隙下气动压铆和电磁铆接工艺试验和准静态拉伸试验。结合铆接干涉行为和失效模式对铆接工艺参数影响接头力学性能的作用机制进行了研究。结果表明，在一定范围内增加钉孔间隙可以提高接头剪切强度，然而过大的钉孔间隙可能导致铆钉提前倾斜而降低连接强度。电磁铆接较气动压铆可将接头强度提升3.8%～12.1%。使用TA1铆钉时，CFRP/30CrMnSiA高强钢接头的接头强度要比CFRP/2A12硬铝合金接头高出约8%，更换Ti45Nb铆钉后，二者差别不大，几何尺寸的差异是导致TA1铆钉接头和Ti45Nb铆钉接头强度差别最主要的原因。

Abstract

Carbon fibre-reinforced polymer/metal double-sided countersunk riveted structures can meet the requirements for aerodynamic shape and lightweight joining of aircraft. This paper focuses on two overlapping forms of CFRP/30CrMnSiA high-strength steel and CFRP/2A12 aluminum alloy in actual machine structures

as well as two types of rivets: TA1 pure titanium solid countersunk rivets and Ti45Nb semi-hollow tailpipe countersunk rivets. Pneumatic pressriveting and electromagnetic riveting process tests and quasi-static tensile tests were conducted under different rivet-hole clearances. The mechanism by which riveting process parameters affect the mechanical properties of joints was explained by combining riveting interference behavior and failure modes. The results indicate that increasing the rivet-hole clearances can improve the shear strength of the joint

but excessive clearances may cause the rivet to tilt prematurely and reduce the joining strength. Electromagnetic riveting can increase the peak load by 3.8% to 12.1% compared to pneumatic pressriveting. When using TA1 rivets

the peak load of CFRP/30CrMnSiA high-strength steel joints is about 8% higher than that of CFRP/2A12 hard aluminum alloy joints. After replacing with Ti45Nb rivets

the difference between the two is not significant

and the difference in geometric dimensions is the main reason for the strength difference between the TA1 rivet joint and the Ti45Nb rivet joint.

关键词

Keywords

references

SUO H Y, DENG K L, ZHANG K F, et al. Static/fatigue response and degradation behaviors of CFRP/Ti bolted joints under salt-fog and ultraviolet synergistic marine environment[J]. Thin-Walled Structures, 2024, 203: 112251.

曹增强，张铭豪，谭学才，等.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, et al. Overview of riveting technology for aviation composite structure[J]. Aeronautical Manufacturing Technology, 2023, 66(1/2): 26-37.

程晖，樊新田，徐冠华，等.航空复合材料结构精密干涉连接技术综述[J].航空学报，2021, 42(10): 48-66.

CHENG Hui, FAN Xintian, XU Guanhua, et al. State of the art of precise interference-fit technology for composite structures in aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2021, 42(10): 48-66.

XU J Y, EL MANSORI M. Experimental study on drilling mechanisms and strategies of hybrid CFRP/Ti stacks[J]. Composite Structures, 2016, 157: 461-482.

JIAO F, LI Y X, NIU Y, et al. A review on the drilling of CFRP/Ti stacks: Machining characteristics, damage mechanisms and suppression strategies at stack interface[J]. Composite Structures, 2023, 305: 116489.

PRAMANIK A, BASAK A K, DONG Y, et al. Joining of carbon fibre reinforced polymer (CFRP) composites and aluminium alloys-A review[J]. Composites Part A: Applied Science and Manufacturing, 2017, 101: 1-29.

李永兵，马运五，楼铭，等.轻量化薄壁结构点连接技术研究进展[J].机械工程学报，2020, 56(6): 125-146.

LI Yongbing, MA Yunwu, LOU Ming, et al. Advances in spot joining technologies of lightweight thin-walled structures[J]. Journal of Mechanical Engineering, 2020, 56(6): 125-146.

CHAKHERLOU T N, TAGHIZADEH H, AGHDAM A B. Experimental and numerical comparison of cold expansion and interference fit methods in improving fatigue life of holed plate in double shear lap joints[J]. Aerospace Science and Technology, 2013, 29(1): 351-362.

