Effect of Riveting Angle and Direction on Fatigue Performance of Riveted Lap Joints

被引：8
|
作者：
Liang, Qingxiao [1 ,2 ]
Zhang, Tianpeng [3 ]
Zhu, Chunrun [3 ]
Bi, Yunbo [3 ]
机构：
[1] Northwestern Polytech Univ, Sch Mech Engn, Xian 710072, Peoples R China
[2] AVIC Xian Aircraft Ind Grp Co LTD, Xian 710089, Peoples R China
[3] Zhejiang Univ, Coll Mech Engn, Key Lab Adv Mfg Technol Zhejiang Prov, Hangzhou 310027, Peoples R China
来源：
COATINGS | 2021年 / 11卷 / 02期
基金：
中国国家自然科学基金;
关键词：
riveting angle; riveting direction; finite element analysis; fatigue performance; riveted lap joint; PROCESS PARAMETERS; COUNTERSUNK; QUALITY; STRESS; METAL; LIFE;
D O I：
10.3390/coatings11020236
中图分类号：
T [工业技术];
学科分类号：
08 ;
摘要：
Riveting is the most commonly used connection method in aircraft assembly, and its quality has a crucial effect on the fatigue performance of aircraft. Many factors affect the riveting quality, among which the influence of the riveting angle and direction is not clear. In this paper, a three-dimensional finite element model of single-rivet lap joints is established and verified by the driven head geometry and the riveting force data obtained from the riveting experiments. Then, by adjusting the angle and direction of the punch in the finite element model, the riveting process is simulated at the angles of 0 degrees, 1 degrees, 2 degrees, and 3 degrees and the directions of 0 degrees and 180 degrees to investigate the deformation of the lap joints, the stress distribution around the hole, and the stress distribution of the rivet. Finally, the fatigue tests of the single-rivet lap joints are performed and the influence of the riveting angle and direction on the connection quality and fatigue performance of the riveting joints is analyzed.
引用
收藏
页码：1 / 23
页数：22
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