Hole surface strengthening mechanism and riveting fatigue life of CFRP/aluminum stacks in robotic rotary ultrasonic drilling

被引:9
|
作者
Dong, Song [1 ]
Liao, Wenhe [1 ]
Zheng, Kan [1 ]
Xue, Feng [1 ]
Sun, Lianjun [1 ]
机构
[1] Nanjing Univ Sci & Technol, Sch Mech Engn, Nanjing 210094, Peoples R China
关键词
CFRP/aluminum stacks; Drilling damage; Residual stress; Riveting fatigue life; Robotic rotary ultrasonic; drilling; CUTTING FORCE; VIBRATION; OPTIMIZATION; TEMPERATURE; PREDICTION; STABILITY; BURR; CFRP;
D O I
10.1016/j.cja.2023.03.023
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Carbon fiber reinforced plastic (CFRP) and aluminum stacks are widely used in aviation industry due to light weight and high performance. Millions of rivet holes need to be drilled on body materials, and more than 80% of fatigue cracks occur at the connection holes, so the damage and residual stress of hole surface have crucial effect on the riveting fatigue life of CFRP/aluminum stacks and the flight performance. Recently, robotic rotary ultrasonic drilling (RRUD) technology is a promising method to machine the stacks. However, the hole surface strengthening mechanism in RRUD and the service performance of the riveting joint are not verified. Thus, in this paper, the hole surface strengthening mechanism of RRUD for CFRP/aluminum stacks is investigated, a theoretical residual stress model is established, and the fatigue life experiment of riveted joints is con-ducted. Firstly, analysis on residual stress in RRUD is carried out with consideration of strengthening force and cutting temperature. Residual stress model is established based on the calculation of elastic stress, plastic stress and stress release. Validation experiment results show that ultrasonic vibration changes residual stress from tensile stress to compressive stress. At the same time, comparative damage analysis of CFRP hole exit and hole surface in robotic conventional drilling (RCD) and RRUD is presented. Finally, fatigue strength experiments of riveted joints are con-ducted for performance verification. Experimental results indicate that fatigue life of single-hole riveted joints is increased by 68% with ultrasonic vibration, and four-hole riveted joint arranged according to aerospace design standards is increased by more than 86%.(c) 2023 Production and hosting by Elsevier Ltd. on behalf of Chinese Society of Aeronautics and Astronautics. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/ licenses/by-nc-nd/4.0/).
引用
收藏
页码:471 / 484
页数:14
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