谢鸣九.复合材料连接技术[M].上海：上海交通大学出版社，2016.

XIE Mingjiu. Joints for composites materials[M]. Shanghai: Shanghai Jiao Tong University Press, 2016.

NEWMAN J C Jr, RAMAKRISHNAN R. Fatigue and crackgrowth analyses of riveted lap-joints in a retired aircraft[J]. International Journal of Fatigue, 2016, 82: 342-349.

薛红前.飞机装配工艺学[M].西安：西北工业大学出版社，2015.

XUE Hongqian. Aircraft assembly technology[M]. Xi'an: Northwestern Polytechnical University Press, 2015.

SKORUPA A, SKORUPA M, MACHNIEWICZ T, et al. Fatigue crack location and fatigue life for riveted lap joints in aircraft fuselage[J]. International Journal of Fatigue, 2014, 58: 209-217.

KORBEL A. Effect of aircraft rivet installation process and production variables on residual stress, clamping force and fatigue behaviour of thin sheet riveted lap joints[J]. Thin-Walled Structures, 2022, 181: 110041.

ZHANG M H, CAO Z Q, CAO Y J, et al. Investigation on interference and damage behaviours of electromagnetic riveted double-sided countersunk 30CrMnSiA/CFRP joints[J]. Composite Structures, 2024, 329:117824.

CAO Z Q, CARDEW-HALL M. Interference-fit riveting technique in fiber composite laminates[J]. Aerospace Science and Technology, 2006, 10(4): 327-330.

LI S P, ZHANG S G, LI H, et al. Numerical and experimental investigation of fitting tolerance effects on bearing strength of CFRP/Al single-lap blind riveted joints[J]. Composite Structures, 2022, 281: 115022.

DE RIJCK J J M, HOMAN J J, SCHIJVE J, et al. The driven rivet head dimensions as an indication of the fatigue performance of aircraft lap joints[J]. International Journal of Fatigue, 2007, 29(12): 2208-2218.

JIANG H, LI G Y, ZHANG X, et al. Fatigue and failure mechanism in carbon fiber reinforced plastics/aluminum alloy single lap joint produced by electromagnetic riveting technique[J]. Composites Science and Technology, 2017, 152: 1-10.

ZENG C, XUE J T, LIU X Y, et al. Design variables influencing the fatigue of Al2024-T3 in riveted aircraft lap joints: Squeeze force and initial fit tolerance[J]. International Journal of Fatigue, 2020, 140: 105751.

李辉，易成君，王倩，等.复合材料斜面压铆和锤铆铆接质量对比分析[J].航空制造技术，2017, 60(18): 97-99, 105.

LI Hui, YI Chengjun, WANG Qian, et al. Contrastive analysis on quality of compression riveting and hammer riveting of slant composites[J]. Aeronautical Manufacturing Technology, 2017, 60(18): 97-99, 105.

曹增强，左杨杰.电磁铆接[M].北京：国防工业出版社，2018.

CAO Zengqiang, ZUO Yangjie. Electromagnetic riveting[M]. Beijing:National Defense Industry Press, 2018.

LI G Y, JIANG H, ZHANG X, et al. Mechanical properties and fatigue behavior of electromagnetic riveted lap joints influenced by shear loading[J]. Journal of Manufacturing Processes, 2017, 26: 226-239.

LIU S W, ZHANG W F, WU Y F, et al. The damage investigation of wedge-shaped electromagnetic riveting structure of CFRP/aluminium alloy[J]. Journal of Testing and Evaluation, 2013, 41(2): 188-193.

ZHANG M H, CAO Z Q, GUO Y J, et al. Stress, damage, and fatigue performance analysis of CFRP/Al double-sided countersunk riveted joints with variable rivet-hole clearance[J]. International Journal of Fatigue, 2024, 186: 108385.

QU L G, LI P, LV G M, et al. Rivet structural design and process optimization for the double-sided countersunk riveting of composite wedge structures[J]. Aerospace, 2024, 11(2): 165.

TIAN S, LI C Y, DAI W B, et al. Effect of the countersunk hole depth on tensile-tensile fatigue behavior of riveted specimens of AA2024 - T3 alloy[J]. Engineering Failure Analysis, 2020, 115: 104639.

EGAN B, MCCARTHY C T, MCCARTHY M A, et al. Stress analysis of single-bolt, single-lap, countersunk composite joints with variable bolt-hole clearance[J]. Composite Structures, 2012, 94(3): 1038-1051.

杨白凤.碳纤维/双马树脂基复合材料及其连接结构在空天环境温度下的力学行为[D].西安：西北工业大学，2018.

YANG Baifeng. Mechanical behaviour of carbon fiber/BMI composites and joints at space environment temperature[D]. Xi'an: Northwestern Polytechnical University, 2018.

中央军委装备发展部.铝合金预拉伸板材规范： GJB 1741A—2018[S].北京：国家军用标准出版发行部，2019.

Central Military Commission Equipment Development Department. Specification for aluminum alloy pre-stretched sheets: GJB 1741A—2018[S]. Beijing: National Military Standard Publishing and Distribution Department, 2019.

中国航空工业总公司.100°沉头纯钛铆钉： HB 6478—1990[S].北京：中国航空综合技术研究所，1990.

China Aviation Industry Corporation. 100° countersunk pure titanium rivet: HB 6478—1990[S]. Beijing: China Aviation General Technology Institute, 1990.

成都飞机设计研究所.钛铌双面埋头铆钉： Q 611S 546—2018[S].成都：成都飞机设计研究所，2018.

Chengdu Aircraft Design and Research Institute. Titanium niobium double-sided countersunk rivet: Q611S 546—2018[S]. Chengdu: Chengdu Aircraft Design and Research Institute, 2018.

刘风雷，刘丹，刘健光.复合材料结构用紧固件及机械连接技术[J].航空制造技术，2012, 55(S1): 102-104, 111.

LIU Fenglei, LIU Dan, LIU Jianguang. Fastener and mechanical joining technology for composites structure[J]. Aeronautical Manufacturing Technology, 2012, 55(S1): 102-104, 111.

ASTM Structural Test Methods Committee. Standard test method for bearing response of polymer matrix composite laminates: ASTM standard D 5961/D 5961M—05[S]. Philadelphia: American Society for Testing and Materials. 2005.

航空航天工业部.紧固件试验方法： GJB 715.19—90[S].北京：国防科学技术工业委员会，1990.

Ministry of Aerospace Industry. Fastener testing method: GJB 715.19—90[S]. Beijing: Commission for Science, Technology and Industry for National Defense, 1990.

国家市场监督管理总局，国家标准化管理委员会.民用飞机复合材料制件铆接要求： GB/T 38825—2020[S].北京：中国标准出版社，2020.

State Administration for Market Regulation. National standardization administration riveting requirements for composite parts of civil aircraft:GB/T 38825—2020[S]. Beijing: China Standard Press, 2020.

MCCARTHY M A, LAWLOR V P, STANLEY W F, et al. Bolt-hole clearance effects and strength criteria in single-bolt, single-lap, composite bolted joints[J]. Composites Science and Technology, 2002, 62(10-11): 1415-1431.

MCCARTHY C T, MCCARTHY M A, STANLEY W F, et al. Experiences with modeling friction in composite bolted joints[J]. Journal of Composite Materials, 2005, 39(21): 1881-1908.

ZHANG M H, CAO Z Q, ZHENG G, et al. Quasi-static tensile failure mechanism analysis of CFRP/Al countersunk electromagnetic riveted joints with different rivet-hole clearances[J]. Engineering Failure Analysis, 2024, 155: 107759.

浏览量

下载量

CSCD

文章被引用时，请邮件提醒。

提交

工具集

关联资源

航空复合材料结构铆接技术综述

电磁铆接驱动力计算及可视化系统设计

单人操作型电磁铆枪研制

手工电磁铆接过程及复合材料铆接质量研究

大直径钢铆钉电磁铆接工艺及性能试验研究